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@AIRBUSA330
AIRCRAFT CHARACTERISTICSAIRPORT AND MAINTENANCE PLANNING
AC
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© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.Customer Services
Technical Data Support and Services31707 Blagnac Cedex
FRANCE
Issue: Jan 01/93 Rev: Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 21 - Apr 01/13
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 1
Section 1-1
Subject 1-1-0
Purpose R PURPOSE CHANGED DUE TO MERGINGOF THE MFP AND AC MANUALS.
Section 1-2 R
Subject 1-2-1 N
Glossary N
Subject 01-02-00 D
CHAPTER 2 R
Section 2-1 R
Subject 02-01-00 D
Subject 2-1-1 R
General Aircraft Characteristics Data R DESCRIPTION TITLE UPDATEDNOTE AMENDED
General Aircraft Characteristics Data R DESCRIPTION TITLE UPDATED
Section 2-2 R
Subject 2-2-0 R
General Aircraft Dimensions R DESCRIPTION TITLE UPDATED
FIGURE General Aircraft Dimensions R ILLUSTRATION REVISED
FIGURE General Aircraft Dimensions -(Pre Mod 48979)
R ILLUSTRATION REVISED
General Aircraft Dimensions R DESCRIPTION TITLE UPDATED
FIGURE General Aircraft Dimensions R ILLUSTRATION REVISED
Section 2-3
Subject 2-3-0
HIGHLIGHTSPage 1
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Ground Clearances R ADDED GROUND CLEARANCES FORFLIGHT CONTROLSUPDATED FIGURES LAYOUT.PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Ground Clearances R
FIGURE Ground Clearances N ILLUSTRATION ADDED
FIGURE Ground Clearances N ILLUSTRATION ADDED
FIGURE Ground Clearances - Ailerons Up N ILLUSTRATION ADDED
FIGURE Ground Clearances - AileronsDown
N ILLUSTRATION ADDED
FIGURE Ground Clearances - SpoilersExtended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Slats FullyExtended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Flaps FullyExtended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Flaps-Tracks Fully Extended
N ILLUSTRATION ADDED
Section 2-4 R
Subject 02-04-00 D
Subject 2-4-1 R
Interior Arrangements - Plan View R DESCRIPTION TITLE UPDATED
FIGURE Interior Arrangements - PlanView - Typical Configuration
R ILLUSTRATION REVISED
FIGURE Interior Arrangements - PlanView - Typical Configuration
R ILLUSTRATION REVISED
Section 2-5 R
Subject 2-5-0 R
Interior Arrangements - Cross Section R REVISED TITLE TO ”INTERIORARRANGEMENTS - CROSS SECTION”.DESCRIPTION TITLE UPDATED
FIGURE Interior Arrangements - CrossSection - Typical Configuration
R ILLUSTRATION REVISED
HIGHLIGHTSPage 2
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Section 2-6 R
Subject 02-06-00 D
Subject 2-6-1 R
Lower Deck Cargo Compartments R
FIGURE Lower Deck CargoCompartments - Location and Dimensions
R
FIGURE Lower Deck CargoCompartments - Loading Combinations
R ILLUSTRATION REVISED
FIGURE Lower Deck CargoCompartments - Loading Combinations
N ILLUSTRATION ADDED
Subject 2-6-2 R
Main Deck Cargo Compartment R DESCRIPTION TITLE UPDATED
FIGURE Main Deck Cargo Compartment -Location and Dimensions
N ILLUSTRATION ADDED
FIGURE Main Deck Cargo Compartment -Loading Combinations
R ILLUSTRATION REVISED
FIGURE Main Deck Cargo Compartment -Loading Combinations
R ILLUSTRATION REVISED
FIGURE Main Deck Cargo Compartment -Loading Combinations
R ILLUSTRATION REVISED
FIGURE Main Deck Cargo Compartment -Loading Combinations
R ILLUSTRATION REVISED
Section 2-7
Subject 2-7-0
Door Clearances R DESCRIPTION TITLE UPDATED
FIGURE Door Identification and location -Door Identification
N ILLUSTRATION ADDED
FIGURE Door Identification and Location- Door Identification
N ILLUSTRATION ADDED
FIGURE Door Identification and Location- Door Identification
N ILLUSTRATION ADDED
Section 2-8 N
Subject 2-8-0 N
Escape Slides N
HIGHLIGHTSPage 3
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Escape Slides - Location N ILLUSTRATION ADDED
FIGURE Escape Slides - Location N ILLUSTRATION ADDED
FIGURE Escape Slides - Location N ILLUSTRATION ADDED
Section 2-9 N
Subject 2-9-0 N
Landing Gear Maintenance Pits N
FIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes
N ILLUSTRATION ADDED
FIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes
N ILLUSTRATION ADDED
Landing Gear N
FIGURE Main Landing Gear - General N ILLUSTRATION ADDED
FIGURE Nose Landing Gear - General N ILLUSTRATION ADDED
Section 2-10 N
Subject 2-10-0 N
Exterior Lighting N
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
Section 2-11 N
Subject 2-11-0 N
Antennas and Probes Location N
FIGURE Antennas and Probes - Location N ILLUSTRATION ADDED
FIGURE Antennas and Probes - Location N ILLUSTRATION ADDED
FIGURE Antennas and Probes - Location N ILLUSTRATION ADDED
Section 2-12 N
Subject 2-12-0 N
Engine and Nacelle N
FIGURE Engine and Nacelle - EngineDimensions - PW 4000
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - NacelleDimensions - PW 4000
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Engine and Nacelle - Fan Cowls -PW 4000
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - ThrustReverser Cowls - PW 4000
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - EngineDimensions - TRENT 700
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - NacelleDimensions - TRENT 700
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - Fan Cowls -TRENT 700
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - ThrustReverser Cowls - TRENT 700
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - EngineDimensions - GE CF6-80E1
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - NacelleDimensions - GE CF6-80E1
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - Fan Cowls -GE CF6-80E1
N ILLUSTRATION ADDED
FIGURE Engine and Nacelle - ThrustReverser Cowls - GE CF6-80E1
N ILLUSTRATION ADDED
Subject 2-12-1 N
Auxiliary Power Unit N
FIGURE Auxiliary Power Unit - AccessDoors
N ILLUSTRATION ADDED
Section 2-13 N
Subject 2-13-0 N
Leveling, Symmetry and Alignment N
FIGURE Location of Leveling Points N ILLUSTRATION ADDED
FIGURE Location of Leveling Points N ILLUSTRATION ADDED
FIGURE Location of Leveling Points N ILLUSTRATION ADDED
Section 2-14 N
Subject 2-14-0 N
Jacking for Maintenance N
FIGURE Jacking for Maintenance -Jacking Points Location
N ILLUSTRATION ADDED
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DESCRIPTIONS OF CHANGE
FIGURE Jacking for Maintenance -Jacking Points Location
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Jacking Points Location
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Forward Jacking Point
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Forward Jacking Point
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - WingJacking Points
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - WingJacking Points
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Auxiliary Jacking Point - Safety Stay
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Auxiliary Jacking Point - Safety Stay
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Auxiliary Jacking Point - Safety Stay
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Specific Jack-Nose Dimensions
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Jacking Dimensions
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Jacking Dimensions
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Jacking Dimensions
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - Loadat the Aircraft Jacking Points
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - Loadat the Aircraft Jacking Points
N ILLUSTRATION ADDED
Subject 2-14-1 N
Jacking for Wheel Change N
FIGURE Jacking for Wheel Change - MLGJacking Point Heights
N ILLUSTRATION ADDED
HIGHLIGHTSPage 6
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Jacking for Wheel Change -Jacking of the NLG
N ILLUSTRATION ADDED
FIGURE Jacking for Wheel Change - MLGJacking Point Loads
N ILLUSTRATION ADDED
FIGURE Jacking for Wheel Change - MLGJacking Point Loads
N ILLUSTRATION ADDED
FIGURE Jacking for Wheel Change - NLGJacking Point Loads
N ILLUSTRATION ADDED
FIGURE Jacking for Wheel Change - NLGJacking Point Loads
N ILLUSTRATION ADDED
Subject 2-14-2 N
Support of Aircraft N
FIGURE Support of Aircraft - Location ofShoring Cradles
N ILLUSTRATION ADDED
FIGURE Support of Aircraft - Location ofShoring Cradles
N ILLUSTRATION ADDED
FIGURE Support of Aircraft - Location ofShoring Cradles
N ILLUSTRATION ADDED
CHAPTER 3 R
Section 3-5 R
Subject 3-5-0
Final Approach Speed R PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
Subject 03-05-01 D
CHAPTER 4
Section 4-2
Subject 4-2-0
FIGURE Turning Radii - (Sheet 1) R
FIGURE Turning Radii - (Sheet 2) R
FIGURE Turning Radii - (Sheet 2) R
Section 4-3
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Subject 4-3-0
FIGURE Minimum Turning Radii R
FIGURE Minimum Turning Radii R ILLUSTRATION REVISED
Section 4-4
Subject 4-4-0
Visibility from Cockpit in Static Position. R
FIGURE Visibility from Cockpit in StaticPosition
R
FIGURE Visibility from Cockpit in StaticPosition
R
FIGURE Binocular Visibility ThroughWindows from Captain Eye Position
N ILLUSTRATION ADDED
Section 4-5
Subject 4-5-3
FIGURE 180˚ Turn on a Runway R ILLUSTRATION REVISED
FIGURE 180˚ Turn on a Runway R ILLUSTRATION REVISED
Section 4-7 R
Subject 4-7-0 R
CHAPTER 5 R
Section 5-1 R
Subject 5-1-0 R
Subject 5-1-1
Symbols Used on Servicing Diagrams R ADDED ”BULK TRAIN”.
Subject 5-1-2 R
Typical Ramp Layout - Open Apron R ADDED ”STAND SAFETY LINE”DEFINITION.DESCRIPTION TITLE UPDATED
FIGURE Typical Ramp Layout - OpenApron
R ILLUSTRATION REVISED
FIGURE Typical Ramp Layout - OpenApron
R ILLUSTRATION REVISED
HIGHLIGHTSPage 8
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Typical Ramp Layout - Open Apron R ADDED ”STAND SAFETY LINE”DEFINITION.DESCRIPTION TITLE UPDATED
FIGURE Typical Ramp Layout - OpenApron
R ILLUSTRATION REVISED
Subject 5-1-3 R
Typical Ramp Layout - Gate R ADDED ”STAND SAFETY LINE”DEFINITION.DESCRIPTION TITLE UPDATED
FIGURE Typical Ramp Layout - Gate R ILLUSTRATION REVISED
FIGURE Typical Ramp Layout - Gate R ILLUSTRATION REVISED
Section 5-2 R
Subject 5-2-0 R
Terminal Operations -- Full ServicingTurn-Round Time
R DESCRIPTION TITLE UPDATED
FIGURE Full Servicing Turn-Round TimeChart
N ILLUSTRATION ADDED
Terminal Operations -- Full ServicingTurn-Round Time
N
FIGURE Full Servicing Turn-Round TimeChart
N ILLUSTRATION ADDED
Terminal Operations - Full ServicingTurn-Round Time
N
FIGURE Full Servicing Turn-Round TimeChart
N ILLUSTRATION ADDED
Subject 05-02-01 D
Section 5-3 R
Subject 5-3-0 R
Terminal Operations - Minimum ServicingTurn-Round Time
R DESCRIPTION TITLE UPDATED
FIGURE Minimum Servicing Turn-RoundTime
N ILLUSTRATION ADDED
Terminal Operations - Minimum ServicingTurn-Round Time
N
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Minimum Servicing Turn-RoundTime
N ILLUSTRATION ADDED
Subject 05-03-01 D
Section 5-4 R
Subject 05-04-00 D
Subject 5-4-1
Ground Service Connections Layout R
FIGURE Ground Service ConnectionsLayout
R ILLUSTRATION REVISED
Ground Service Connections Layout R
FIGURE Ground Service ConnectionsLayout
R ILLUSTRATION REVISED
Subject 5-4-3
Hydraulic System R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Green System Ground Service Panel
N ILLUSTRATION ADDED
FIGURE Ground Service Connections -Blue System Ground Service Panel
N ILLUSTRATION ADDED
FIGURE Ground Service Connections -Yellow System Ground Service Panel
N ILLUSTRATION ADDED
Subject 5-4-4
Electrical System R NOTE AMENDED
FIGURE Ground Service Connections -Electrical Service Panel
N ILLUSTRATION ADDED
FIGURE Ground Service Connections -Electrical Service Panel
N ILLUSTRATION ADDED
Subject 5-4-5
Oxygen System R PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Ground Service Connections -Oxygen System
N ILLUSTRATION ADDED
HIGHLIGHTSPage 10
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Service Connections -Oxygen System
N ILLUSTRATION ADDED
Subject 5-4-6
Fuel System R
Subject 5-4-7
Pneumatic System R
FIGURE Ground Service Connections - LPand HP Ground Connectors
N ILLUSTRATION ADDED
Subject 5-4-8
Potable Water System R PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Ground Service Connections -Potable-Water Ground Service Panels
N ILLUSTRATION ADDED
Potable Water System N
FIGURE Ground Service Connections -Potable-Water Ground Service Panels
N ILLUSTRATION ADDED
Potable Water System N
FIGURE Ground Service Connections -Potable-Water Ground Service Panel
N ILLUSTRATION ADDED
Subject 5-4-9
APU Oil System R ADDED ACCESS DOORS FOR ”APU OILSERVICING”.
FIGURE Ground Service Connections -APU Oil Servicing
R
Subject 5-4-10
Vacuum Toilet System R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Waste Water Ground Service Panel
N ILLUSTRATION ADDED
FIGURE Ground Service Connections -Waste Water Ground Service Panel
N ILLUSTRATION ADDED
Section 5-5 R
Subject 5-5-0
HIGHLIGHTSPage 11
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Engine Starting Pneumatic Requirements R ADDED PERFORMANCE REQUIREMENTSFOR PNEUMATIC ENGINE STARTING.CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Example for Use of the Charts R ILLUSTRATION REVISED
FIGURE Engine Starting PneumaticRequirements - GE CF6-80E1 SeriesEngine
N ILLUSTRATION ADDED
FIGURE Engine Starting PneumaticRequirements - Rolls Royce Trent 700Series Engine
N ILLUSTRATION ADDED
FIGURE Engine Starting PneumaticRequirements - Pratt & Whitney PW4000Series Engine
N ILLUSTRATION ADDED
Subject 05-05-01 D
Subject 05-05-02 D
Subject 05-05-03 D
Section 5-6 R
Subject 5-6-0
Ground Pneumatic Power Requirements R ADDED PERFORMANCE REQUIREMENTSOF THE GROUND PNEUMATIC SERVICEEQUIPMENT FOR HEATING ANDCOOLING OF THE CABIN.NOTE AMENDED
FIGURE Ground Pneumatic PowerRequirements - Heating
N ILLUSTRATION ADDED
FIGURE Ground Pneumatic PowerRequirements - Cooling
N ILLUSTRATION ADDED
Subject 05-06-01 D
Subject 05-06-02 D
Section 5-7
Subject 5-7-0
Preconditioned Airflow Requirements R UPDATED REQUIREMENTS FORPRECONDITIONED AIRFLOW AT THEGROUND CONNECTION.
HIGHLIGHTSPage 12
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Preconditioned AirflowRequirements
R
Section 5-8
Subject 5-8-0
Ground Towing Requirements R
Section 5-9 N
Subject 5-9-0 N
De-Icing and External Cleaning N
CHAPTER 7
Section 7-1
Subject 7-1-0
General Information R TEXT UPDATED
Section 7-2
Subject 7-2-0
Landing Gear Footprint R ILLUSTRATIONS UPDATED
FIGURE Landing Gear Footprint R ILLUSTRATION REVISED
FIGURE Landing Gear Footprint R
FIGURE Landing Gear Footprint R ILLUSTRATION REVISED
Section 7-3
Subject 7-3-0
Maximum Pavement Loads R ILLUSTRATIONS UPDATED
FIGURE Maximum Pavement Loads R ILLUSTRATION REVISED
FIGURE Maximum Pavement Loads R
FIGURE Maximum Pavement Loads R ILLUSTRATION REVISED
Section 7-4 R
Subject 7-4-0
Landing Gear Loading on Pavement R ILLUSTRATIONS AND EXAMPLEUPDATED.
FIGURE Landing Gear Loading onPavement - WV026, MRW 192 900 kg
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - WV001, MRW 227 900 kg
N ILLUSTRATION ADDED
HIGHLIGHTSPage 13
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FIGURE Landing Gear Loading onPavement - WV001, MRW 184 900 kg
N ILLUSTRATION ADDED
Subject 07-04-01 D
Section 7-5 R
Subject 7-5-0
Flexible Pavement Requirements - USArmy Corps of Engineers Design MethodS-77-1
R ILLUSTRATIONS AND EXAMPLEUPDATED.DESCRIPTION TITLE UPDATED
FIGURE Flexible Pavement Requirements- WV026, MRW 192 900 kg, CG 38.8 %
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- WV001, MRW 227 900 kg, CG 37.6 %
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- WV001, MRW 184 900 kg, CG 40.1 %
N ILLUSTRATION ADDED
Subject 07-05-01 D
Section 7-6 R
Subject 7-6-0
Flexible Pavement Requirements - LCNConversion
R TEXT, ILLUSTRATIONS AND EXAMPLEUPDATED.
FIGURE Flexible Pavement Requirements- LCN table
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN - WV026, MRW 192 900 kg, CG38.8 %
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN table
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN - WV001, MRW 227 900 kg, CG37.6 %
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN table
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN - WV001, MRW 184 900 kg, CG40.1 %
N ILLUSTRATION ADDED
Subject 07-06-01 D
HIGHLIGHTSPage 14
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Section 7-7 R
Subject 7-7-0
Rigid Pavement Requirements - PortlandCement Association Design Method
R TEXT, ILLUSTRATIONS AND EXAMPLEUPDATED.NOTE AMENDED
FIGURE Rigid Pavement Requirements -WV026, MRW 192 900 kg, CG 38.8 %
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -WV001, MRW 227 900 kg, CG 37.6 %
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -WV001, MRW 184 900 kg, CG 40.1 %
N ILLUSTRATION ADDED
Subject 07-07-01 D
Section 7-8 R
Subject 7-8-0
Rigid Pavement Requirements - LCNConversion
R TEXT, ILLUSTRATIONS AND EXAMPLEUPDATED.
FIGURE Rigid Pavement Requirements -LCN table
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN table
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN table
N ILLUSTRATION ADDED
FIGURE Radius of Relative Stiffness (L) N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN - WV026, MRW 192 900 kg, CG38.8 %
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN - WV001, MRW 227 900 kg, CG37.6 %
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN - WV001, MRW 184 900 kg, CG40.1 %
N ILLUSTRATION ADDED
FIGURE Radius of Relative Stiffness(Effect E and µ ON ”L” values)
N ILLUSTRATION ADDED
Subject 07-08-01 D
HIGHLIGHTSPage 15
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Subject 07-08-02 D
Subject 07-08-03 D
Subject 07-08-04 D
Section 7-9 R
Subject 7-9-0
Aircraft Classification Number - Flexibleand Rigid Pavement
R TEXT, ILLUSTRATIONS AND EXAMPLEUPDATED.DESCRIPTION TITLE UPDATEDNOTE AMENDED
FIGURE Aircraft Classification Number -ACN Table
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - WV026, MRW 192900 kg, CG 38.8 %
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - WV058, MRW 238900 kg, CG 31.3 %
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -ACN Table
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - WV001, MRW 227900 kg, CG 37.6 %
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - WV000, MRW 233900 kg, CG 37.4 %
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -ACN Table
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - WV001, MRW 184900 kg, CG 40.1 %
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - WV054, MRW 235900 kg, CG 35.7 %
N ILLUSTRATION ADDED
Subject 07-09-01 D
Subject 07-09-02 D
HIGHLIGHTSPage 16
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DESCRIPTIONS OF CHANGE
CHAPTER 8 R
Section 8-0 N
Subject 8-0-0 N
Scaled Drawings N
FIGURE Scaled Drawing N ILLUSTRATION ADDED
FIGURE Scaled Drawing N ILLUSTRATION ADDED
FIGURE Scaled Drawing N ILLUSTRATION ADDED
Section 08-01 D
CHAPTER 10 N
Section 10-0 N
Subject 10-0-0 N
Aircraft Rescue and Fire Fighting N
FIGURE Front Page N ILLUSTRATION ADDED
FIGURE Highly Flammable and HazardousMaterials and Components
N ILLUSTRATION ADDED
FIGURE Crew Rest CompartmentsLocation
N ILLUSTRATION ADDED
FIGURE Wheel/Brake Overheat - WheelSafety Area
N ILLUSTRATION ADDED
FIGURE Composite Materials Location N ILLUSTRATION ADDED
FIGURE Ground Lock Safety Devices N ILLUSTRATION ADDED
FIGURE Emergency Evacuation Devices N ILLUSTRATION ADDED
FIGURE Pax/Crew Doors and EmergencyExits
N ILLUSTRATION ADDED
FIGURE FWD and AFT Lower DeckCargo Doors
N ILLUSTRATION ADDED
FIGURE Control Panels N ILLUSTRATION ADDED
FIGURE APU Compartment Access N ILLUSTRATION ADDED
FIGURE Ground Clearances N ILLUSTRATION ADDED
FIGURE Structural Break-in Points N ILLUSTRATION ADDED
Aircraft Rescue and Fire Fighting N
FIGURE Front Page N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Highly Flammable and HazardousMaterials and Components
N ILLUSTRATION ADDED
FIGURE Wheel/Brake Overheat - WheelSafety Area
N ILLUSTRATION ADDED
FIGURE Composite Materials Location N ILLUSTRATION ADDED
FIGURE Ground Lock Safety Devices N ILLUSTRATION ADDED
FIGURE Emergency Evacuation Devices N ILLUSTRATION ADDED
FIGURE Crew Doors and Emergency Exits N ILLUSTRATION ADDED
FIGURE Cargo Doors - FWD and AFTLower Deck Compartments
N ILLUSTRATION ADDED
FIGURE Control Panels N ILLUSTRATION ADDED
FIGURE APU Compartment Access N ILLUSTRATION ADDED
FIGURE Ground Clearances N ILLUSTRATION ADDED
FIGURE Structural Break-in Points N ILLUSTRATION ADDED
HIGHLIGHTSPage 18
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 21 - Apr 01/13
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 1
Subject 1-1-0
Purpose R Apr 01/13
Subject 1-2-1
Glossary N Apr 01/13
CHAPTER 2
Subject 2-1-1
General Aircraft Characteristics Data R Apr 01/13
General Aircraft Characteristics Data R Apr 01/13
Subject 2-2-0
General Aircraft Dimensions R Apr 01/13
FIGURE General Aircraft Dimensions R Apr 01/13
FIGURE General Aircraft Dimensions - (Pre Mod 48979) R Apr 01/13
General Aircraft Dimensions R Apr 01/13
FIGURE General Aircraft Dimensions R Apr 01/13
Subject 2-3-0
Ground Clearances R Apr 01/13
FIGURE Ground Clearances R Apr 01/13
FIGURE Ground Clearances N Apr 01/13
FIGURE Ground Clearances N Apr 01/13
FIGURE Ground Clearances - Ailerons Up N Apr 01/13
FIGURE Ground Clearances - Ailerons Down N Apr 01/13
FIGURE Ground Clearances - Spoilers Extended N Apr 01/13
FIGURE Ground Clearances - Slats Fully Extended N Apr 01/13
FIGURE Ground Clearances - Flaps Fully Extended N Apr 01/13
FIGURE Ground Clearances - Flaps-Tracks Fully Extended N Apr 01/13
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Apr 01/13
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Subject 2-4-1
Interior Arrangements - Plan View R Apr 01/13
FIGURE Interior Arrangements - Plan View - Typical Configuration R Apr 01/13
FIGURE Interior Arrangements - Plan View - Typical Configuration R Apr 01/13
Subject 2-5-0
Interior Arrangements - Cross Section R Apr 01/13
FIGURE Interior Arrangements - Cross Section - TypicalConfiguration
R Apr 01/13
Subject 2-6-1
Lower Deck Cargo Compartments R Apr 01/13
FIGURE Lower Deck Cargo Compartments - Location and Dimensions R Apr 01/13
FIGURE Lower Deck Cargo Compartments - Loading Combinations R Apr 01/13
FIGURE Lower Deck Cargo Compartments - Loading Combinations N Apr 01/13
Subject 2-6-2
Main Deck Cargo Compartment R Apr 01/13
FIGURE Main Deck Cargo Compartment - Location and Dimensions N Apr 01/13
FIGURE Main Deck Cargo Compartment - Loading Combinations R Apr 01/13
FIGURE Main Deck Cargo Compartment - Loading Combinations R Apr 01/13
FIGURE Main Deck Cargo Compartment - Loading Combinations R Apr 01/13
FIGURE Main Deck Cargo Compartment - Loading Combinations R Apr 01/13
Subject 2-6-3
Main and Lower Deck Cross-sections Feb 01/09
FIGURE Main and Lower Deck Cross-sections Jan 01/12
Subject 2-7-0
Door Clearances R Apr 01/13
FIGURE Door Identification and location - Door Identification N Apr 01/13
FIGURE Door Identification and Location - Door Identification N Apr 01/13
FIGURE Door Identification and Location - Door Identification N Apr 01/13
Subject 2-7-1
L.E.C.Page 2
Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
Forward Passenger / Crew Door Feb 01/09
FIGURE Forward Passenger / Crew Doors May 01/07
FIGURE Forward Passenger / Crew Doors Feb 01/09
Subject 2-7-2
Mid Passenger / Crew Door May 01/07
FIGURE Mid Passenger / Crew Door May 01/07
Subject 2-7-3
Emergency Exits May 01/07
FIGURE Emergency Exits May 01/07
Subject 2-7-4
Aft Passenger / Crew Doors May 01/07
FIGURE Aft Passenger / Crew Doors May 01/07
Subject 2-7-5
Forward Cargo Compartment Doors May 01/07
FIGURE Forward Cargo Compartment Doors May 01/07
Forward Cargo Compartment Doors Feb 01/09
FIGURE Forward Cargo Compartment Doors Feb 01/09
FIGURE Forward Cargo Compartment Doors Feb 01/09
Subject 2-7-6
Aft Cargo Compartment Doors Feb 01/09
FIGURE Aft Cargo Compartment Doors Feb 01/09
FIGURE Aft Cargo Compartment Doors Feb 01/09
FIGURE Aft Cargo Compartment Doors Feb 01/09
Subject 2-7-7
Bulk Cargo Compartment Doors May 01/07
FIGURE Bulk Cargo Compartment Doors May 01/07
Bulk Cargo Compartment Doors Feb 01/09
FIGURE Bulk Cargo Compartment Doors Feb 01/09
Subject 2-7-8
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Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
Main Landing Gear Doors May 01/07
FIGURE Main Landing Gear Doors May 01/07
Main Landing Gear Doors Feb 01/09
FIGURE Main Landing Gear Doors Feb 01/09
Subject 2-7-9
Radome Feb 01/09
FIGURE Radome Feb 01/09
Subject 2-7-10
APU and Nose Landing Gear Doors May 01/07
FIGURE APU and Nose Landing Gear Doors May 01/07
APU and Nose Landing Gear Doors Feb 01/09
FIGURE APU and Nose Landing Gear Doors Feb 01/09
Subject 2-8-0
Escape Slides N Apr 01/13
FIGURE Escape Slides - Location N Apr 01/13
FIGURE Escape Slides - Location N Apr 01/13
FIGURE Escape Slides - Location N Apr 01/13
Subject 2-9-0
Landing Gear Maintenance Pits N Apr 01/13
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes N Apr 01/13
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes N Apr 01/13
Landing Gear N Apr 01/13
FIGURE Main Landing Gear - General N Apr 01/13
FIGURE Nose Landing Gear - General N Apr 01/13
Subject 2-10-0
Exterior Lighting N Apr 01/13
FIGURE Exterior Lighting N Apr 01/13
FIGURE Exterior Lighting N Apr 01/13
FIGURE Exterior Lighting N Apr 01/13
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CONTENT CHGCODE
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Subject 2-11-0
Antennas and Probes Location N Apr 01/13
FIGURE Antennas and Probes - Location N Apr 01/13
FIGURE Antennas and Probes - Location N Apr 01/13
FIGURE Antennas and Probes - Location N Apr 01/13
Subject 2-12-0
Engine and Nacelle N Apr 01/13
FIGURE Engine and Nacelle - Engine Dimensions - PW 4000 N Apr 01/13
FIGURE Engine and Nacelle - Nacelle Dimensions - PW 4000 N Apr 01/13
FIGURE Engine and Nacelle - Fan Cowls - PW 4000 N Apr 01/13
FIGURE Engine and Nacelle - Thrust Reverser Cowls - PW 4000 N Apr 01/13
FIGURE Engine and Nacelle - Engine Dimensions - TRENT 700 N Apr 01/13
FIGURE Engine and Nacelle - Nacelle Dimensions - TRENT 700 N Apr 01/13
FIGURE Engine and Nacelle - Fan Cowls - TRENT 700 N Apr 01/13
FIGURE Engine and Nacelle - Thrust Reverser Cowls - TRENT 700 N Apr 01/13
FIGURE Engine and Nacelle - Engine Dimensions - GE CF6-80E1 N Apr 01/13
FIGURE Engine and Nacelle - Nacelle Dimensions - GE CF6-80E1 N Apr 01/13
FIGURE Engine and Nacelle - Fan Cowls - GE CF6-80E1 N Apr 01/13
FIGURE Engine and Nacelle - Thrust Reverser Cowls - GE CF6-80E1 N Apr 01/13
Subject 2-12-1
Auxiliary Power Unit N Apr 01/13
FIGURE Auxiliary Power Unit - Access Doors N Apr 01/13
Subject 2-13-0
Leveling, Symmetry and Alignment N Apr 01/13
FIGURE Location of Leveling Points N Apr 01/13
FIGURE Location of Leveling Points N Apr 01/13
FIGURE Location of Leveling Points N Apr 01/13
Subject 2-14-0
Jacking for Maintenance N Apr 01/13
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Apr 01/13
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CONTENT CHGCODE
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FIGURE Jacking for Maintenance - Jacking Points Location N Apr 01/13
FIGURE Jacking for Maintenance - Jacking Points Location N Apr 01/13
FIGURE Jacking for Maintenance - Jacking Points Location N Apr 01/13
FIGURE Jacking for Maintenance - Forward Jacking Point N Apr 01/13
FIGURE Jacking for Maintenance - Forward Jacking Point N Apr 01/13
FIGURE Jacking for Maintenance - Wing Jacking Points N Apr 01/13
FIGURE Jacking for Maintenance - Wing Jacking Points N Apr 01/13
FIGURE Jacking for Maintenance - Auxiliary Jacking Point - SafetyStay
N Apr 01/13
FIGURE Jacking for Maintenance - Auxiliary Jacking Point - SafetyStay
N Apr 01/13
FIGURE Jacking for Maintenance - Auxiliary Jacking Point - SafetyStay
N Apr 01/13
FIGURE Jacking for Maintenance - Specific Jack-Nose Dimensions N Apr 01/13
FIGURE Jacking for Maintenance - Jacking Dimensions N Apr 01/13
FIGURE Jacking for Maintenance - Jacking Dimensions N Apr 01/13
FIGURE Jacking for Maintenance - Jacking Dimensions N Apr 01/13
FIGURE Jacking for Maintenance - Load at the Aircraft JackingPoints
N Apr 01/13
FIGURE Jacking for Maintenance - Load at the Aircraft JackingPoints
N Apr 01/13
Subject 2-14-1
Jacking for Wheel Change N Apr 01/13
FIGURE Jacking for Wheel Change - MLG Jacking Point Heights N Apr 01/13
FIGURE Jacking for Wheel Change - Jacking of the NLG N Apr 01/13
FIGURE Jacking for Wheel Change - MLG Jacking Point Loads N Apr 01/13
FIGURE Jacking for Wheel Change - MLG Jacking Point Loads N Apr 01/13
FIGURE Jacking for Wheel Change - NLG Jacking Point Loads N Apr 01/13
FIGURE Jacking for Wheel Change - NLG Jacking Point Loads N Apr 01/13
Subject 2-14-2
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CONTENT CHGCODE
LAST REVISIONDATE
Support of Aircraft N Apr 01/13
FIGURE Support of Aircraft - Location of Shoring Cradles N Apr 01/13
FIGURE Support of Aircraft - Location of Shoring Cradles N Apr 01/13
FIGURE Support of Aircraft - Location of Shoring Cradles N Apr 01/13
CHAPTER 3
Subject 3-1-0
General Information Jan 01/10
Subject 3-2-0
Payload / Range Feb 01/09
Subject 3-2-1
ISA Conditions May 01/07
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - GE CF6-80E1 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - GE CF6-80E1 Series Engine Feb 01/09
ISA Conditions Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
Subject 3-3-0
FAR / JAR Takeoff Weight Limitation Feb 01/09
Subject 3-3-1
FAR / JAR Takeoff Weight Limitation Feb 01/09
FIGURE Takeoff Weight Limitation - ISA Conditions - PW 4000Series Engine
Feb 01/09
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Takeoff Weight Limitation - ISA Conditions - RR TRENT700 Series Engine
Feb 01/09
FIGURE Takeoff Weight Limitation - ISA Conditions - GE CF6-80E1Series Engine
Feb 01/09
Subject 3-3-2
ISA +15 ˚C (ISA +27 ˚F) Conditions Jan 01/10
FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15˚C (ISA+27˚F) Conditions - PW 4000 Series Engine
Jan 01/10
FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15˚C (ISA+27˚F) Conditions - RR TRENT 700 Series Engine
Jan 01/10
FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15˚C (ISA+27˚F) Conditions - GE CF6-80E1 Series Engine
Jan 01/10
Subject 3-4-0
Landing Field Length Feb 01/09
Subject 3-4-1
ISA Conditions All series engine Jan 01/10
FIGURE FAR / JAR Landing Field Length - ISA Conditions - PW4000 Series Engine
Jan 01/10
FIGURE FAR / JAR Landing Field Length - ISA Conditions - RRTRENT 700 Series Engine
Jan 01/10
FIGURE FAR / JAR Landing Field Length - ISA Conditions - GECF6-80E1 Series Engine
Jan 01/10
Subject 3-5-0
Final Approach Speed R Apr 01/13
CHAPTER 4
Subject 4-1-0
General Information Feb 01/09
Subject 4-2-0
Turning Radii Feb 01/09
FIGURE Turning Radii - (Sheet 1) R Apr 01/13
FIGURE Turning Radii - (Sheet 2) R Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Turning Radii - (Sheet 2) R Apr 01/13
Subject 4-3-0
Minimum Turning Radii Jan 01/11
FIGURE Minimum Turning Radii R Apr 01/13
FIGURE Minimum Turning Radii R Apr 01/13
Subject 4-4-0
Visibility from Cockpit in Static Position. R Apr 01/13
FIGURE Visibility from Cockpit in Static Position R Apr 01/13
FIGURE Visibility from Cockpit in Static Position R Apr 01/13
FIGURE Binocular Visibility Through Windows from Captain EyePosition
N Apr 01/13
Subject 4-5-0
Runway and Taxiway Turn Paths Jan 01/10
Subject 4-5-1
135˚ Turn - Runway to Taxiway Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
Subject 4-5-2
90˚ Turn - Runway to Taxiway Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
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Subject 4-5-3
180˚ Turn on a Runway Jan 01/11
FIGURE 180˚ Turn on a Runway R Apr 01/13
FIGURE 180˚ Turn on a Runway R Apr 01/13
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway Jan 01/11
FIGURE 135˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
FIGURE 135˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/11
Subject 4-6-0
Runway Holding Bay (Apron) Jan 01/11
FIGURE Runway Holding Bay (Apron) Jan 01/11
Subject 4-7-0
Airplane Parking Feb 01/09
FIGURE Airplane Parking - Steering Geometry May 01/07
FIGURE Airplane Parking - Steering Geometry May 01/07
FIGURE Airplane Parking - Minimum Parking Space Requirements May 01/07
L.E.C.Page 10
Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Airplane Parking - Steering Geometry Feb 01/09
FIGURE Airplane Parking - Steering Geometry Feb 01/09
FIGURE Airplane Parking - Minimum Parking Space Requirements Feb 01/09
CHAPTER 5
Subject 5-0-0
TERMINAL SERVICING Jan 01/10
Subject 5-1-0
Airplane Servicing Arrangements Jan 01/10
Airplane Servicing Arrangements Jan 01/10
Subject 5-1-1
Symbols Used on Servicing Diagrams R Apr 01/13
Subject 5-1-2
Typical Ramp Layout - Open Apron R Apr 01/13
FIGURE Typical Ramp Layout - Open Apron R Apr 01/13
FIGURE Typical Ramp Layout - Open Apron R Apr 01/13
Typical Ramp Layout - Open Apron R Apr 01/13
FIGURE Typical Ramp Layout - Open Apron R Apr 01/13
Subject 5-1-3
Typical Ramp Layout - Gate R Apr 01/13
FIGURE Typical Ramp Layout - Gate R Apr 01/13
FIGURE Typical Ramp Layout - Gate R Apr 01/13
Subject 5-2-0
Terminal Operations -- Full Servicing Turn-Round Time R Apr 01/13
FIGURE Full Servicing Turn-Round Time Chart N Apr 01/13
Terminal Operations -- Full Servicing Turn-Round Time N Apr 01/13
FIGURE Full Servicing Turn-Round Time Chart N Apr 01/13
Terminal Operations - Full Servicing Turn-Round Time N Apr 01/13
FIGURE Full Servicing Turn-Round Time Chart N Apr 01/13
Subject 5-3-0
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Terminal Operations - Minimum Servicing Turn-Round Time R Apr 01/13
FIGURE Minimum Servicing Turn-Round Time N Apr 01/13
Terminal Operations - Minimum Servicing Turn-Round Time N Apr 01/13
FIGURE Minimum Servicing Turn-Round Time N Apr 01/13
Subject 5-4-1
Ground Service Connections Layout R Apr 01/13
FIGURE Ground Service Connections Layout R Apr 01/13
Ground Service Connections Layout R Apr 01/13
FIGURE Ground Service Connections Layout R Apr 01/13
Subject 5-4-2
Grounding Points Feb 01/09
FIGURE Ground Service Connections - Grounding Points Feb 01/09
FIGURE Ground Service Connections - Grounding Points Feb 01/09
Subject 5-4-3
Hydraulic System R Apr 01/13
FIGURE Ground Service Connections - Green System Ground ServicePanel
N Apr 01/13
FIGURE Ground Service Connections - Blue System Ground ServicePanel
N Apr 01/13
FIGURE Ground Service Connections - Yellow System Ground ServicePanel
N Apr 01/13
Subject 5-4-4
Electrical System R Apr 01/13
FIGURE Ground Service Connections - Electrical Service Panel N Apr 01/13
FIGURE Ground Service Connections - Electrical Service Panel N Apr 01/13
Subject 5-4-5
Oxygen System R Apr 01/13
FIGURE Ground Service Connections - Oxygen System N Apr 01/13
FIGURE Ground Service Connections - Oxygen System N Apr 01/13
Subject 5-4-6
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CONTENT CHGCODE
LAST REVISIONDATE
Fuel System R Apr 01/13
FIGURE Overpressure Protector and NACA Flame Arrestor Jan 01/12
Subject 5-4-7
Pneumatic System R Apr 01/13
FIGURE Ground Service Connections - LP and HP GroundConnectors
N Apr 01/13
Subject 5-4-8
Potable Water System R Apr 01/13
FIGURE Ground Service Connections - Potable-Water Ground ServicePanels
N Apr 01/13
Potable Water System N Apr 01/13
FIGURE Ground Service Connections - Potable-Water Ground ServicePanels
N Apr 01/13
Potable Water System N Apr 01/13
FIGURE Ground Service Connections - Potable-Water Ground ServicePanel
N Apr 01/13
Subject 5-4-9
Oil System Feb 01/09
FIGURE Ground Service Connections - Engine Oil Tank - PW 4000series engine
Feb 01/09
FIGURE Ground Service Connections - Engine Oil Tank - RR Trent700 series engine
Feb 01/09
FIGURE Ground Service Connections - Engine Oil Tank - GECF6-80E1 series engine
May 01/07
FIGURE Ground Service Connections - IDG Oil Tank - PW 4000series engine
Feb 01/09
FIGURE Ground Service Connections - IDG Oil Tank - RR Trent 700series engine
Feb 01/09
FIGURE Ground Service Connections - IDG Oil Tank - GE CF6-80E1series engine
May 01/07
APU Oil System R Apr 01/13
FIGURE Ground Service Connections - APU Oil Servicing R Apr 01/13
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Subject 5-4-10
Vacuum Toilet System R Apr 01/13
FIGURE Ground Service Connections - Waste Water Ground ServicePanel
N Apr 01/13
FIGURE Ground Service Connections - Waste Water Ground ServicePanel
N Apr 01/13
Subject 5-5-0
Engine Starting Pneumatic Requirements R Apr 01/13
FIGURE Example for Use of the Charts R Apr 01/13
FIGURE Engine Starting Pneumatic Requirements - GE CF6-80E1Series Engine
N Apr 01/13
FIGURE Engine Starting Pneumatic Requirements - Rolls Royce Trent700 Series Engine
N Apr 01/13
FIGURE Engine Starting Pneumatic Requirements - Pratt & WhitneyPW4000 Series Engine
N Apr 01/13
Subject 5-6-0
Ground Pneumatic Power Requirements R Apr 01/13
FIGURE Ground Pneumatic Power Requirements - Heating N Apr 01/13
FIGURE Ground Pneumatic Power Requirements - Cooling N Apr 01/13
Subject 5-7-0
Preconditioned Airflow Requirements R Apr 01/13
FIGURE Preconditioned Airflow Requirements R Apr 01/13
Subject 5-8-0
Ground Towing Requirements R Apr 01/13
FIGURE Ground Towing Requirements Jan 01/11
Subject 5-9-0
De-Icing and External Cleaning N Apr 01/13
CHAPTER 6
Subject 6-1-0
Engine Exhaust Velocities and Temperatures Jan 01/10
Subject 6-1-1
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CONTENT CHGCODE
LAST REVISIONDATE
Engine Exhaust Velocities Contours - Ground Idle Power Feb 01/09
FIGURE Engine Exhaust Velocities - Ground Idle Power - PW 4000series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Ground Idle Power - RR Trent700 series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Ground Idle Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power Jan 01/10
FIGURE Engine Exhaust Temperatures - Ground Idle Power - PW4000 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Ground Idle Power - RRTrent 700 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Ground Idle Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-3
Engine Exhaust Velocities Contours - Breakaway Power Feb 01/09
FIGURE Engine Exhaust Velocities - Breakaway Power - PW 4000series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Breakaway Power - RR Trent700 series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Breakaway Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power Jan 01/10
FIGURE Engine Exhaust Temperatures - Breakaway Power - PW4000 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Breakaway Power - RRTrent 700 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Breakaway Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-5
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CONTENT CHGCODE
LAST REVISIONDATE
Engine Exhaust Velocities Contours - Takeoff Power Feb 01/09
FIGURE Engine Exhaust Velocities - Takeoff Power - PW 4000 seriesengine
Feb 01/09
FIGURE Engine Exhaust Velocities - Takeoff Power - RR Trent 700series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Takeoff Power - GE CF6-80E1series engine
May 01/07
Subject 6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power Feb 01/09
FIGURE Engine Exhaust Temperatures - Takeoff Power - PW 4000series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Takeoff Power - RR Trent700 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Takeoff Power - GECF6-80E1 series engine
May 01/07
Subject 6-2-0
Airport and Community Noise Data Feb 01/09
Subject 6-2-1
Noise Data Feb 01/09
FIGURE Airport and Community Noise - PW 4000 series engine Feb 01/09
FIGURE Airport and Community Noise - RR Trent 700 series engine Feb 01/09
FIGURE Airport and Community Noise - GE CF6-80E1 series engine May 01/07
Subject 6-3-0
Danger Areas of Engines Jan 01/10
Subject 6-3-1
Ground Idle Power Feb 01/09
FIGURE Danger Areas of Engines - PW 4000 series engine Feb 01/09
FIGURE Danger Areas of Engines - RR Trent 700 series engine Feb 01/09
FIGURE Danger Areas of Engines - GE CF6-80E1 series engine May 01/07
Subject 6-3-2
Breakaway Power Feb 01/09
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Danger Areas of Engines - PW 4000 series engine Feb 01/09
FIGURE Danger Areas of Engines - RR Trent 700 series engine Feb 01/09
FIGURE Danger Areas of Engines - GE CF6-80E1 series engine May 01/07
Subject 6-3-3
Takeoff Power Feb 01/09
FIGURE Danger Areas of Engines - PW 4000 series engine Feb 01/09
FIGURE Danger Areas of Engines - RR Trent 700 series engine Feb 01/09
FIGURE Danger Areas of Engines - GE CF6-80E1 series engine May 01/07
Subject 6-4-0
APU Exhaust Velocities and Temperatures Jan 01/10
Subject 6-4-1
APU - GARRETT Feb 01/09
FIGURE Exhaust Velocities and Temperatures - APU -- GARRETTGTCP 331-350
Feb 01/09
CHAPTER 7
Subject 7-1-0
General Information R Apr 01/13
Subject 7-2-0
Landing Gear Footprint R Apr 01/13
FIGURE Landing Gear Footprint R Apr 01/13
FIGURE Landing Gear Footprint R Apr 01/13
FIGURE Landing Gear Footprint R Apr 01/13
Subject 7-3-0
Maximum Pavement Loads R Apr 01/13
FIGURE Maximum Pavement Loads R Apr 01/13
FIGURE Maximum Pavement Loads R Apr 01/13
FIGURE Maximum Pavement Loads R Apr 01/13
Subject 7-4-0
Landing Gear Loading on Pavement R Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Loading on Pavement - WV026, MRW 192900 kg
N Apr 01/13
FIGURE Landing Gear Loading on Pavement - WV001, MRW 227900 kg
N Apr 01/13
FIGURE Landing Gear Loading on Pavement - WV001, MRW 184900 kg
N Apr 01/13
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method S-77-1
R Apr 01/13
FIGURE Flexible Pavement Requirements - WV026, MRW 192 900kg, CG 38.8 %
N Apr 01/13
FIGURE Flexible Pavement Requirements - WV001, MRW 227 900kg, CG 37.6 %
N Apr 01/13
FIGURE Flexible Pavement Requirements - WV001, MRW 184 900kg, CG 40.1 %
N Apr 01/13
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion R Apr 01/13
FIGURE Flexible Pavement Requirements - LCN table N Apr 01/13
FIGURE Flexible Pavement Requirements - LCN - WV026, MRW 192900 kg, CG 38.8 %
N Apr 01/13
FIGURE Flexible Pavement Requirements - LCN table N Apr 01/13
FIGURE Flexible Pavement Requirements - LCN - WV001, MRW 227900 kg, CG 37.6 %
N Apr 01/13
FIGURE Flexible Pavement Requirements - LCN table N Apr 01/13
FIGURE Flexible Pavement Requirements - LCN - WV001, MRW 184900 kg, CG 40.1 %
N Apr 01/13
Subject 7-7-0
Rigid Pavement Requirements - Portland Cement Association DesignMethod
R Apr 01/13
FIGURE Rigid Pavement Requirements - WV026, MRW 192 900 kg,CG 38.8 %
N Apr 01/13
FIGURE Rigid Pavement Requirements - WV001, MRW 227 900 kg,CG 37.6 %
N Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements - WV001, MRW 184 900 kg,CG 40.1 %
N Apr 01/13
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion R Apr 01/13
FIGURE Rigid Pavement Requirements - LCN table N Apr 01/13
FIGURE Rigid Pavement Requirements - LCN table N Apr 01/13
FIGURE Rigid Pavement Requirements - LCN table N Apr 01/13
FIGURE Radius of Relative Stiffness (L) N Apr 01/13
FIGURE Rigid Pavement Requirements - LCN - WV026, MRW 192900 kg, CG 38.8 %
N Apr 01/13
FIGURE Rigid Pavement Requirements - LCN - WV001, MRW 227900 kg, CG 37.6 %
N Apr 01/13
FIGURE Rigid Pavement Requirements - LCN - WV001, MRW 184900 kg, CG 40.1 %
N Apr 01/13
FIGURE Radius of Relative Stiffness (Effect E and µ ON ”L” values) N Apr 01/13
Subject 7-9-0
Aircraft Classification Number - Flexible and Rigid Pavement R Apr 01/13
FIGURE Aircraft Classification Number - ACN Table N Apr 01/13
FIGURE Aircraft Classification Number - Flexible Pavement - WV026,MRW 192 900 kg, CG 38.8 %
N Apr 01/13
FIGURE Aircraft Classification Number - Flexible Pavement - WV058,MRW 238 900 kg, CG 31.3 %
N Apr 01/13
FIGURE Aircraft Classification Number - ACN Table N Apr 01/13
FIGURE Aircraft Classification Number - Flexible Pavement - WV001,MRW 227 900 kg, CG 37.6 %
N Apr 01/13
FIGURE Aircraft Classification Number - Flexible Pavement - WV000,MRW 233 900 kg, CG 37.4 %
N Apr 01/13
FIGURE Aircraft Classification Number - ACN Table N Apr 01/13
FIGURE Aircraft Classification Number - Flexible Pavement - WV001,MRW 184 900 kg, CG 40.1 %
N Apr 01/13
FIGURE Aircraft Classification Number - Flexible Pavement - WV054,MRW 235 900 kg, CG 35.7 %
N Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 8
Subject 8-0-0
Scaled Drawings N Apr 01/13
FIGURE Scaled Drawing N Apr 01/13
FIGURE Scaled Drawing N Apr 01/13
FIGURE Scaled Drawing N Apr 01/13
CHAPTER 10
Subject 10-0-0
Aircraft Rescue and Fire Fighting N Apr 01/13
FIGURE Front Page N Apr 01/13
FIGURE Highly Flammable and Hazardous Materials and Components N Apr 01/13
FIGURE Crew Rest Compartments Location N Apr 01/13
FIGURE Wheel/Brake Overheat - Wheel Safety Area N Apr 01/13
FIGURE Composite Materials Location N Apr 01/13
FIGURE Ground Lock Safety Devices N Apr 01/13
FIGURE Emergency Evacuation Devices N Apr 01/13
FIGURE Pax/Crew Doors and Emergency Exits N Apr 01/13
FIGURE FWD and AFT Lower Deck Cargo Doors N Apr 01/13
FIGURE Control Panels N Apr 01/13
FIGURE APU Compartment Access N Apr 01/13
FIGURE Ground Clearances N Apr 01/13
FIGURE Structural Break-in Points N Apr 01/13
Aircraft Rescue and Fire Fighting N Apr 01/13
FIGURE Front Page N Apr 01/13
FIGURE Highly Flammable and Hazardous Materials and Components N Apr 01/13
FIGURE Wheel/Brake Overheat - Wheel Safety Area N Apr 01/13
FIGURE Composite Materials Location N Apr 01/13
FIGURE Ground Lock Safety Devices N Apr 01/13
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Emergency Evacuation Devices N Apr 01/13
FIGURE Crew Doors and Emergency Exits N Apr 01/13
FIGURE Cargo Doors - FWD and AFT Lower Deck Compartments N Apr 01/13
FIGURE Control Panels N Apr 01/13
FIGURE APU Compartment Access N Apr 01/13
FIGURE Ground Clearances N Apr 01/13
FIGURE Structural Break-in Points N Apr 01/13
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TABLE OF CONTENTS
1 SCOPE
1-1-0 Purpose
1-2-1 Glossary
2 AIRCRAFT DESCRIPTION
2-1-1 General Aircraft Characteristics Data
2-2-0 General Aircraft Dimensions
2-3-0 Ground Clearances
2-4-1 Interior Arrangements - Plan View
2-5-0 Interior Arrangements - Cross Section
2-6-1 Lower Deck Cargo Compartments
2-6-2 Main Deck Cargo Compartments
2-6-3 Main and Lower Deck Cross-sections
2-7-0 Door Clearances
2-7-1 Forward Passenger / Crew Doors
2-7-2 Mid Passenger / Crew Doors
2-7-3 Emergency Exits
2-7-4 Aft Passenger / Crew Doors
2-7-5 Forward Cargo Compartment Doors
2-7-6 Aft Cargo Compartment Doors
2-7-7 Bulk Cargo Compartment Doors
2-7-8 Main and Center Landing Gear Doors
2-7-9 Radome
2-7-10 APU and Nose Landing Gear Doors
2-8-0 Escape Slides
2-9-0 Landing Gear
2-10-0 Exterior Lighting
2-11-0 Antennas and Probes Location
2-12-0 Engine and Nacelle
2-12-1 Auxiliary Power Unit
2-13-0 Levelling, symmetry and Alignment
2-14-0 Jacking for Maintenance
2-14-1 Jacking for Wheel Change
2-14-2 Support of Aircraft
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3 AIRCRAFT PERFORMANCE
3-1-0 General Information
3-2-0 Payload / Range
3-2-1 ISA Conditions
3-3-0 FAR / JAR Takeoff Weight Limitation
3-3-1 ISA Conditions
3-3-2 ISA +15˚C (ISA +27˚F) Conditions
3-4-0 FAR / JAR Landing Field Length
3-4-1 ISA Conditions All series engines
3-5-0 Final Approach Speed
4 GROUND MANEUVERING
4-1-0 General Information
4-2-0 Turning Radii
4-3-0 Minimum Turning Radii
4-4-0 Visibility from Cockpit in Static Position
4-5-0 Runway and Taxiway Turn Paths
4-5-1 135˚ Turn - Runway to Taxiway
4-5-2 90˚ Turn - Runway to Taxiway
4-5-3 180˚ Turn on a Runway
4-5-4 135˚ Turn - Taxiway to Taxiway
4-5-5 90˚ Turn - Taxiway to Taxiway
4-6-0 Runway Holding Bay (Apron)
4-7-0 Aircraft Parking
5 TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
5-1-0 Aircraft Servicing Arrangements
5-1-1 Symbols Used on Servicing Diagrams
5-1-2 Typical Ramp Layout - Open Apron
5-1-3 Typical Ramp Layout - Gate
5-2-0 Terminal Operations - Full Servicing
5-3-0 Terminal Operations - Transit
5-4-1 Ground Service Connections Layout
5-4-2 Grounding Points
5-4-3 Hydraulic System
5-4-4 Electrical System
5-4-5 Oxygen System
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5-4-6 Fuel System
5-4-7 Pneumatic System
5-4-8 Potable Water System
5-4-9 Oil System
5-4-10 Vacuum Toilet System
5-5-0 Engine Starting Pneumatic Requirements
5-6-0 Ground Pneumatic Power Requirements
5-7-0 Preconditioned Airflow Requirements
5-8-0 Ground Towing Requirements
5-9-0 De-Icing and External Cleaning
6 OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
6-2-0 Airport and Community Noise
6-2-1 Noise Data
6-3-0 Danger Areas of Engines
6-3-1 Ground Idle Power
6-3-2 Breakaway Power
6-3-3 Takeoff Power
6-4-0 APU Exhaust Velocities and Temperatures
6-4-1 APU
7 PAVEMENT DATA
7-1-0 General Information
7-2-0 Landing Gear Footprint
7-3-0 Maximum Pavement Loads
7-4-0 Landing Gear Loading on Pavement
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-6-0 Flexible Pavement Requirements - LCN Conversion
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-0 Rigid Pavement Requirements - LCN Conversion
7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements
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8 SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
10 AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0 Purpose
**ON A/C A330-200 A330-200F A330-300
Purpose
1. GeneralThe A330 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING (AC)manual is issued for the A330-200, A330-200F and A330-300 basic versions to provide necessary datato airport operators, airlines and Maintenance/Repair Organizations (MRO) for airport andmaintenance facilities planning.
This revision is now a merging of the Maintenance Facility Planning (MFP) document and theAirplane Characteristics for Airport Planning (AC). This document has been renamed AircraftCharacteristics - Airport and Maintenance Planning (AC) to reflect this change.Additionally, a chapter 10 ”Aircraft Rescue and Fire Fighting” has been added to the AC. Thischapter contains the illustrations of the Aircraft Rescue and Fire fighting Charts poster and replacesthe PDF document that was available for download.
This document is not customized and must not be used for training purposes.
The A330 Family -- with Passenger, Freighter, VIP and Military Transport/Tanker variants - is one ofthe most widely-used, versatile and economic wide-bodies in service and has nearly 100 operators andcustomers flying to more than 300 airports every week.
The A330-200 and A330-300 offer several payload capabilities ranging from 200 passengers in a highcomfort multi-class layout, up to 440 passengers in a high efficiency configuration. The new-generation mid-size freighter, the A330-200F, has up to 70 t (154 324 lb) payload and a range up to4 000 nm (7 408 km). It offers better payload, range and economics than previous-generationfreighters.The ACJ330 offers true space and comfort whilst delivering a ”non-stop to the world” range forcorporate, VIP and government operators.The A330 MRTT is the most capable in-flight refueling platform available.
The A330 combines maturity and reliability with the most up-to-date technology. It consistentlyachieves an average dispatch reliability of over 99% and annual utilization of up to 5 500 FlightHours. At the same time it is continuously improved by incorporating the latest technologies, to loweroperating costs, increase efficiency, improve safety and enhance the passenger product -- pioneering240 minutes ETOPS, introducing RNP to wide-bodies and being the first aircraft to have line-fit totalconnectivity for passengers.
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The latest improvement is an increase to 242t (533 519 lb) MTOW adding even more range -- 2 100nm (3 889 km) more range since the A330-300 EIS -- with lower fuel burn. In the meantime the A330engine manufacturers - General Electric, Pratt & Whitney and Rolls-Royce - have recently introducedfeatures to further reduce fuel burn, maintenance costs and improve performance.
This document does not include the latest A330 at 242t (533 519 lb) MTOW which is underdevelopment.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services1, Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0Page 2
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1-2-1 Glossary
**ON A/C A330-200 A330-200F A330-300
Glossary
1. List of Abbreviations
A/C Aircraft
ACN Aircraft Classification NumberAMM Aircraft Maintenance ManualAPU Auxiliary Power Unit
B/C (except A330-200F) Business Class
C/L Center Line
CBR California Bearing Ratio
CC Cargo Compartment
CG Center of Gravity
CKPT Cockpit
E Young’s Modulus
ELEC Electric, Electrical, Electricity
ESWL Equivalent Single Wheel Load
F/C (except A330-200F) First Class
FAA Federal Aviation AdministrationFDL Fuselage Datum Line
FR FrameFSTE Full Size Trolley Equivalent
FWD ForwardGPU Ground Power UnitGSE Ground Support Equipment
HYD Hydraulic
ICAO International Civil Aviation Organisation
IDG Integrated Drive Generator
ISA International Standard Atmosphere
L Radius of relative stiffnessLCN Load Classification NumberLD Load DeviceLD Lower DeckL/G Landing Gear
LH Left HandLPS (except A330-200F) Last Pax Seating
MAC Mean Aerodynamic Chord
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
MAX MaximumMD Main DeckMDCC (A330-200F only) Main Deck Cargo Compartment
MIN MinimumMLG Main Landing Gear
MLW Maximum Design Landing Weight
MRW Maximum Design Ramp Weight
MTOW Maximum Design Take-Off Weight
MTW Maximum Design Taxi Weight
MZFW Maximum Design Zero Fuel Weight
NLG Nose Landing Gear
OAT Outside Air Temperature
PAX (except A330-200F) Passenger
PB/D (except A330-200F) Passenger Boarding/Deboarding
PBB Passenger Boarding Bridge
PCA Portland Cement AssociationPCN Pavement Classification Number
PRM (except A330-200F) Passenger with Reduced Mobility
RH Right Hand
ULD Unit Load DeviceUS United StatesWV Weight Variant
Y/C (except A330-200F) Economy Class
2. Design Weight Terminology- Maximum Design Ramp Weight (MRW):
Maximum weight for ground maneuver (including weight of taxi and run-up fuel) as limited byaircraft strength and airworthiness requirements. It is also called Maximum Design Taxi Weight(MTW).
- Maximum Design Landing Weight (MLW):Maximum weight for landing as limited by aircraft strength and airworthiness requirements.
- Maximum Design Take-Off Weight (MTOW):Maximum weight for take-off as limited by aircraft strength and airworthiness requirements. (Thisis the maximum weight at start of the take-off run).
- Maximum Design Zero Fuel Weight (MZFW):Maximum permissible weight of the aircraft without usable fuel.
- Maximum Seating Capacity:Maximum number of passengers specifically certified or anticipated for certification.
- Usable Volume:
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Usable volume available for cargo, pressurized fuselage, passenger compartment and cockpit.- Water Volume:
Maximum volume of cargo compartment.- Usable Fuel:
Fuel available for aircraft propulsion.
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-1-1 General Aircraft Characteristics Data
**ON A/C A330-200 A330-300
General Aircraft Characteristics Data
**ON A/C A330-300
1. The following table provides characteristics of A330-300 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002 WV003
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
212 900 kg(469 364 lb)
184 900 kg(407 635 lb)
212 900 kg(469 364 lb)
215 900 kg(475 978 lb)
Maximum Take-Off Weight(MTOW)
212 000 kg(467 380 lb)
184 000 kg(405 650 lb)
212 000 kg(467 380 lb)
215 000 kg(473 994 lb)
Maximum Landing Weight (MLW)174 000 kg(383 604 lb)
174 000 kg(383 604 lb)
177 000 kg(390 218 lb)
177 000 kg(390 218 lb)
Maximum Zero Fuel Weight(MZFW)
164 000 kg(361 558 lb)
164 000 kg(361 558 lb)
167 000 kg(368 172 lb)
167 000 kg(368 172 lb)
Aircraft Characteristics
WV004 * WV010 WV011 WV012
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
209 900 kg to 215900 kg
(462 750 lb to 475978 lb)
217 900 kg(480 387 lb)
212 900 kg(469 364 lb)
218 900 kg(482 592 lb)
Maximum Take-Off Weight(MTOW)
209 000 kg to 215000 kg
(460 766 lb to 473994 lb)
217 000 kg(478 403 lb)
212 000 kg(467 380 lb)
218 000 kg(480 608 lb)
Maximum Landing Weight (MLW)
182 000 kg to 177000 kg
(401 241 lb to 390218 lb)
179 000 kg(394 627 lb)
177 000 kg(390 218 lb)
182 000 kg(401 241 lb)
Maximum Zero Fuel Weight(MZFW)
172 000 kg to 167000 kg
(379 195 lb to 368172 lb)
169 000 kg(372 581 lb)
167 000 kg(368 172 lb)
172 000 kg(379 195 lb)
NOTE : * Linear MTOW/MZFW trade-off relationship.
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Aircraft CharacteristicsWV013 WV014 WV020 WV022 WV024
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
215 900 kg(475 978 lb)
205 900 kg(453 932 lb)
230 900 kg(509 047 lb)
233 900 kg(515 661 lb)
205 900 kg(453 932 lb)
Maximum Take-Off Weight(MTOW)
215 000 kg(473 994 lb)
205 000 kg(451 948 lb)
230 000 kg(507 063 lb)
233 000 kg(513 677 lb)
205 000 kg(451 948 lb)
Maximum Landing Weight (MLW)177 000 kg(390 218 lb)
182 000 kg(401 241 lb)
185 000 kg(407 855 lb)
187 000 kg(412 264 lb)
185 000 kg(407 855 lb)
Maximum Zero Fuel Weight(MZFW)
167 000 kg(368 172 lb)
172 000 kg(379 195 lb)
173 000 kg(381 400 lb)
175 000 kg(385 809 lb)
173 000 kg(381 400 lb)
Aircraft CharacteristicsWV025 WV050 WV051 WV052 WV053
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
217 900 kg(480 387 lb)
230 900 kg(509 047 lb)
212 900 kg(469 364 lb)
233 900 kg(515 661 lb)
205 900 kg(453 932 lb)
Maximum Take-Off Weight(MTOW)
217 000 kg(478 403 lb)
230 000 kg(507 063 lb)
212 000 kg(467 380 lb)
233 000 kg(513 677 lb)
205 000 kg(451 948 lb)
Maximum Landing Weight (MLW)179 000 kg(394 627 lb)
185 000 kg(407 855 lb)
187 000 kg(412 264 lb)
187 000 kg(412 264 lb)
185 000 kg(407 855 lb)
Maximum Zero Fuel Weight(MZFW)
169 000 kg(372 581 lb)
173 000 kg(381 400 lb)
175 000 kg(385 809 lb)
175 000 kg(385 809 lb)
173 000 kg(381 400 lb)
Aircraft CharacteristicsWV054 WV055 ** WV056
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
235 900 kg(520 070 lb)
235 900 kg(520 070 lb)
205 900 kg(453 932 lb)
Maximum Take-Off Weight(MTOW)
235 000 kg(518 086 lb)
235 000 kg(518 086 lb)
205 000 kg(451 948 lb)
Maximum Landing Weight (MLW)187 000 kg(412 264 lb)
187 000 kg(412 264 lb)
187 000 kg(412 264 lb)
Maximum Zero Fuel Weight(MZFW)
173 000 kg(381 400 lb)
173 000 kg to 175 000 kg(381 400 lb to 385 809 lb)
175 000 kg(385 809 lb)
NOTE : ** Dynamic Payload between WV052 and WV054.
2. The following table provides characteristics of A330-300 Models, these data are common to eachWeight Variant:
Aircraft Characteristics
Standard Seating Capacity (Single-class) 335
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics97 530 l
(25 765 US gal)Usable Fuel Capacity(density = 0.785 kg/l) 76 561 kg
(168 787 lb)
Pressurized Fuselage Volume (A/C nonequipped)
1 056 m3
(37 292 ft3)
Passenger Compartment Volume372 m3
(13 137 ft3)
Cockpit Volume12 m3
(424 ft3)
Usable Volume, FWD CC(Based on LD3)
78 m3
(2754 ft3)
Usable Volume, AFT CC(Based on LD3)
60.7 m3
(2 142 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC107 m3
(3 789ft3)
Water Volume, AFT CC85.7 m3
(3 026ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
**ON A/C A330-200
3. The following table provides characteristics of A330-200 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV020 WV021 WV022 WV023 WV024
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
230 900 kg(509 047
lb)
230 900 kg(509 047
lb)
233 900 kg(515 661
lb)
233 900 kg(515 661
lb)
202 900 kg(447 318
lb)
Maximum Take-Off Weight (MTOW)230 000 kg(507 063
lb)
230 000 kg(507 063
lb)
233 000 kg(513 677
lb)
233 000 kg(513 677
lb)
202 000 kg(445 334
lb)
Maximum Landing Weight (MLW)180 000 kg(396 832
lb)
182 000 kg(401 241
lb)
182 000 kg(401 241
lb)
180 000 kg(396 832
lb)
180 000 kg(396 832
lb)
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsWV020 WV021 WV022 WV023 WV024
Maximum Zero Fuel Weight (MZFW)168 000 kg(370 376
lb)
170 000 kg(374 786
lb)
170 000 kg(374 786
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
Aircraft CharacteristicsWV025 WV026 WV027 WV050 WV051
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
220 900 kg(487 001
lb)
192 900 kg(425 272
lb)
220 900 kg(487 001
lb)
230 900 kg(509 047
lb)
192 900 kg(425 272
lb)
Maximum Take-Off Weight (MTOW)220 000 kg(485 017
lb)
192 000 kg(423 287
lb)
220 000 kg(485 017
lb)
230 000 kg(507 063
lb)
192 000 kg(423 287
lb)
Maximum Landing Weight (MLW)182 000 kg(401 241
lb)
180 000 kg(396 832
lb)
180 000 kg(396 832
lb)
180 000 kg(396 832
lb)
180 000 kg(396 832
lb)
Maximum Zero Fuel Weight (MZFW)170 000 kg(374 786
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
Aircraft CharacteristicsWV052 WV053 WV054 WV055 WV056
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
233 900 kg(515 661
lb)
210 900 kg(464 955
lb)
230 900 kg(509 047
lb)
192 900 kg(425 272
lb)
233 900 kg(515 661
lb)
Maximum Take-Off Weight (MTOW)233 000 kg(513 677
lb)
210 000 kg(462 971
lb)
230 000 kg(507 063
lb)
192 000 kg(423 287
lb)
233 000 kg(513 677
lb)
Maximum Landing Weight (MLW)182 000 kg(401 241
lb)
180 000 kg(396 832
lb)
182 000 kg(401 241
lb)
182 000 kg(401 241
lb)
180 000 kg(396 832
lb)
Maximum Zero Fuel Weight (MZFW)170 000 kg(374 786
lb)
168 000 kg(370 376
lb)
170 000 kg(374 786
lb)
170 000 kg(374 786
lb)
168 000 kg(370 376
lb)
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsWV057 WV058 WV059 WV060
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
236 900 kg(522 275 lb)
238 900 kg(526 684 lb)
202 900 kg(447 318 lb)
220 900 kg(487 001 lb)
Maximum Take-Off Weight (MTOW)236 000 kg(520 291 lb)
238 000 kg(524 700 lb)
202 000 kg(445 334 lb)
220 000 kg(485 017 lb)
Maximum Landing Weight (MLW)182 000 kg(401 241 lb)
182 000 kg(401 241 lb)
182 000 kg(401 241 lb)
182 000 kg(401 240 lb)
Maximum Zero Fuel Weight (MZFW)170 000 kg(374 786 lb)
168 000 kg(370 376 lb)
170 000 kg(374 786 lb)
170 000 kg(374 786 lb)
Aircraft CharacteristicsWV061 WV062 ***
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
230 900 kg(509 047 lb)
238 900 kg(526 684 lb)
Maximum Take-Off Weight (MTOW)230 000 kg(507 063 lb)
238 000 kg(524 700 lb)
Maximum Landing Weight (MLW)182 000 kg(401 240 lb)
182 000 kg(401 241 lb)
Maximum Zero Fuel Weight (MZFW)168 000 kg(370 376 lb)
168 000 kg to 170 000 kg(370 376 lb to 374 786 lb)
NOTE : *** Dynamic Payload between WV057 and WV058.
4. The following table provides characteristics of A330-200 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard Seating Capacity 303
139 090 l(36 744 US gal)Usable Fuel Capacity
(density = 0.785 kg/l) 109 185 kg(240 711 lb)
Pressurized Fuselage Volume (A/C nonequipped)
950 m3
(33 548 ft3)
Passenger Compartment Volume335 m3
(11 830 ft3)
Cockpit Volume12 m3
(424 ft3)
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Aircraft CharacteristicsUsable Volume, FWD CC(Based on LD3)
60.7 m3
(2 142 ft3)
Usable Volume, AFT CC(Based on LD3)
52 m3
(1 836 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC84.6 m3
(2 988 ft3)
Water Volume, AFT CC71.1 m3
(2 511 ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
2-1-1Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
General Aircraft Characteristics Data
1. The following table provides characteristics of A330-200F Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002*
Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)
233 900 kg(515 661 lb)
227 900 kg(502 433 lb)
233 900 kg(515 661 lb)
Maximum Take-Off Weight(MTOW)
233 000 kg(513 677 lb)
227 000 kg(500 449 lb)
233 000 kg(513 677 lb)
Maximum Landing Weight(MLW)
182 000 kg(401 241 lb)
187 000 kg(412 264 lb)
187 000 kg(412 264 lb)
Maximum Zero Fuel Weight(MZFW)
173 000 kg(381 400 lb)
178 000 kg(392 423 lb)
173 000 kg to 178 000kg
(381 399 lb to 392 422lb)
Estimated MaximumPayload PW 4000
64 742 kg(142 732 lb)
69 742 kg(153 755 lb)
64 742 kg to 69 742 kg(142 732 lb to 153 755
lb)
Estimated MaximumPayload TRENT 700
65 000 kg(143 300 lb)
70 000 kg(154 324 lb)
65 000 kg to 70 000 kg(143 300 lb to 154 324
lb)
NOTE : * Dynamic Payload between WV000 and WV001
2. The following table provides characteristics of A330-200F Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsSupernumerary area 6
Usable Fuel Capacity(density = 0.785 kg/l)
139 090 l(36 755 US gal)
Pressurized Fuselage Volume(A/C non equipped)
900 m3
(31 783 ft3)
Cockpit Volume12 m3
(424 ft3)
2-1-1Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsMain Deck CargoCompartment Usable Volume(Based on 96”x125” pallet)
336.8 m3
(11 894 ft3)
Main Deck CargoCompartment Water Volume
466.5 m3
(16 474 ft3)
Usable Volume, FWD CC(Based on LD3)
60.7 m3
(2 142 ft3)
Usable Volume, AFT CC(Based on LD3)
52 m3
(1 836 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC84.6 m3
(2 988 ft3)
Water Volume, AFT CC71.1 m3
(2 511 ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
2-1-1Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0 General Aircraft Dimensions
**ON A/C A330-200 A330-300
General Aircraft Dimensions
1. This section provides General Aircraft Dimensions for pax version.
2-2-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
(35.04 ft)10.68 m
(41.37 ft)12.61 m
(61.48 ft)18.74 m
(2.33 ft)0.71 m
(197.83 ft)60.3 m
(63.65 ft)19.4 m
(105.15 ft)32.05 m
(18.5 ft)5.64 m
(25.56 ft)7.79 m
(172.01 ft)52.43 m
(206.33 ft)62.89 m
(208.89 ft)63.67 m
(10.17 ft)3.1 m
(21.88 ft)6.67 m
(27.23 ft)8.3 m
(26.71 ft)8.14 m
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. F_AC_020200_1_0010101_01_02
General Aircraft Dimensions(Sheet 1 of 2)
FIGURE-2-2-0-991-001-A01
2-2-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
(69.82 ft)21.28 m
(138.52 ft)42.22 m
(128.28 ft)39.1 m
(202.33 ft)61.67 m
(208.99 ft)63.7 m
(34.65 ft)10.56 m
(8.23 ft)2.51 m
(6.66 ft)2.03 m
(21.1 ft)6.43 m
(35.7 ft)10.88 m
7.46 m
(46.
62 ft
)14
.21
m
(57.
91 ft
)17
.65
m
(24.48 ft)
(70.37 ft)21.45 m
(69.36 ft)21.14 m
GE
PW
RR
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
F_AC_020200_1_0010104_01_00
General Aircraft Dimensions(Sheet 2 of 2)
FIGURE-2-2-0-991-001-A01
2-2-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
(94.65 ft)28.85 m
(18.5 ft)5.64 m
(28.15 ft)8.58 m
(154.49 ft)47.09 m
(188.68 ft)57.51 m
(193.57 ft)59 m
(9.15 ft)2.79 m
(21.88 ft)6.67 m
(35.04 ft)10.68 m
(41.37 ft)12.61 m
(61.48 ft)18.74 m
(2.33 ft)0.71 m
(197.83 ft)60.3 m
(63.65 ft)19.4 m
(30.51 ft)9.3 m
(29.92 ft)9.12 m
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. F_AC_020200_1_0020101_01_02
General Aircraft Dimensions(Pre Mod 48979) (Sheet 1 of 3)
FIGURE-2-2-0-991-002-A01
2-2-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
(94.65 ft)28.85 m
(18.5 ft)5.64 m
(28.15 ft)8.58 m
(154.49 ft)47.09 m
(188.68 ft)57.51 m
(192.98 ft)58.82 m
(10.17 ft)3.1 m
(21.88 ft)6.67 m
(35.04 ft)10.68 m
(41.37 ft)12.61 m
(61.48 ft)18.74 m
(2.33 ft)0.71 m
(197.83 ft)60.3 m
(63.65 ft)19.4 m
(28.87 ft)8.8 m
(28.31 ft)8.63 m
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. F_AC_020200_1_0020103_01_00
General Aircraft Dimensions(Post Mod 48979) (Sheet 2 of 3)
FIGURE-2-2-0-991-002-A01
2-2-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
(59.32 ft)18.08 m
(128.08 ft)39.04 m
(117.98 ft)35.96 m
(184.91 ft)56.36 m
(191.5 ft)58.37 m
(34.65 ft)10.56 m
(8.07 ft)2.46 m
(6.59 ft)2.01 m
(21.13 ft)6.44 m
(35.7 ft)10.88 m
7.46 m
(46.
62 ft
)14
.21
m
(57.
91 ft
)17
.65
m
(24.48 ft)
(59.88 ft)18.25 m
(58.86 ft)17.94 m
GE
PW
RR
F_AC_020200_1_0020102_01_00
General Aircraft Dimensions(Sheet 3 of 3)
FIGURE-2-2-0-991-002-A01
2-2-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
General Aircraft Dimensions
1. This section provides General Aircraft Dimensions for cargo version.
2-2-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
(94.65 ft)28.85 m
(154.49 ft)47.09 m
(188.68 ft)57.51 m
(192.98 ft)58.82 m
(18.5 ft)5.64 m
(28.15 ft)8.58 m
(10.17 ft)3.1 m
(28.31 ft)8.63 m
(21.88 ft)6.67 m
(28.87 ft)8.8 m
(197.83 ft)60.3 m
(63.65 ft)19.4 m
(35.04 ft)10.68 m
(41.37 ft)12.61 m
(61.48 ft)18.74 m
(2.33 ft)0.71 m
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
F_AC_020200_1_0030101_01_02
General Aircraft Dimensions(Sheet 1 of 2)
FIGURE-2-2-0-991-003-A01
2-2-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
(59.32 ft)18.08m
(126.08 ft)38.43 m
(117.95 ft)35.95 m
(184.84 ft)56.34 m
(191.47 ft)58.36 m
(59.88 ft)18.25 m
PW
RR
(8.14 ft)2.48 m
(6.63 ft)2.02 m
(21.1 ft)6.43 m
(34.61 ft)10.55 m
(35.7 ft)10.88 m
7.46 m(24.48 ft)
(46.
62 ft
)14
.21
m
(57.
91 ft
)17
.65
m
F_AC_020200_1_0030102_01_00
General Aircraft Dimensions(Sheet 2 of 2)
FIGURE-2-2-0-991-003-A01
2-2-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0 Ground Clearances
**ON A/C A330-200 A330-200F A330-300
Ground Clearances
1. This section gives the height of various points of the aircraft, above the ground, for different aircraftpax configurations.Dimensions in the tables are approximate and will vary with tire type, W&B an others specialconditions.
The dimensions are given for:- A light weight for an A/C in maintenance configuration with a mid CG,- The MRW for the lightest weight variant with a FWD CG and a AFT CG,- The MRW for the heaviest weight variant with a FWD CG and a AFT CG,- Aircraft on jacks, FDL at 6.5 m (21.33 ft).
NOTE : Passenger and cargo door clearances are measured from the center of the door sill and fromfloor level.
2-3-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
X L C2 Y KE3 H E2
D C1B E1
AM
P N V U T S R O
J
MRW212 900 kg469 360 lb
Am ftm ftm ftm
BC1C2D
GE = RPW = RRR = R
YXVUTS
PONMLKJH
E3E2E1
3.687.484.974.644.333.870.870.900.948.058.336.4617.185.773.435.342.042.742.282.104.838.537.742.704.55
12.0724.54
15.2214.2012.702.852.953.0826.4127.3221.2056.3618.9311.2517.56.7
8.997.486.89
15.8428
25.48.85
14.92
16.30
3.467.244.724.414.133.680.690.720.767.708.096.13
16.945.553.225.311.862.542.101.954.678.317.582.554.41
11.3523.7615.4814.4613.5512.072.262.362.49
25.2626.5420.1155.5818.2010.5617.46.108.336.886.39
15.3227.2624.868.36
14.46
3.357.034.674.374.11
0.720.750.797.617.886.0616.725.413.135.201.852.452.142.034.738.197.672.664.55
3.64
1123.0615.3214.3313.4811.942.362.462.59
24.9625.8519.8854.8517.7510.2717.066.078.037.026.6615.5126.8725.16
8.7214.92
4.398.106.30
65.705.252.212.292.348.969.237.55
17.626.534.246.433.263.683.683.686.329.329.324.146.32
14.426.520.619.618.717.27.257.517.6729.430.224.757.821.4
21.110.7121212
20.730.530.513.520.7
13.9
ft
NOTE:
MAXIMUM RAMPWEIGHT CG 36.5%
MAXIMUM RAMPWEIGHT CG 15%
AIRCRAFTON JACKS
PASSENGER AND CARGO DOOR CLEARANCES ARE MEASURED FROMTHE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
119 000 kgCG 26.8%
F_AC_020300_1_0010101_01_02
Ground ClearancesFIGURE-2-3-0-991-001-A01
2-3-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
K
E3 H E2 B E1M
P N V U T S R O
ZJ
Am ftm m ftm
BC1C2D
PW = RRR = R
VUTS
PON
MLKJHE3E2E1
3.683.68
6.32
20.619.618.717.27.257.517.6729.430.224.7
21.4
10.7121212
20.730.5
20.7
MAXIMUM RAMPWEIGHT CG 37.5%
5.413.667.474.954.634.353.890.870.900.948.088.306.48
5.743.505.36
2.702.232.044.868.547.75
2.02
YZ
2.784.63
12.01
16.2415.1914.2712.762.852.953.0826.5127.2321.26
18.8311.4817.66.638.867.31
28.02
17.75
24.51
25.429.12
15.19
3.437.234.734.424.133.670.670.700.747.718.056.14
5.513.275.151.812.482.031.844.668.317.56
4.442.58
17.1211.2523.7215.52
13.5512.042.192.292.42
25.2926.4120.14
18.0710.73
5.938.136.666.03
27.2624.80
14.568.46
5.433.306.974.674.374.113.640.720.750.797.617.776.05
5.353.165.101.832.402.122.014.78
4.632.74
17.8110.8222.8615.3214.3313.4811.942.362.462.59
24.9625.4919.85
17.5510.3616.7
67.876.956.5915.7
25.2326.77
8.99
ft15.19
7.104.398.106.30
65.705.252.212.292.348.969.237.55
6.534.246.463.26
3.686.369.329.324.14 13.5
30.5
21.213.9
14.423.30
MRW230 900 kg509 042 lb
14.50
8.167.69
ft
MAXIMUM RAMPWEIGHT CG 21%
15.96.7
15.3
16.9
5.22
25.5
V U
V U
M1 18.1261.0959.45
18.23 59.858.17
17.9817.48
58.9957.35
17.7117.21
58.1 18.6256.4617.73
AIRCRAFTON JACKS
M1 = POST MOD 48979 (SHORTER FIN INSTALLATION).NOTE:
GE = R
PASSENGER AND CARGO DOOR CLEARANCES ARE MEASURED FROMTHE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
L C2 D C1 AY
176 000 kgMID CG 27.9%
F_AC_020300_1_0010202_01_00
Ground ClearancesFIGURE-2-3-0-991-001-B01
2-3-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
OR
ST
UV
NP
ZC
1J
VU
M
E5
RH
E6
C2
KY
NO
TE
:P
AS
SE
NG
ER
AN
D C
AR
GO
DO
OR
CLE
AR
AN
CE
S A
RE
ME
AS
UR
ED
FR
OM
TH
E C
EN
TE
RO
F T
HE
DO
OR
SIL
L A
ND
FR
OM
FLO
OR
LE
VE
L.
DB
E3
A
F_AC_020300_1_0010301_01_00
Ground Clearances(Sheet 1 of 2)
FIGURE-2-3-0-991-001-C01
2-3-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
m 5.06
8.44
8.06
3.11
4.98
16.6
027
.69
26.4
410
.20
16.3
4ft
2.98
9.79
17.4
157
.12
1.06
1.13
7.80
3.52
5.55
2.16
2.70
2.47
2.22
3.48
3.71
25.5
9
11.5
518
.21
7.09
8.86
8.10
7.28
8.31
27.2
69.
2330
.28
3.61
7.92
11.8
425
.98
6.22
20.4
1
2.74
2.92
3.02
8.99
9.59
9.91
NO
TE
:P
AS
SE
NG
ER
AN
D C
AR
GO
DO
OR
CLE
AR
AN
CE
S A
RE
ME
AS
UR
ED
FR
OM
TH
E C
EN
TE
R O
F T
HE
DO
OR
SIL
L A
ND
FR
OM
FLO
OR
LE
VE
L.
115
000
kgC
G 2
0%ft
mft
m
4.88
8.06
7.87
2.93
4.82
16.0
126
.44
25.8
29.
6115
.81
5.03
7.91
8.01
3.085
16.5
025
.95
26.2
810
.10
16.4
0
0.82
0.89
7.46
16.9
53.
155.
131.
892.
372.
262.
06
2.69
2.92
24.4
855
.61
10.3
316
.83
6.20
7.78
7.41
6.76
0.87
0.95
7.36
16.6
73.
044.
911.
912.
292.
352.
24
2.85
3.12
24.1
554
.69
9.97
16.1
16.
277.
517.
717.
35
7.85
25.7
57.
5724
.84
8.88
29.1
38.
7828
.81
3.25
7.46
10.6
624
.48
3.12
7.19
10.2
423
.59
6.08
19.9
56.
2920
.64
2.44
2.69
2.63
2.70
8 8.83
8.62
8.86
2.41
2.67
2.60
2.64
7.89
8.75
8.53
8.66
MR
W 2
33 9
00 k
gC
G 2
0.6%
MR
W 2
33 9
00 k
gC
G 3
7.4%
A B C1
C2 D
PW
RR
R R
YVUVUTSMKJHE6
E5
E3 N ZO P
F_AC_020300_1_0010302_01_00
Ground Clearances(Sheet 2 of 2)
FIGURE-2-3-0-991-001-C01
2-3-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
A B C
m ft m ft m ft
A
B
C
D
MAXIMUM RAMPWEIGHT CG 15.0%
MAXIMUM RAMPWEIGHT CG 36.5%
6.426.506.85
6.58 6.26 6.20
6.206.266.58
6.38 6.07 6.02
D
22.47
21.59
21.59
20.93
21.33
20.54
20.54
19.91
21.06
20.34
20.34
19.75
AILERONS UP
A/C IN MAINTENANCECONFIGURATION
MID CG 26.8%
F_AC_020300_1_0150101_01_00
Ground ClearancesAilerons Up
FIGURE-2-3-0-991-015-A01
2-3-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
A B C D
m ft m ft m ft
A
B
C
D
MAXIMUM RAMPWEIGHT CG 15.0%
MAXIMUM RAMPWEIGHT CG 36.5%
6.30
5.83
5.83
5.47
5.94
5.51
5.51
5.17
5.87
5.44
5.44
5.11
20.67 19.49 19.26
16.7716.9617.95
19.13
19.13
18.08
18.08
17.85
17.85
AILERONS DOWN
A/C IN MAINTENANCECONFIGURATION
MID CG 26.8%
F_AC_020300_1_0160101_01_00
Ground ClearancesAilerons Down
FIGURE-2-3-0-991-016-A01
2-3-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
m ft m ft m ft
A
B
C
D
5.10
E
F
G
H
J
K
L
M 4.58
5.68
5.68
5.48
MAXIMUM RAMPWEIGHT CG 15.0%
MAXIMUM RAMPWEIGHT CG 36.5%
6.60
6.44
6.44
6.29
6.29
6.12
6.12
5.93
5.93
5.72
5.31
4.76
6.31
6.18
6.18
6.04
6.04
5.89
5.89
5.71
5.71
5.51
6.26
6.13
6.13
6.00
6.00
5.86
5.86
5.07
4.55
21.65
21.13
21.13
20.64
20.64
20.08
20.08
19.46
19.46
18.77
17.42
15.62
20.70
20.28
20.28
19.82
19.82
19.32
19.32
18.73
18.73
18.08
16.73
15.03
20.54
20.11
20.11
19.69
19.69
19.23
19.23
18.64
17.98
16.63
14.93
18.64
SPOILERS 1 TO 6 EXTENDED
A/C IN MAINTENANCECONFIGURATION
MID CG 26.8%
A B C D E F G H L MJ K
F_AC_020300_1_0170101_01_00
Ground ClearancesSpoilers Extended
FIGURE-2-3-0-991-017-A01
2-3-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
m ft m ft m ft
A
B
C
D
E
F
G
H
J
K
L
M
N
P
3.46
4.25
4.28
4.65
4.65
4.99
4.99
5.30
5.37
5.65
5.65
5.91
5.91
6.16
3.28
4.09
4.10
4.45
4.45
4.77
4.77
5.06
5.12
5.37
5.37
5.61
5.61
5.82
3.31
4.10
4.11
4.45
4.45
4.76
4.76
5.03
5.09
5.33
5.33
5.56
5.56
5.76
MAXIMUM RAMPWEIGHT CG 36.5%
MAXIMUM RAMPWEIGHT CG 15.0%
11.35
13.94
14.04
15.26
15.26
16.37
16.37
17.39
17.62
18.54
18.54
19.39
19.39
20.21
10.76
13.42
13.45
14.60
14.60
15.65
15.65
16.60
16.80
17.62
17.62
18.41
18.41
19.09
10.86
13.45
13.48
14.60
14.60
15.62
15.62
16.50
16.70
17.49
17.49
18.24
18.24
18.90
LEADING EDGE SLATS EXTENDED
A/C IN MAINTENANCECONFIGURATION
MID CG 26.8%
A D E F G H J K L M N PB C
F_AC_020300_1_0180101_01_00
Ground ClearancesSlats Fully Extended
FIGURE-2-3-0-991-018-A01
2-3-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
m ft m ft m ft
A
B
C
D
A B C D
5.21
4.00
4.00
2.71
4.91
3.79
3.80
2.52
4.85
3.75
3.76
2.49
MAXIMUM RAMPWEIGHT CG 15.0%
MAXIMUM RAMPWEIGHT CG 36.5%
17.09
13.12
13.12
8.89
16.11
12.43
12.47
8.27
15.91
12.30
12.34
8.17
INNER AND OUTER FLAPS EXTENDED
A/C IN MAINTENANCECONFIGURATION
MID CG 26.8%
F_AC_020300_1_0190101_01_00
Ground ClearancesFlaps Fully Extended
FIGURE-2-3-0-991-019-A01
2-3-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
m ft m ft m ft
A
B
C
D
3.24
4.08
3.73
3.48
2.95
MAXIMUM RAMPWEIGHT CG 15.0%
MAXIMUM RAMPWEIGHT CG 36.5%
3.88
3.53
3.29
2.75
3.82
3.48
2.71
13.39
12.24
11.42
9.68
12.73
11.58
10.79
9.02
12.53
11.42
10.63
8.89
A B C D
FLAP TRACKS EXTENDED
A/C IN MAINTENANCECONFIGURATION
MID CG 26.8%
F_AC_020300_1_0200101_01_00
Ground ClearancesFlaps-Tracks Fully ExtendedFIGURE-2-3-0-991-020-A01
2-3-0Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1 Interior Arrangements - Plan View
**ON A/C A330-200 A330-300
Interior Arrangements - Plan View
1. This section gives the typical configuration for A330 pax version.
2-4-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
NO
TE
:F
OR
DO
OR
SIZ
ES
SE
E C
HA
PT
ER
2−
7
PA
SS
EN
GE
R S
EA
TS
(29
5 T
OT
AL)
12 F
IRS
T C
LAS
S
241
EC
ON
OM
Y C
LAS
S
CO
AT
ST
OW
AG
E
ST
OW
AG
E
GA
LLE
Y
LAV
AT
OR
Y
AT
TE
ND
AN
TS
SE
AT
42 B
US
INE
SS
CLA
SS
VCC
ITE
MD
ES
IGN
AT
ION
A C G L S
(12)
(4)
(7)
(9)
(1)
A
A AA
A A
A A
A A
AA
GG
GG
GG
G
C C
CC
L LLL
L L L L
L
S
F_AC_020401_1_0010101_01_00
Interior Arrangements - Plan ViewTypical Configuration
FIGURE-2-4-1-991-001-A01
2-4-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
NO
TE
:F
OR
DO
OR
SIZ
ES
SE
E C
HA
PT
ER
2−
7
PA
SS
EN
GE
R S
EA
TS
(25
3 T
OT
AL)
12 F
IRS
T C
LAS
S
205
EC
ON
OM
Y C
LAS
S
TR
OLL
EY
36 B
US
INE
SS
CLA
SS
VC
C
CO
AT
ST
OW
AG
E
ST
OW
AG
E
GA
LLE
Y
LAV
AT
OR
Y
AT
TE
ND
AN
TS
SE
AT
ITE
MD
ES
IGN
AT
ION
A C G L S
(12)
(2)
(6)
(8)
(1)
Tr
(2)
A
A AA
AA
AA
A A
A AC
C
G
GG
G
G G
L L L LLL
L LS
Tr
Tr
F_AC_020401_1_0020101_01_00
Interior Arrangements - Plan ViewTypical Configuration
FIGURE-2-4-1-991-002-A01
2-4-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0 Interior Arrangements - Cross Section
**ON A/C A330-200 A330-300
Interior Arrangements - Cross Section
1. This section gives the typical configuration of A330 pax version.
2-5-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
AB
C C D
C D C D
F N M
C C D
H
K K
F G
222 in5.640 m
208 in5.290 m
FIRST CLASS, 6 ABREAST BUSINESS CLASS, 7 ABREAST
TOURIST CLASS, 8 ABREAST CHARTER CLASS, 9 ABREAST
A − 54.0 in (1371.6 mm)B − 21.0 in (533 mm)C − 39.6 in (1006 mm)D − 17.7 in (450 mm)E − 72.0 in (1829 mm)F − 19.0 in (483 mm)
G − 48.0 in (1219 mm)H − 19.8 in (503 mm)K − 41.5 in (1054.1 mm)M − 57.1 in (1450 mm)N − 16.5 in (419 mm)
91.7 in2.330 mA E
H C
M
F_AC_020500_1_0010101_01_00
Interior Arrangements - Cross SectionTypical Configuration
FIGURE-2-5-0-991-001-A01
2-5-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-1 Lower Deck Cargo Compartments
**ON A/C A330-200 A330-200F A330-300
Lower Deck Cargo Compartments
1. This section gives the following data about lower deck cargo compartments:- Location and dimensions- Loading combinations.
2-6-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
0.95 m(3.12 ft)
2.75 m(9.02 ft)
2.78 m(9.12 ft)
15.02 m(49.28 ft)
A330−300
11.82 m(38.78 ft)
A330−200/−200F
12.32 m(40.42 ft)
10.19 m(33.43 ft)
4.04 m(13.25 ft)
4.04 m(13.25 ft)
LOWER DECKFWD CARGO
COMPARTMENT
LOWER DECKAFT CARGO
COMPARTMENT
LOWER DECKBULK CARGO
COMPARTMENT
FR39.1 FR53.2 FR65 FR73FR20
NOTE:APPROXIMATE DIMENSIONS DEPENDING ON AIRCRAFT CONFIGURATION.
F_AC_020601_1_0030101_01_01
Lower Deck Cargo CompartmentsLocation and Dimensions
FIGURE-2-6-1-991-003-A01
2-6-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
14 LD3 60.4 in X 61.5 in
7 LD3 60.4 in X 61.5 in
4 PALLETS 96 in X 125 in
4 PALLETS 88 in X 125 in
7 PALLETS 60.4 in X 125 in
12 LD3 60.4 in X 61.5 in
6 LD3 60.4 in X 61.5 in
4 PALLETS 96 in X 125 in
4 PALLETS 88 in X 125 in
6 PALLETS 60.4 in X 125 in
F_AC_020601_1_0040101_01_01
Lower Deck Cargo CompartmentsLoading Combinations
FIGURE-2-6-1-991-004-A01
2-6-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
18 LD3 60.4 in X 61.5 in
9 LD3 60.4 in X 61.5 in
6 PALLETS 96 in X 125 in
6 PALLETS 88 in X 125 in
9 PALLETS 60.4 in X 125 in
14 LD3 60.4 in X 61.5 in
7 LD3 60.4 in X 61.5 in
4 PALLETS 96 in X 125 in
5 PALLETS 88 in X 125 in
7 PALLETS 60.4 in X 125 in
F_AC_020601_1_0040201_01_00
Lower Deck Cargo CompartmentsLoading Combinations
FIGURE-2-6-1-991-004-B01
2-6-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-2 Main Deck Cargo Compartments
**ON A/C A330-200F
Main Deck Cargo Compartment
1. This section gives the following data about the main deck cargo compartment:- Location and dimensions- Loading combinations.
2-6-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
3.69 m(12.11 ft)
FR19 FR80
41.04 m(134.65 ft)
MAIN DECKCARGO
COMPARTMENT
NOTE:DEPENDING ON A/C CONFIGURATION. F_AC_020602_1_0060101_01_00
Main Deck Cargo CompartmentLocation and Dimensions
FIGURE-2-6-2-991-006-A01
2-6-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
1R
1L
2R
2L
3R
3L
4R
4L
5R
5L
6R
6L
7R
7L
8R
8L
9R
9L
10R
10L
11R
11L23 24 25 26
22 HCU−6/E (MILITARY) ULDs
4 HCU−6/E (MILITARY) ULDs
ABR
ABL
BCR
BCL
CER
CEL
EFR
EFL
FHR
FHL
HJR
HJL
JKR
JKL
KMR
KML
MPR
MPL
PRR
PRL
ABL
BCR
BCL
CER
CEL
EFR
EFL
FHR
FHL
HJR
HJL
JKR
JKL
KMR
KML
MPR
MPLSSRR TTPP
18 ULDs
96 in x 125 in
20 ULDs
88 in x 125 in3 ULDs
88 in x 125 in
4 ULDs
96 in x 125 in
ABR
F_AC_020602_1_0010101_01_01
88 in x 108 in
88 in x 108 in
T US
Main Deck Cargo CompartmentLoading Combinations
FIGURE-2-6-2-991-001-A01
2-6-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
AA BB CC DD EE FF GG HH JJ KK LL MM PP RR SS TT
16 ULDs
96 in x 125 in
17 ULDs
88 in x 125 in
AA BB CC DD EE FF GG HH JJ KK LL MM PP RR SS TT UU
AB BC CE EF FH HJ JK KM MP PP RR SS TT
9 AMA ULDs
96 in x 125 in
4 ULDs
96 in x 125 in
AB BC CE EF FH HJ JK KM MP
9 AMA ULDs
96 in x 125 in
R S T U
F_AC_020602_1_0020101_01_01
4 ULDs
88 in x 125 in
Main Deck Cargo CompartmentLoading Combinations
FIGURE-2-6-2-991-002-A01
2-6-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
42 AYY ULDs
1R
1C
1L
2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R
2C 3R 4C 5C 6C 7C 8C 9C 10C 11C 12C 13C 14C
2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L
1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R
1L 2L 3L 4L 5L 6L 7L 8L 9L 10L15R 16R 17R
15L 16L 17L
1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L
2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R
15 16 17
15R 16R 17R
15L 16L 17L
1R
88 in x 62 in
6 AYY ULDs
14 AYY ULDs + 10 AMJ ULDs
14 AYY ULDs + 14 SAA ULDs
6 AYY ULDs
SAA
88 in x 62 in
88 in x 62 in
3 SAA ULDs
AYY
AYY
AMJ
88 in x 125 in
62 in x 88 in + 96 in x 125 in
62 in x 88 in + 88 in x 125 in
F_AC_020602_1_0030101_01_02
Main Deck Cargo CompartmentLoading Combinations
FIGURE-2-6-2-991-003-A01
2-6-2Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_020602_1_0050101_01_00
LPR PP RR SS TT
4 ULDs 4 ULDs
96 in x 125 in
JLRFHRCERBBAA
2 ULDs
96 in x 125 in
PP RR SS TT
3 ULDs 5 ULDs
96 in x 125 in
CEGBBAA
2 ULDs
96 in x 125 in
PP RR SS TT
8 ULDs 4 ULDs
96 in x 125 in
4 ULDs
96 in x 125 in
MMFJG JMG
CFRR
CFRL
BCR
BCL
ABR
ABL
FHRR
FHRL
JLRR
JLRL
LPRR
LPRL
16 ft
20 ft
16 ft
Main Deck Cargo CompartmentLoading Combinations
FIGURE-2-6-2-991-005-A01
2-6-2Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-3 Main and Lower Deck Cross-sections
**ON A/C A330-200F
Main and Lower Deck Cross-sections
1. This section gives Main and Lower Deck Cross-sections for cargo version.
2-6-3Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
LD6 / AAFCONTAINER AKE AKE
LD3 LD3ALF / AAF / AMF
CONTAINER PALLET
62"
96"
96"
AMA
125"
96"
96"
AMF96" x 125"
LD988" x 125"
88"
96"
REFERENCE CARGO CONFIGURATION LAYOUT
OPTIONAL CARGO CONFIGURATIONS
PALLETS88" x 108"/125"SIDE BY SIDE
PALLETS96" x 125"
SIDE BY SIDE
88"/96"
88" x 125"
79"
96"
62"
96" AYYSAA
125"
AMJ AYY AYY AYY AYY
F_AC_020603_1_0010101_01_01
Main and Lower Deck Cross-sectionsFIGURE-2-6-3-991-001-A01
2-6-3Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0 Door Clearances
**ON A/C A330-200 A330-200F A330-300
Door Clearances
1. This section gives door identification and location.
2-7-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
FWDPASSENGER/CREW
DOOR (1L)
MIDPASSENGER/CREW
DOOR (2L)
EMERGENCY EXITDOOR (3L)
AFTPASSENGER/CREW
DOOR (4L)
BULK CARGOCOMPARTMENT
DOOR AFT CARGO
COMPARTMENTDOOR
AFTPASSENGER/CREW
DOOR (4R)
EMERGENCY EXITDOOR (3R)
FWDPASSENGER/CREW
DOOR (1R)MID
PASSENGER/CREWDOOR (2R)
FWD CARGOCOMPARTMENT
DOOR
F_AC_020700_1_0060101_01_00
Door Identification and locationDoor Identification (Sheet 1 of 2)
FIGURE-2-7-0-991-006-A01
2-7-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
45.63 m(149.7 ft)
32.77 m(107.51 ft)
14.56 m(47.77 ft)
5.85 m(19.19 ft)
42.01 m(137.83 ft)
9.53 m(31.27 ft)
38.98 m(127.89 ft)
F_AC_020700_1_0060102_01_00
Door Identification and locationDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-006-A01
2-7-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FWDPASSENGER/CREW
DOOR (1L)
MIDPASSENGER/CREW
DOOR (2L)
EMERGENCY EXITDOOR (3L)
AFTPASSENGER/CREW
DOOR (4L)
BULK CARGOCOMPARTMENT
DOOR AFT CARGO
COMPARTMENTDOOR
AFTPASSENGER/CREW
DOOR (4R)
EMERGENCY EXITDOOR (3R)
FWDPASSENGER/CREW
DOOR (1R)MID
PASSENGER/CREWDOOR (2R)
FWD CARGOCOMPARTMENT
DOOR
F_AC_020700_1_0060201_01_00
Door Identification and LocationDoor Identification (Sheet 1 of 2)
FIGURE-2-7-0-991-006-B01
2-7-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
50.96 m(167.19 ft)
35.96 m(117.98 ft)
17.74 m(58.2 ft)
5.85 m(19.19 ft)
47.35 m(155.35 ft)
9.53 m(31.27 ft)
44.36 m(145.54 ft)
F_AC_020700_1_0060202_01_00
Door Identification and LocationDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-006-B01
2-7-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
FWD CREWDOOR (1L)
BULK CARGOCOMPARTMENT
DOOR AFT CARGO
COMPARTMENTDOOR
FWD CREWDOOR (1R)
FWD CARGOCOMPARTMENT
DOOR
MAIN DECKCARGO DOOR
F_AC_020700_1_0060301_01_00
Door Identification and LocationDoor Identification (Sheet 1 of 2)
FIGURE-2-7-0-991-006-C01
2-7-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
5.85 m(19.19 ft)
42.01 m(137.83 ft)
9.53 m(31.27 ft)
39.03 m(128.05 ft)
9.92 m(32.55 ft)
F_AC_020700_1_0060302_01_00
Door Identification and LocationDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-006-C01
2-7-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-1 Forward Passenger / Crew Doors
**ON A/C A330-200 A330-200F A330-300
Forward Passenger / Crew Door
1. This section gives forward passenger / crew doors clearances.
2-7-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
CRITICALCLEARANCELIMIT
CL
CL
CL
2.43 m(7 ft 11 in)
0.64 m(2 ft 1 in)
1.07 m(3 ft 6 in)
0.75 m(2 ft 5 in)
5.85 m(19 ft 2 in) 3.00 m
(9 ft 10 in)
1.93 m(6 ft 3 in)
SEECHAPTER
2−3
(10 ft 9 in)3.3 m
G_AC_020701_0_F00AAM0_05_00
0.045 m
(1.77 in)
F_AC_020701_1_0010101_01_00
Forward Passenger / Crew DoorsFIGURE-2-7-1-991-001-A01
2-7-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
CRITICALCLEARANCELIMIT
CL
CL
CL
2.43 m(7 ft 11 in)
0.64 m(2 ft 1 in)
1.07 m(3 ft 6 in)
0.75 m(2 ft 5 in)
5.85 m(19 ft 2 in) 3.00 m
(9 ft 10 in)
1.93 m(6 ft 3 in)
SEECHAPTER
2−3
(10 ft 9 in)3.3 m
0.045 m
(1.77 in)
F_AC_020701_1_0020101_01_00
Forward Passenger / Crew DoorsFIGURE-2-7-1-991-002-A01
2-7-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-2 Mid Passenger / Crew Doors
**ON A/C A330-200 A330-300
Mid Passenger / Crew Door
1. This section gives mid passenger / crew doors clearances.
2-7-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
(TOP OF FLOOR)
CL
CL
CL
(FROM NOSE)
0.75 m(2 ft 5 in)
1.07 m(3 ft 6 in)
2.43 m(7 ft 11 in)
A330−200: 14.561 m (47ft 9 in)
A330−300: 17.741 m (58 ft 2 in)
0.64 m(2 ft 1 in)
3.41 m(11 ft 2 in)
(6 ft 3 in)
SEECHAPTER
2−3
1.93 m
A
A
A AF_AC_020702_1_0010101_01_00
(1.77 in)0.045 m
Mid Passenger / Crew DoorFIGURE-2-7-2-991-001-A01
2-7-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-3 Emergency Exits
**ON A/C A330-200 A330-300
Emergency Exits
1. This section gives emergency exits doors clearances.
2-7-3Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
CL
(TOP OF FLOOR)
CL
CL
0.75 m(2 ft 5 in)
1.07 m(3 ft 6 in)
3.2 m(10 ft 5 in)
0.64 m(2 ft 1 in)
(FROM NOSE)A330−200: 32.767 m (107 ft 6 in)
A330−300: 35.961 m (117 ft 11 in)
1.66 m(5 ft 5 in)
2−3
SEECHAPTER
A A
A
A
F_AC_020703_1_0010101_01_00
2.43 m(7 ft 11 in)
0.03 m(1.18 in)
Emergency ExitsFIGURE-2-7-3-991-001-A01
2-7-3Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-4 Aft Passenger / Crew Doors
**ON A/C A330-200 A330-300
Aft Passenger / Crew Doors
1. This section gives Aft passenger / crew doors clearances.
2-7-4Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
CRITICALCLEARANCE
LIMIT
CL
CL CL
CL
2.43 m(8 ft)
1.07 m(3 ft 6 in)
0.75 m(2 ft 5 in)
3 m(9 ft 10 in)
1.99 m(6 ft 6 in)
0.64 m(2 ft 1 in)
A330−200: 45.628 m (149 ft 8 in)
A330−300: 50.956 m (167 ft 2 in)
(FROMNOSE)
SEECHAPTER
2−3
A A
A
A
F_AC_020704_1_0010101_01_00
0.045 m(1.8 in)
Aft Passenger / Crew DoorsFIGURE-2-7-4-991-001-A01
2-7-4Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-5 Forward Cargo Compartment Doors
**ON A/C A330-200 A330-300
Forward Cargo Compartment Doors
1. This section gives forward cargo compartment doors clearances for pax version.
2-7-5Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
(FROM NOSE)
CL
CL
CL
SEECHAPTER
2−3
CL
9.53 m(31 ft 3 in)
0.64 m(2 ft 1 in)
6.37 m(20 ft 10 in)
2.7 m(8 ft 10 in)
1.70 m(5 ft 6 in)
2.04 m(6 ft 8 in)
5.27 m(17 ft 3 in)
MID PASSENGER/CREW DOOR CREW DOORFORWARD PASSENGER/
A A
A
A
F_AC_020705_1_0010101_01_00
FORWARD CARGOCOMPARTMENT DOOR
Forward Cargo Compartment DoorsFIGURE-2-7-5-991-001-A01
2-7-5Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Forward Cargo Compartment Doors
1. This section gives forward cargo compartment doors clearances for cargo version.
2-7-5Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
CL
CL
SEECHAPTER
2−3
CL
1.70 m(5 ft 6 in)
2.04 m(6 ft 8 in)
5.27 m(17 ft 3 in)
FORWARD CARGOCOMPARTMENT DOOR
9.53 m (31 ft 3 in) (FROM NOSE)
CREW DOORFORWARD
A A
2.7 m(8 ft 10 in)
A
A
FWD
F_AC_020705_1_0020101_01_01
Forward Cargo Compartment DoorsFIGURE-2-7-5-991-002-A01
2-7-5Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
PW= 8.45 m (27 ft 8 in)RR= 8.13 m (26 ft 8 in)
9.92m(32 ft 6 in)
2.44 m(8 ft 1 in)
2.58 m(8 ft 5.5 in)
3.36 m(11 ft)
4.6 m(15 ft 1 in)
PW= 18.253 m (59 ft 10 in)RR= 18.081 m (59 ft 3 in)
(FROM NOSE)
(FROM NOSE)
CL
SEECHAPTER
2−3
3.69 m(12 ft 1.2 in)
4.07 m(13 ft 1 in)
A
A
A AF_AC_020705_1_0030101_01_01
Forward Cargo Compartment DoorsFIGURE-2-7-5-991-003-A01
2-7-5Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-6 Aft Cargo Compartment Doors
**ON A/C A330-200 A330-200F A330-300
Aft Cargo Compartment Doors
1. This section gives Aft cargo compartment doors clearances.
2-7-6Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
SEECHAPTER
2−3
1.68 m(5 ft 6 in)
2.03 m(6 ft 7 in)
5.19 m(17 ft)
(FROM NOSE)A330−200: 38.978 m(127 ft 10 in)
AFT CARGO COMPARTMENT DOOR
(9 ft 1in)2.78 m
AFT PASSENGER/CREW DOOR
CL
CL
CL
CL
A A
A
A
BULK CARGOCOMPARTMENT DOOR
F_AC_020706_1_0010101_01_01
Aft Cargo Compartment DoorsFIGURE-2-7-6-991-001-A01
2-7-6Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
SEECHAPTER
2−3
1.68 m(5 ft 6 in)
2.03 m(6 ft 7 in)
5.19 m(17 ft)
(FROM NOSE)A330−300: 44.36 m(145 ft 6 in)
AFT CARGO COMPARTMENT DOOR
(9 ft 1in)2.78 m
AFT PASSENGER/CREW DOOR
CL
CL
CL
CL
A A
A
A
BULK CARGOCOMPARTMENT DOOR
F_AC_020706_1_0030101_01_00
Aft Cargo Compartment DoorsFIGURE-2-7-6-991-003-A01
2-7-6Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
SEECHAPTER
2−3
1.68 m(5 ft 6 in)
2.03 m(6 ft 7 in)
5.19 m(17 ft)
(FROM NOSE)
A330−200F: 38.978 m (127 ft 10 in)
AFT CARGO COMPARTMENT DOOR
(9 ft 1in)2.78 m
CL
CL
CL
CL
A A
A
A
BULK CARGOCOMPARTMENT DOOR
F_AC_020706_1_0020101_01_01
Aft Cargo Compartment DoorsFIGURE-2-7-6-991-002-A01
2-7-6Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-7 Bulk Cargo Compartment Doors
**ON A/C A330-200 A330-300
Bulk Cargo Compartment Doors
1. This section gives the bulk cargo compartment doors clearances for pax version.
2-7-7Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
CL
CL
CL
SEECHAPTER
2−3
CL
1.11 m(3 ft 7 in)
0.95 m(3 ft 1 in)
1.41 m(4 ft 7 in)
1.07 m(3 ft 6 in)
(FROM NOSE)A330−200: 42.014 m (137 ft 10 in)
A330−300: 47.342 m (155 ft 3 in)
AFT PASSENGER/CREW DOOR(REF)
AFT CARGO COMPARTMENT DOOR
A
A
BULK CARGOCOMPARTMENT DOOR
A A
F_AC_020707_1_0010101_01_00
Bulk Cargo Compartment DoorsFIGURE-2-7-7-991-001-A01
2-7-7Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Bulk Cargo Compartment Doors
1. This section gives the bulk cargo compartment doors clearances for cargo version.
2-7-7Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
(FROM NOSE)A330−200F: 42.014 m (137 ft 10 in)
CL
SEECHAPTER
2−3
0.95 m(3 ft 1 in)
1.11 m(3 ft 7 in)
FWD
A
A
BULK CARGOCOMPARTMENT DOOR
AFT CARGOCOMPARTMENT DOOR
CL
CL
1.41 m(4 ft 7 in)
1.07 m(3 ft 6 in)
A A
F_AC_020707_1_0020101_01_00
Bulk Cargo Compartment DoorsFIGURE-2-7-7-991-002-A01
2-7-7Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-8 Main and Center Landing Gear Doors
**ON A/C A330-200 A330-300
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances for pax version.
2-7-8Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
A
A
GROUND LINE
A/C
C L
81°
3.96 m(13 ft)
1.56 m(5 ft 1 in)
Z−2 m (6 ft 6 in)
3.03 m(9 ft 11in)
2.34 m(7 ft 8 in)
1.1 m(3 ft 7 in)
2.7 m(8 ft 10 in)
A330−200: 26.786 m (87 ft 10 in)
A330−300: 29.45 m (96 ft 7 in)
0.23 m(9 in)
F_AC_020708_1_0010101_01_00
Main Landing Gear DoorsFIGURE-2-7-8-991-001-A01
2-7-8Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances for cargo version.
2-7-8Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
A330−200F: 26.786 m (87 ft10 in) 3.96 m(13 ft)
GROUND LINE
A/C
C L
81°
1.56 m(5 ft 1 in)
Z−2 m (6 ft 6 in)
3.03 m(9 ft 11in)
2.34 m(7 ft 8 in)
1.1 m(3 ft 7 in)
2.7 m(8 ft 10 in)
0.23 m(9 in)
A
A
F_AC_020708_1_0020101_01_00
Main Landing Gear DoorsFIGURE-2-7-8-991-002-A01
2-7-8Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-9 Radome
**ON A/C A330-200 A330-200F A330-300
Radome
1. This section gives the radome clearances.
2-7-9Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
67°
CL
STA 7662.5FR1
1.32
5 m
(4 ft
4 in
)1.
25 m
(4 ft
1 in
)
1.65 m(5 ft 4 in)
F_AC_020709_1_0010101_01_00
RadomeFIGURE-2-7-9-991-001-A01
2-7-9Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-10 APU and Nose Landing Gear Doors
**ON A/C A330-200 A330-300
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances for pax version.
2-7-10Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
FUSELAGE DATUM LINE
FR95
FR101
5.83
m(1
9 ft
1 in
)
6.55
m(2
1 ft
5 in
)
1.82
m(5
ft 1
1 in
)
1.49 m(4 ft 10 in)
F_AC_020710_1_0010101_01_00
APU and Nose Landing Gear DoorsFIGURE-2-7-10-991-001-A01
2-7-10Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances for cargo version.
2-7-10Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
FUSELAGE DATUM LINE
FR95
FR101
5.83
m(1
9 ft
1 in
)
6.55
m(2
1 ft
5 in
)
1.38 m(4 ft 6 in)
2.00
m(6
ft 6
in)
FWD
F_AC_020710_1_0020101_01_00
APU and Nose Landing Gear DoorsFIGURE-2-7-10-991-002-A01
2-7-10Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0 Escape Slides
**ON A/C A330-200 A330-200F A330-300
Escape Slides
1. GeneralThis section gives the location of the cabin escape facilities and their related clearances.
**ON A/C A330-200 A330-300
2. LocationEscape facilities are provided at the following locations:
A. Door Escape Facility- One dual lane escape slide-raft at each passenger/crew door (total six)- One single lane escape slide-raft at each emergency exit door (total two).The slides are installed in a container in the lower part of the door.
**ON A/C A330-200F
3. LocationEscape facilities are provided at the following locations:
A. Door Escape Facility- One dual lane escape slide-raft at each FWD cabin door (total two).The slides are installed in a container in the lower part of the door.
2-8-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
FWD CABIN ESCAPE SLIDE
MID CABIN ESCAPE SLIDE
EMERGENCY EXIT
AFT CABIN
ESCAPE SLIDE
ESCAPE SLIDE
F_AC_020800_1_0010101_01_00
Escape SlidesLocation (Sheet 1 of 2)
FIGURE-2-8-0-991-001-A01
2-8-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
GR
ID E
QU
ALS
1 m
(3.
28 ft
) IN
RE
ALI
TY
EM
ER
GE
NC
Y D
ES
CE
NT
DE
VIC
ET
HR
OU
GH
WIN
DO
W O
PE
NIN
G
0 −3
−6 −9
−12
−15 −21
−18
−24
−27
−30 −33
F_AC_020800_1_0010108_01_00
Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-001-A01
2-8-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
CABIN ESCAPE SLIDE
F_AC_020800_1_0010201_01_00
Escape SlidesLocation (Sheet 1 of 2)
FIGURE-2-8-0-991-001-B01
2-8-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
GR
ID E
QU
ALS
1 m
(3.
28 ft
) IN
RE
ALI
TY
EM
ER
GE
NC
Y D
ES
CE
NT
DE
VIC
ET
HR
OU
GH
WIN
DO
W O
PE
NIN
G
0 −3
−6 −9
−12
−15 −21
−18
−24
−27
−30 −33
F_AC_020800_1_0010202_01_00
Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-001-B01
2-8-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
EMERGENCY EXITESCAPE SLIDE
FWD CABIN ESCAPE SLIDE
MID CABIN ESCAPE SLIDE
AFT CABINESCAPE SLIDE
F_AC_020800_1_0010301_01_00
Escape SlidesLocation (Sheet 1 of 2)
FIGURE-2-8-0-991-001-C01
2-8-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
GR
ID E
QU
ALS
1 m
(3.
28 ft
) IN
RE
ALI
TY
EM
ER
GE
NC
Y D
ES
CE
NT
DE
VIC
ET
HR
OU
GH
WIN
DO
W O
PE
NIN
G
0 −3
−6 −9
−12
−15 −21
−18
−24
−27
−30 −33
F_AC_020800_1_0010304_01_00
Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-001-C01
2-8-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0 Landing Gear
**ON A/C A330-200 A330-200F A330-300
Landing Gear Maintenance Pits
1. GeneralThe minimum maintenance pit envelopes for the main landing gear shock absorber removal are shownin Figures 1 and 2.
All dimensions shown are minimum dimensions with zero clearances.
The dimensions for the pits have been determined for these design factors:- The length and width of the pits allow the gear to rotate as the weight is taken off the landing
gear- The depth of the pits allow the shock absorber to be removed when all the weight is taken off the
landing gear.
Dimensions for elevators and associated mechanisms must be added to those in Figures 1 and 2.
A. ElevatorsThese can be either mechanical or hydraulic. Elevators are used to:- permit easy movement of persons and equipment around the main landing gears- lift and remove the landing gear assemblies out of the pits.
B. JackingThe aircraft must be in position over the pits to put the gear on the elevators. Jacks must beinstalled and engaged with all the jacking points (Ref. Section 2-14 for Jacking).Jacks must support the total aircraft weight i.e. when the landing gears do not touch theelevators on retraction/extension tests.When tripod support jacks are used, the tripod-base circle radius must be limited because thelocations required for positioning the jacks are close to the sides of the pits.
2-9-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
3.58
m(1
1.75
ft)
8.51
m(2
7.92
ft)
3.89
m(1
2.76
ft)
6.31
m(2
0.7
ft)
5.34
m(1
7.52
ft)
34.3
1 m
(112
.57
ft)
31.5
5 m
(103
.51
ft)
25.3
8 m
(83.
27 ft
)
3.65
m(1
1.98
ft)
FR
ON
T O
F N
OS
E R
AD
OM
E
FO
RW
AR
D J
AC
KIN
G P
OIN
T
WIN
G J
AC
KIN
G P
OIN
T
AIR
CR
AF
T C
EN
TE
R L
INE
NO
TE
:E
NV
ELO
PE
S S
HO
WN
WIT
H Z
ER
O C
LEA
RA
NC
E T
O O
UT
SID
E E
DG
E O
F T
IRE
S.
WIN
G J
AC
KIN
G P
OIN
T
F_AC_020900_1_0010101_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 1 of 2)
FIGURE-2-9-0-991-001-A01
2-9-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
3. ’C
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E D
EF
LAT
ED
AN
DC
OM
PR
ES
SE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
4. ’D
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E E
XT
EN
DE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
DIM
EN
SIO
NS
mm
ftft
6.53
m(2
1.42
ft)
1.53
5.02
0.2
0.6
60.
812.
66
mft
FU
SE
LAG
E H
OR
IZO
NT
AL
DA
TU
M
(103
.02
ft)31
.4 m
33.1
3 m
(108
.69
ft)
FR
ON
T O
F N
OS
E R
AD
OM
EAB
C
BC
D
mft
A
1.56
5.12
1. ’A
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
NLG
WH
EE
LA
BO
VE
ST
AT
IC G
RO
UN
D L
INE
WIT
H A
IRC
RA
FT
LEV
ELL
ED
AN
D J
AC
KE
D.
A P
IT IS
NO
T R
EQ
UIR
ED
FO
R T
HE
NLG
.
2. ’B
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
LO
WE
ST
MLG
MA
IN W
HE
EL
AB
OV
E S
TA
TIC
GR
OU
ND
LIN
EW
ITH
AIR
CR
AF
T J
AC
KE
D IN
TO
PO
SIT
ION
AB
OV
E H
YD
RA
ULI
C O
R M
EC
HA
NIC
AL
ELE
VA
TO
R,
FO
R R
ET
RA
CT
ION
/EX
TE
NS
ION
TE
ST
S.
6.67
m(2
1.88
ft)
NO
TE
:D
MA
IN L
AN
DIN
G G
EA
R
F_AC_020900_1_0010104_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 2 of 2)
FIGURE-2-9-0-991-001-A01
2-9-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
FR
ON
T O
F N
OS
E R
AD
OM
E
FO
RW
AR
D J
AC
KIN
G P
OIN
T
WIN
G J
AC
KIN
G P
OIN
T
AIR
CR
AF
T C
EN
TE
R L
INE
WIN
G J
AC
KIN
G P
OIN
T28
.35
m(9
3.01
ft)
3.58
m(1
1.75
ft)
8.51
m(2
7.92
ft)
3.89
m(1
2.76
ft)
6.31
m(2
0.7
ft)
5.34
m(1
7.52
ft)
31.1
2 m
(102
.1 ft
)22.1
8 m
(72.
77 ft
)
3.65
m(1
1.98
ft)
NO
TE
:E
NV
ELO
PE
S S
HO
WN
WIT
H Z
ER
O C
LEA
RA
NC
E T
O O
UT
SID
E E
DG
E O
F T
IRE
S.
F_AC_020900_1_0010301_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 1 of 2)
FIGURE-2-9-0-991-001-C01
2-9-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
3. ’C
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E D
EF
LAT
ED
AN
DC
OM
PR
ES
SE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
4. ’D
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E E
XT
EN
DE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
FU
SE
LAG
E H
OR
IZO
NT
AL
DA
TU
M
FR
ON
T O
F N
OS
E R
AD
OM
EAB
C
1. ’A
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
NLG
WH
EE
LA
BO
VE
ST
AT
IC G
RO
UN
D L
INE
WIT
H A
IRC
RA
FT
LEV
ELL
ED
AN
D J
AC
KE
D.
A P
IT IS
NO
T R
EQ
UIR
ED
FO
R T
HE
NLG
.
2. ’B
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
LO
WE
ST
MLG
MA
IN W
HE
EL
AB
OV
E S
TA
TIC
GR
OU
ND
LIN
EW
ITH
AIR
CR
AF
T J
AC
KE
D IN
TO
PO
SIT
ION
AB
OV
E H
YD
RA
ULI
C O
R M
EC
HA
NIC
AL
ELE
VA
TO
R,
FO
R R
ET
RA
CT
ION
/EX
TE
NS
ION
TE
ST
S.
6.67
m(2
1.88
ft)
NO
TE
:D
6.53
m(2
1.42
ft)
(92.
36 ft
)28
.15
m
29.3
4 m
(96.
26 ft
)
DIM
EN
SIO
NS
mm
ftft
1.53
5.02
0.2
0.6
60.
812.
66
mft
BC
D
mft
A
1.56
5.12
MA
IN L
AN
DIN
G G
EA
R
F_AC_020900_1_0010302_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 2 of 2)
FIGURE-2-9-0-991-001-C01
2-9-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
Landing Gear
1. General
The aircraft has:- Two Main Landing Gears (MLG) with four wheel bogie assembly and related doors- A Nose Landing Gear (NLG) with twin wheel assembly and related doors.The Main Landing Gears are located under each wing and retract sideways towards the fuselagecenterline.The Nose Landing Gear retracts forward into a fuselage compartment below the cockpit.The retraction and extension of the landing gears and landing gear doors are operated hydraulicallyand mechanically. The control, sequence and indication are electrical.In abnormal operation, the landing gears can be extended by gravity.
For the dimensions of the landing gear footprint and tire size, refer to 7-2-0.
2. Main Landing Gear and Doors
Each Main Landing Gear has a leg assembly and a four-wheel bogie beam. The MLG leg includes ashortening mechanism, a bogie pitch trimmer and an oleo-pneumatic shock absorber. In flight, withthe MLG extended, the bogie is held in a trailing condition (rear wheels low) by an articulationlinkage and a pitch trimmer. The folding sidestay is locked mechanically by a lockstay (which isoperated by the downlock actuator) when the MLG is fully extended.
Each MLG bay has the following doors:- A hydraulically-operated main door- A mechanically-operated hinged door- A fairing door on the MLG leg.
All the doors close when the MLG retracts. When the MLG is extended the main door closes and thehinged door stays open. A manually operated mechanism (for maintenance personnel) lets the maindoors be opened for access to the MLG bay when the aircraft is on the ground.
3. Nose Landing Gear and Doors
The NLG includes a twin-wheel axle assembly and an oleo-pneumatic shock absorber. The NLG issupported longitudinally by a two-piece dragstay. The dragstay is locked mechanically by the locklinks when the NLG is fully extended.
Each NLG bay has the following doors:- Two hydraulically-operated FWD doors- Two mechanically-operated AFT doors- A fixed fairing door on the NLG leg.
2-9-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
All the doors close when the NLG retracts. When the NLG is extended the FWD doors close and theAFT doors stay open. A door opening mechanism lets the FWD doors be opened on the ground foraccess to the NLG bay.
4. Nose Wheel Steering
Nose wheel steering system is a computer controlled electro-hydraulic system. The system uses theGreen main hydraulic power system to operate the hydraulic components.The steering is controlled by two hand wheel transmitters in the cockpit, which supply the primarysteering inputs to the BSCU (Brake and Steering Control Unit ).A steering disconnection box is installed on the NLG to disconnect the steering for towing.
For the operation and control of nose wheel steering, refer to AMM 32-51-00.For the steering angle limits, refer to AMM 09-10-00.
5. Landing Gear Servicing Points
A. GeneralFluid filling and gas charging of the MLG and NLG shock absorbers are accomplished throughMS28889 standard valves.
B. Charging PressuresFor charging of the landing gear shock absorbers, refer to AMM 12-14-32.
6. Landing Gear Control
The landing gear and door operation is controlled electrically by one of the two Landing Gear Controland Interface Units (LGCIU). Control changes from one LGCIU to the other after each extensioncycle.In normal operation, the landing gears and doors are operated by the Green hydraulic system.In abnormal operation, the landing gears can be extended by the operation of electro-mechanical free-fall system. The related electrical switches in the cockpit disengages the doors and the landing gearuplocks. The landing gears then extend by free-fall and the downlock links of each landing gear (L/G)are locked in position by springs.
7. Braking
A. GeneralCarbon multi-disc brakes are installed on each wheel of the MLG. Each brake assembly has twowear indicators installed.
The braking system has four braking modes with autobrake and anti-skid systems:- Normal braking with anti-skid.- Alternate braking with anti-skid.- Alternate braking without anti-skid.- Parking brake with full brake pressure.
2-9-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B. In-Flight Wheel BrakingBraking occurs automatically during the retraction of the landing gears. This stops the rotationof the MLG wheels before the landing gears go into their related bays.
8. Tire Pressure Indicating System (TPIS)
The TPIS automatically monitors the tire pressures and shows these values on Test Equipment(BITE) and also supplies other data and warnings on the WHEEL page of the System Display (SD).
9. Built In Test Equipment (BITE)
The BITE has hardware and software for these functions:- to automatically do a self test at power-up- to continuously monitor the related systems for failures- to continuously monitor the interface with other specified systems in the aircraft- to keep a record of each failure and defect and send this data to other systems in the aircraft- to automatically do a functional test of some related systems before a landing- to do specified system tests during ground maintenance.
The BITE for the following systems is described in these chapters:- The Brakes and Steering AMM 32-46-00- The TPIS AMM 32-49-00- The Landing GearAMM 32-69-00.
2-9-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
MAIN DOOR
HINGED DOOR
FIXED FAIRING DOOR
A
B
C
D
F
E
DOWNLOCKACTUATOR
SHORTENINGMECHANISM
SIDE STAYASSEMBLY MLG LEG
ASSEMBLY
TORQUE LINKS
BOGIE PITCHTRIMMER
BOGIE BEAMASSEMBLY
SHOCK ABSORBER
ARTICULATING LINKS
RADIAL OR BIASPLY TIRES
A
(HYDRAULICALLYOPERATED)
FWD AXLE
AFT AXLE
BRAKE RODASSEMBLY
F_AC_020900_1_0070101_01_00
Main Landing GearGeneral (Sheet 1 of 3)
FIGURE-2-9-0-991-007-A01
2-9-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
C
WARNING FLAG
GROUND LOCK PIN
LOCK STAY
BLH SHOWN
RH SYMMETRICAL
QUICK RELEASE PIN
SAFETYCOLLAR
WARNING FLAG
WARNING FLAG
QUICK RELEASE PIN
DOOR ACTUATOR
F_AC_020900_1_0070102_01_00
Main Landing GearSafety Devices (Sheet 2 of 3)FIGURE-2-9-0-991-007-A01
2-9-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
SEAL CHANGEOVERVALVE
BLEED/INFLATIONVALVE
D
E
F
FWD
FILL VALVE
GROUND POINT
F_AC_020900_1_0070103_01_00
Main Landing GearServicing (Sheet 3 of 3)
FIGURE-2-9-0-991-007-A01
2-9-0Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
RETRACTION ACTUATOR
DOWNLOCKACTUATOR
MAIN FITTING
DOWNLOCK SPRINGS
TORQUE LINKS
RADIAL OR BIASPLY TIRES
TOWING BRACKET
SHOCK ABSORBER
AXLE
NWS ACTUATORS
LOWER DRAGSTAY(FOLDING STRUT)
UPPER DRAGSTAY(FOLDING STRUT)
EH
D
AFT DOOR(MECHANICALLY OPERATED)
FWD DOORS
A
(HYDRAULICALLY
AFT DOOR(MECHANICALLY OPERATED)
FIXED FAIRING
A
C
F
G
OPERATED)
B
B
F_AC_020900_1_0080101_01_00
Nose Landing GearGeneral (Sheet 1 of 4)
FIGURE-2-9-0-991-008-A01
2-9-0Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
DRAG STAYATTACHMENT
GROUNDLOCK PIN
LOCK SPRINGATTACHMENT
LOWERLOCK−LINK
UPPERLOCK−LINK
DOWN LOCKACTUATOR
ATTACHMENT
WARNING FLAG
C
BRH SHOWN
LH SYMMETRICAL
SAFETYCOLLAR
QUICK RELEASE PIN
WARNING FLAG
WARNING FLAG
QUICK RELEASE PIN
DOOR ACTUATOR
F_AC_020900_1_0080102_01_00
Nose Landing GearSafety Devices (Sheet 2 of 4)FIGURE-2-9-0-991-008-A01
2-9-0Page 13
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
SEAL CHANGEOVERVALVE
CHARGE VALVE
BLEED VALVE
E
D
INFLATION VALVE(FIRST STAGE)
FWD
F_AC_020900_1_0080103_01_00
Nose Landing GearServicing (Sheet 3 of 4)
FIGURE-2-9-0-991-008-A01
2-9-0Page 14
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
INFLATION VALVE(SECOND STAGE)
LANDING GEAR
GROUND POINT
FWD
F
TOWING LEVER
SAFETY PIN(TOWING POSITION)
WARNING FLAG
NORMAL POSITION(NOSE WHEEL STEERING
OPERATIONAL)
TOWING POSITION(NOSE WHEEL STEERING
DEACTIVATED)
G
H
F_AC_020900_1_0080104_01_00
Nose Landing GearServicing and Steering Disconnection Box (Sheet 4 of 4)
FIGURE-2-9-0-991-008-A01
2-9-0Page 15
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0 Exterior Lighting
**ON A/C A330-200 A330-200F A330-300
Exterior Lighting
1. GeneralThis section gives the location of the aircraft exterior lighting.
EXTERIOR LIGHTINGITEM DESCRIPTION
1 RIGHT NAVIGATION LIGHT (GREEN)
2 LEFT NAVIGATION LIGHT (RED)
3 TAIL NAVIGATION LIGHT (WHITE)
4 UPPER ANTI-COLLISION LIGHT/BEACON(RED)
5 LOWER ANTI-COLLISION LIGHT/BEACON(RED)
6 LOGO LIGHTS7 ENGINE SCAN LIGHTS8 WING SCAN LIGHTS9 WING STROBE LIGHT (HIGH INTENSITY,
WHITE)
10 TAIL STROBE LIGHT (HIGH INTENSITY,WHITE)
11 LANDING LIGHTS12 RUNWAY TURN-OFF LIGHTS13 TAXI LIGHTS14 TAKE-OFF LIGHTS15 CARGO COMPARTMENT FLOOD LIGHTS16 LANDING GEAR BAY/WELL LIGHTS (DOME)
17 (A330-200F only) CARGO COMPARTMENT FLOOD LIGHTS -MAIN DECK
2-10-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
1 RH
2 LH
98 7
46
5
10
3
F_AC_021000_1_0010101_01_00
Exterior Lighting(Sheet 1 of 5)
FIGURE-2-10-0-991-001-A01
2-10-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
14
13 12 11
NOTE:LIGHTS 13 AND 14 ARE THE SAME, BUT THEY OPERATE WITH DIFFERENT POWER SETTINGS.
F_AC_021000_1_0010102_01_00
Exterior Lighting(Sheet 2 of 5)
FIGURE-2-10-0-991-001-A01
2-10-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
21
7 7
1212
13
14
3
F_AC_021000_1_0010103_01_00
Exterior Lighting(Sheet 3 of 5)
FIGURE-2-10-0-991-001-A01
2-10-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
10
99
54
8
1111
8
F_AC_021000_1_0010104_01_00
Exterior Lighting(Sheet 4 of 5)
FIGURE-2-10-0-991-001-A01
2-10-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
15 16 15 16
6
6
F_AC_021000_1_0010105_01_00
Exterior Lighting(Sheet 5 of 5)
FIGURE-2-10-0-991-001-A01
2-10-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
1 RH
2 LH
6
10
3
5
78
4
9
F_AC_021000_1_0020101_01_00
Exterior Lighting(Sheet 1 of 6)
FIGURE-2-10-0-991-002-A01
2-10-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
14
1113 12
NOTE:LIGHTS 13 AND 14 ARE THE SAME, BUT THEY OPERATE WITH DIFFERENT POWER SETTINGS.
F_AC_021000_1_0020102_01_00
Exterior Lighting(Sheet 2 of 6)
FIGURE-2-10-0-991-002-A01
2-10-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
21
3
77
12 12
13
14
F_AC_021000_1_0020103_01_00
Exterior Lighting(Sheet 3 of 6)
FIGURE-2-10-0-991-002-A01
2-10-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
99
88
1111
10
4 5
F_AC_021000_1_0020104_01_00
Exterior Lighting(Sheet 4 of 6)
FIGURE-2-10-0-991-002-A01
2-10-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
6
6
15 16 15 16
F_AC_021000_1_0020105_01_00
Exterior Lighting(Sheet 5 of 6)
FIGURE-2-10-0-991-002-A01
2-10-0Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
HID LIGHT CEILING LIGHT
EXAMPLE FOR LIGHT N° 17
17
F_AC_021000_1_0020106_01_00
Exterior Lighting(Sheet 6 of 6)
FIGURE-2-10-0-991-002-A01
2-10-0Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
1 RH
LH
10
3
78
46
2
9
5
F_AC_021000_1_0030101_01_00
Exterior Lighting(Sheet 1 of 5)
FIGURE-2-10-0-991-003-A01
2-10-0Page 13
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
14
13 12 11
NOTE:LIGHTS 13 AND 14 ARE THE SAME, BUT THEY OPERATE WITH DIFFERENT POWER SETTINGS.
F_AC_021000_1_0030102_01_00
Exterior Lighting(Sheet 2 of 5)
FIGURE-2-10-0-991-003-A01
2-10-0Page 14
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
21
7
14
13
12
7
3
12
F_AC_021000_1_0030103_01_00
Exterior Lighting(Sheet 3 of 5)
FIGURE-2-10-0-991-003-A01
2-10-0Page 15
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
99
4 5
8
1111
8
10
F_AC_021000_1_0030104_01_00
Exterior Lighting(Sheet 4 of 5)
FIGURE-2-10-0-991-003-A01
2-10-0Page 16
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
6
6
15 16 15 16
F_AC_021000_1_0030105_01_00
Exterior Lighting(Sheet 5 of 5)
FIGURE-2-10-0-991-003-A01
2-10-0Page 17
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0 Antennas and Probes Location
**ON A/C A330-200 A330-200F A330-300
Antennas and Probes Location
1. This section gives the location of antennas and probes.
2-11-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
VH
F(3
)E
LT
AO
A S
EN
SO
R(1
)
WE
AT
HE
R R
AD
AR
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
LOC
RA
DIO
ALT
IME
TE
R(2
)
HF
RA
DIO
ALT
IME
TE
R(1
)G
LID
E
PIT
OT
PR
OB
E(1
)
PIT
OT
PR
OB
E(3
)
TA
T P
RO
BE
ICE
DE
TE
CT
OR
PR
OB
ET
CA
S B
OT
TO
M
DM
E(1
)
DM
E(2
)
MA
RK
ER
VH
F(4
)
GP
S(1
)
GP
S(2
)
TC
AS
TO
P
VH
F(1
)A
TC
(4) ST
AT
IC P
RO
BE
(2)
ST
AT
IC P
RO
BE
(1)
AT
C(1
)
F_AC_021100_1_0010101_01_00
Antennas and ProbesLocation (Sheet 1 of 2)
FIGURE-2-11-0-991-001-A01
2-11-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
AD
F(2
)A
DF
(1)
VO
R
TA
T P
RO
BE
ICE
DE
TE
CT
OR
PR
OB
E
ST
AT
IC P
RO
BE
(1)
ST
AT
IC P
RO
BE
(2)
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)A
OA
SE
NS
OR
(3)
ST
BY
AT
C(2
)
VH
F(2
)
AO
A S
EN
SO
R(2
)
PIT
OT
PR
OB
E(2
)
AT
C(3
)
SA
TC
OM
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0010102_01_00
Antennas and ProbesLocation (Sheet 2 of 2)
FIGURE-2-11-0-991-001-A01
2-11-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
GP
S(1
)
GP
S(2
)
TC
AS
TO
P
VH
F(1
)
VH
F(3
)E
LT
AO
A S
EN
SO
R(1
)
AT
C(4
)
WE
AT
HE
R R
AD
AR
ST
AT
IC P
RO
BE
(2)
ST
AT
IC P
RO
BE
(1)
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
AT
C(1
)
LOC
RA
DIO
ALT
IME
TE
R(2
)
RA
DIO
ALT
IME
TE
R(1
)
HF
GLI
DE
PIT
OT
PR
OB
E(1
)
PIT
OT
PR
OB
E(3
)
TA
T P
RO
BE
ICE
DE
TE
CT
OR
PR
OB
ET
CA
S B
OT
TO
M
DM
E(1
)
DM
E(2
)
MA
RK
ER
VH
F(4
)
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0020101_01_00
Antennas and ProbesLocation (Sheet 1 of 2)
FIGURE-2-11-0-991-002-A01
2-11-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
AD
F(2
)A
DF
(1)
TA
T P
RO
BE
ICE
DE
TE
CT
OR
PR
OB
E
ST
AT
IC P
RO
BE
(1)
ST
AT
IC P
RO
BE
(2)
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)A
OA
SE
NS
OR
(3)
ST
BY
AT
C(2
)
VH
F(2
)
VO
R
AO
A S
EN
SO
R(2
)
PIT
OT
PR
OB
E(2
)
AT
C(3
)
SA
TC
OM
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0020102_01_00
Antennas and ProbesLocation (Sheet 2 of 2)
FIGURE-2-11-0-991-002-A01
2-11-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
GP
S(1
)
GP
S(2
)
TC
AS
TO
P
VH
F(1
)
GP
S(2
)
AT
C(4
)
VH
F(3
)E
LT
WE
AT
HE
R R
AD
AR
GP
S(1
)
LOC
HF
ST
AT
IC P
RO
BE
(2)
ST
AT
IC P
RO
BE
(1)
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
AO
A S
EN
SO
R(1
)
MA
RK
ER
RA
DIO
ALT
IME
TE
R(2
)
RA
DIO
ALT
IME
TE
R(1
)
AT
C(1
)
PIT
OT
PR
OB
E(3
)
GLI
DE
PIT
OT
PR
OB
E(1
)
TA
T P
RO
BE
ICE
DE
TE
CT
OR
PR
OB
E
DM
E(1
)
DM
E(2
)
TC
AS
BO
TT
OM
VH
F(4
)
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0030101_01_00
Antennas and ProbesLocation (Sheet 1 of 2)
FIGURE-2-11-0-991-003-A01
2-11-0Page 6
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
AD
F(2
)A
DF
(1)
VO
R
VH
F(2
)
AO
A S
EN
SO
R(2
)
TA
T P
RO
BE
AT
C(3
)
PIT
OT
PR
OB
E(2
)S
AT
CO
M
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
ST
AT
IC P
RO
BE
(2)
ST
AT
IC P
RO
BE
(1)
ICE
DE
TE
CT
OR
PR
OB
E
AT
C(2
)
AO
A S
EN
SO
R(3
) S
TB
Y
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0030102_01_00
Antennas and ProbesLocation (Sheet 2 of 2)
FIGURE-2-11-0-991-003-A01
2-11-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0 Engine and Nacelle
**ON A/C A330-200 A330-200F A330-300
Engine and Nacelle
1. Engine and Nacelle - PW 4000 Engine
A. EngineThe PW 4000 engine is a two spool, axial flow, high bypass ratio turbofan engine.The engine has four major sections as follows:- The compressor section- The combustion section- The turbine section- The accessory drive section.
The compressor section has a six-stage low pressure compressor, a fan case, an intermediatecase and an eleven-stage high pressure compressor. The 1st stage rotor in the low pressurecompressor flows air through both the fan nozzle and the low compressor rotor/statorassemblies to the core of the engine. The high pressure compressor is used to increase thepressure of the primary airflow from the low compressor and send it to the diffuser.The engine combustion section comprises the diffuser case and a combustion chamber installedin the case. The chamber forms the enclosure where fuel is mixed with air and burned to addenergy to the primary gaspath.The turbine section comprises the rear compressor drive turbine, the front compressor driveturbine and the Turbine Exhaust Case (TEC). The rear compressor drive turbine is the two-stage High Pressure Turbine (HPT) and the front compressor drive turbine is the five-stage LowPressure Turbine (LPT). The HPT case assembly is air-cooled as part of the Turbine CaseCooling (TCC) system. The LPT rotor and stator assembly includes the front compressordriveshaft, the LPT case and the LPT spool case. The LPT case is externally cooled by turbinecase cooling tubes.The accessory drive section comprises the main gearbox and angle gearbox. The high pressurerotor is used to supply the main gearbox with power to drive the engine and aircraft-suppliedaccessories. Power comes from the towershaft in the intermediate case which is geared to thefront of the high pressure rotor. The towershaft drives the angle gearbox bevel gear set whichtransmits power through the horizontal driveshaft assembly to the main gearbox group.
B. NacelleThe nacelle is the aerodynamic structure around the basic engine. The nacelle provides asmooth airflow both around and into the engine to decrease drag and give better engineperformance and prevents damage to the external surface of the engine and its accessories. Thenacelle consists of the following major components:
2-12-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(1) Air Intake CowlThe air intake cowl is an interchangeable aerodynamic fairing assembly that permitssmooth airflow to the engine fan and core sections during ground and flight operation. Theair intake cowl is attached with bolts to the engine fan case.
(2) Fan CowlsFan cowls comprise a forward (fixed) fan cowl panel assembly and an aft fan cowl doorassembly. The fan cowl panels and doors protect the engine and its components, andoptimize the aerodynamic characteristics of the nacelle.
(3) Thrust ReverserThe thrust reverser system is a component of the aircraft engine nacelle and is used tocancel the forward thrust and to give aerodynamic braking of the aircraft. The principle ofthe thrust reverser is to procedure forward flow of the fan exhaust by a hydraulically-actuated mechanical system. The system is designed to be used on the ground only.
(4) Exhaust SystemThe turbine exhaust system has an exhaust nozzle and an exhaust plug. Both systemcomponents are acoustically treated and made to resist severe ambient conditions. Theexhaust nozzle forms the outer contour of the engine primary exhaust annulus and theinner flow path of the fan airstream. The exhaust plug forms the inner contour of theengine primary exhaust annulus. The exhaust nozzle and exhaust plug are line replaceableunits.
2. Engine and Nacelle - TRENT 700 Engine
A. EngineThe RB211-TRENT 700 engine is a high bypass ratio, triple spool turbofan.The principal modules of the engine are:- The Low Pressure Compressor (LPC) rotor- The Intermediate Pressure (IP) compressor- The intermediate case- The HP system (this includes the High Pressure Compressor (HPC), the combustion system
and the High Pressure Turbine (HPT))- The Intermediate Pressure Turbine (IPT)- The external gearbox- The LPC case- The Low Pressure Turbine (LPT).
2-12-0Page 2
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The compressor system has three axial flow compressors in a triple spool configuration. Thecompressors are turned independently by their related turbines, each at its most satisfactoryspeed. The LP system has a single-stage compressor installed at the front of the engine. A shaftconnects the compressor to a four-stage turbine at the rear of the gas generator. The gasgenerator also includes an eight-stage IP compressor, a six-stage HPC and a combustion system.Each of the compressors in the gas generator is connected to, and turned by, a different single-stage turbine. Between the HPC and the HPT is the annular combustion system which burns amixture of fuel and air to supply energy as heat. Behind the LPT there is a common nozzleassembly which mixes the cold air and hot gas exhaust flows. The external gearbox module isinstalled below the rear case of the fan case. It has a gear train that decreases and increases thespeed to meet the specified drive requirements of each accessory.
B. NacelleThe nacelle gives the engine an aerodynamic shape. Each engine is housed in a nacellesuspended from a pylon attached below the wing. The nacelle consists of the following majorcomponents:
(1) Air Intake CowlThe air intake cowl is attached to the forward flange of the front LPC case. Its function isto supply inlet air in a satisfactory condition for the engine compressors.
(2) Fan Cowl DoorsThe fan cowl doors hang on the aircraft wing pylon and are closed around the LPC cases.They can be opened during ground maintenance to give access to the components installedon the cases and to let the thrust reverser cowl doors be opened.
(3) Thrust ReverserThe thrust reverser is a component of the aircraft engine nacelle. The thrust reverser is atwin thrust reverser cowl door (’C’ duct) construction providing a fan duct inner wallfairing for the core engine between the top and bottom bifurcation walls. The thrustreverser incorporates hydraulically-powered actuators to operate four pivoting doors whichredirect the fan air flow in reverse thrust. Hydraulic power is provided from the aircrafthydraulic system to position the doors in a ”stowed” position for forward thrust and”deployed” position for reverse thrust.
(4) Common Nozzle Assembly (CNA)The CNA is attached to the aft flange of the exhaust case. The function of the CNA is tomix the core engine exhaust with the LPC outlet air.
**ON A/C A330-200 A330-300
3. Engine and Nacelle - GE CF6--80E1 Engine
A. EngineThe CF6-80E1 engine is a high bypass ratio, dual-rotor, axial-flow turbofan engine.The major modules of the engine are:- The fan module- The core module
2-12-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- The High Pressure Turbine (HPT)- The Low Pressure Turbine (LPT)- The accessory drive modules.
The fan module supplies approximately 80 percent of the total engine thrust throughsecondary air flow acceleration. The fan module also boosts primary air flow to the highpressure compressor. The fan rotor and booster assembly is part of the fan module. Air,taken in through the fan section, passes through successive stages of compressor rotorblades and compressor stator vanes, being compressed as it passes from stage to stage. Theinlet guide vanes and the first five-stages of the stator are variable, and change their angularposition as a function of the compressor inlet temperature and corrected engine speed. Thecombustion of fuel takes place in the combustor installed in the compressor rear frame. Thetwo main modules of the turbine are the HPT and the LPT. The function of the HPT is todrive the high pressure compressor by converting the combustor exhaust gas flow intomechanical force. The LPT subsequently also converts this flow into force to drive the fanand booster assemblies. The HPT rotor is a two-stage air-cooled turbine. The LPT rotordrives the fan and booster rotors through the LPT rotor shaft by extracting energy from thecombustion gases leaving the HPT. Power for both engine and aircraft accessories isextracted through a system of gearboxes and shafts. The accessory gearbox assembly ismounted on the compressor casing. The gearbox receives torque from the horizontal driveshaft and distributes the torque through spur gears to drive the gearbox-mountedaccessories.
B. NacelleThe nacelle provides protection for the engine and the engine accessories, and aerodynamicairflow around the engine during operation. Each engine is mounted in a nacelle suspended froma pylon attached to the wing lower surface. The nacelle consists of the following majorcomponents:
(1) Air Intake Cowl AssemblyThe air intake cowl structure is an interchangeable aerodynamically-faired assembly whichsupplies the inlet airflow to the fan and core sections of the engine. It is installed on theforward face of the engine fan case.
(2) Fan Cowl DoorsThe fan cowl door assemblies are engine-to-engine interchangeable units enclosing theengine fan case between the air intake cowl and thrust reverser cowl doors. Each assemblyis supported by three hinges at the pylon and latched along the bottom splitline with threetension hook latches.
(3) Thrust ReverserThe thrust reverser is a bifurcated assembly of two halves forming the fan exhaust ductand nozzle, enclosing the engine between the fan frame and the core cowling, andcontaining the mechanism for reversing the fan exhaust flow during aircraft landing.
2-12-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(4) Core Cowl DoorsThe core cowl door assemblies are interchangeable units which enclose the core enginebetween the thrust reverser cowl doors and the exhaust nozzle. Each assembly is hingedfrom the pylon in three locations and latched along the bottom splitline with three tensionhook latches.
(5) Exhaust NozzleThe exhaust nozzle, through which all exhaust gases are expelled, is part of theaerodynamically-structured nacelle. The exhaust nozzle provides a fixed area annulus forexhausting the core engine gas stream flow and provides a continuation of the aerodynamiccowling from the core cowl interface.
2-12-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
A
TURBINEEXHAUST
CASE
TURBINESECTION
COMBUSTIONSECTION
LOW PRESSURECOMPRESSOR
HIGH PRESSURECOMPRESSOR
COMPRESSORSECTION
TURBINE LOW PRESSURE
HIGHPRESSURE
TURBINE
SECTIONACCESSORY DRIVE
4.14 m(13.58 ft)
2.72 m(8.92 ft)
NOTE:APPROXIMATE DIMENSIONS.
0.83 m(2.72 ft)
2.26 m(7.41 ft)
2.54 m(8.33 ft)
4.29 m(14.07 ft)
A
1.98 m(6.5 ft)
FWD
F_AC_021200_1_0010101_01_00
Engine and NacelleEngine Dimensions - PW 4000FIGURE-2-12-0-991-001-A01
2-12-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
W
U
V
U = VW = U + V
A−A
B−B
C−C
D−D
E−E
F−F
W U V NAC STA
(10.24 ft)3.12 m
(5.12 ft)1.56 m
(5.12 ft)1.56 m
(2.92 ft)0.89 m
(5.87 ft)1.79 m
(5.18 ft)1.58 m
(5.18 ft)1.58 m
(10.37 ft)3.16 m
(10.04 ft)3.06 m
(5.02 ft)1.53 m
(5.02 ft)1.53 m
(8.6 ft)2.62 m
(15.16 ft) *4.62 m
(4.23 ft)1.29 m
(4.23 ft)1.29 m
(8.46 ft)2.58 m
(4.66 ft)1.42 m
(2.33 ft)0.71 m
(2.33 ft)0.71 m
(17.16 ft)5.23 m
(3.28 ft)1 m
(1.64 ft)0.5 m
(1.64 ft)0.5 m
(19.91 ft)6.07 m
*
(20.24 ft)6.17 m(2.92 ft)
0.89 m
INTAKECOWL
(3.25 ft)0.99 m
FAN COWL
(5.68 ft)1.73 m
THRUST REVERSER
(8.53 ft)2.6 m
EXHAUST
(2.76 ft)0.84 m
4°
STOWED POSITION
F
FE
E
D
DC
CB
B
A
A
NOZZLE
NOTE:APPROXIMATE DIMENSIONS.
DISTANCEFROM NOSE
A330−200/A330−200FA330−300
A (70.37 ft)21.45 m
(59.88 ft)18.25 m
A
(7.81 ft)2.38 m
F_AC_021200_1_0020101_01_00
Engine and NacelleNacelle Dimensions - PW 4000FIGURE-2-12-0-991-002-A01
2-12-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
GROUND
CLOSED
WL 100
(5.87 ft)1.79 m
(2.36 ft)0.72 m
53.8°
(19.32 ft)5.89 m
NOTE:APPROXIMATE DIMENSIONS.
WL 100
(10.33 ft)3.15 m
F_AC_021200_1_0030101_01_00
Engine and NacelleFan Cowls - PW 4000
FIGURE-2-12-0-991-003-A01
2-12-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
GROUND
48°
(17.68 ft)5.39 m
1.55 m(5.09 ft)
3.15 m(10.33 ft)
CLOSED
WL 100
WL 100
CAUTION:DO NOT ACTUATE SLATS WITH THRUST REVERSERCOWLS AT 48° OPEN POSITION.
NOTE:
VIEW ON REAR OFENGINE
APPROXIMATE DIMENSIONS.
0.72 m(2.36 ft)
F_AC_021200_1_0040101_01_00
Engine and NacelleThrust Reverser Cowls - PW 4000
FIGURE-2-12-0-991-004-A01
2-12-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
3.91 m(12.83 ft)
SECTIONCOMBUSTION
EXHAUST
IP TURBINE
0.81 m(2.66 ft)
NOZZLETURBINE EXHAUST
LP TURBINEHP TURBINE
HP COMPRESSORIP COMPRESSOR
1.4 m(4.59 ft)
4.17 m(13.68 ft)
SECTIONACCESSORY DRIVE
A
2.56 m(8.4 ft)
2.79 m(9.15 ft)
0.84 m(2.76 ft)
0.76 m(2.49 ft)
B
LP COMPRESSOR
CONE
1.55 m(5.09 ft)
B
0.76 m(2.49 ft)
NOTE:APPROXIMATE DIMENSIONS.
A
FWD
1.22 m(4.0 ft)
0.64 m(2.1 ft)
F_AC_021200_1_0050101_01_00
Engine and NacelleEngine Dimensions - TRENT 700
FIGURE-2-12-0-991-005-A01
2-12-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
NOSECOWL
THRUSTREVERSER
BL 100BL 100 BL 100
WL100
WL100
(10.01 ft)3.05 m
(10.10 ft)3.08 m
(8.17 ft)2.49 m
(5.68 ft)(8.30 ft)2.53 m
(5.58 ft)1.7 m
(4.49 ft)1.37 m
(24.02 ft)7.32 m
DISTANCEFROM NOSE A330−300 A330−200/
−200F
(69.82 ft)21.28 m
(59.32 ft)18.08 m
1.73 m
NOTE:APPROXIMATE DIMENSIONS.
A
A
A
B
B
C
C
A A B B C C
(6.2 ft)1.89 m
(7.41 ft)2.26 m
COMMONNOZZLE
ASSEMBLYFAN COWL
(10.5 ft)3.2 m
A
F_AC_021200_1_0060101_01_00
Engine and NacelleNacelle Dimensions - TRENT 700
FIGURE-2-12-0-991-006-A01
2-12-0Page 11
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
WL 100
GROUND
FAN COWLOPEN 55°
(19.16 ft)5.84 m
(2.26 ft)0.69 m
(9.61 ft)2.93 m
1.99 m(6.53 ft)
CLOSED
WL 100
(10.1 ft)3.08 m
NOTE:APPROXIMATE DIMENSIONS.
F_AC_021200_1_0070101_01_00
Engine and NacelleFan Cowls - TRENT 700
FIGURE-2-12-0-991-007-A01
2-12-0Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
WL 100
GROUND
THRUSTREVERSEROPEN 43°
CLOSED
WL 100
VIEW ON REAR OFENGINE
(10.10 ft)3.08 m
(2.26 ft)0.69 m
1.48 m(4.86 ft) 1.28 m
(4.2 ft)
1.91 m(6.27 ft)
(7.19 ft)2.19 m
(17.09 ft)5.21 m
NOTE:APPROXIMATE DIMENSIONS.
F_AC_021200_1_0080101_01_00
Engine and NacelleThrust Reverser Cowls - TRENT 700
FIGURE-2-12-0-991-008-A01
2-12-0Page 13
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
LP
ACCESSORYDRIVE SECTION
HP TURBINE
LP COMPRESSOR CORE MODULE
TURBINE
TURBINE
REAR FRAME
HP COMPRESSOR COMBUSTION
SECTION
A
A
FWD
F_AC_021200_1_0090101_01_00
Engine and NacelleEngine Dimensions - GE CF6-80E1
FIGURE-2-12-0-991-009-A01
2-12-0Page 14
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
4°
W
U
V
INLETREVERSER
(26.08 ft)7.95 m
(5.02 ft)1.53 m
(5.05 ft)1.54 m
(5.54 ft)1.69 m
(3.54 ft)1.08 m
(5.48 ft)1.67 m
(1.44 ft)0.44 m
(4.76 ft)1.45 m
THRUST
NOZZLE
A
A
C
C
D
D
NOTE:APPROXIMATE DIMENSIONS
A−A
B−B
C−C
D−D
W U V NAC STA
(10.1 ft)3.08 m
(4.95 ft)1.51 m
(5.22 ft)1.59 m
(11.45 ft)3.49 m
(16.5 ft)5.03 m
(4.63 ft)1.41 m
(4.63 ft)1.41 m
(9.25 ft)2.82 m
(8.17 ft)2.49 m
(4.1 ft)1.25 m
(4.1 ft)1.25 m
(21 ft)6.4 m
(27.03 ft)8.24 m
(2.1 ft)0.64 m
(2.1 ft)0.64 m
(4.2 ft)1.28 m
DISTANCE FROMTHE NOSE A330−200A330−300
A (69.36 ft)21.14 m
(58.86 ft)17.94 m
A
PLUGEXHAUST
EXHAUSTB
B
(8.53 ft)2.6 m
COWLFAN
COWLCORECOWL
F_AC_021200_1_0100101_01_00
Engine and NacelleNacelle Dimensions - GE CF6-80E1
FIGURE-2-12-0-991-010-A01
2-12-0Page 15
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
GROUND
CLOSED
WL 100
(2.53 ft)0.77 m
(12.47 ft)3.8 m
(16.24 ft)4.95 m
(17.19 ft)5.24 m
(10.10 ft)3.08 m
55°
NOTE:APPROXIMATE DIMENSIONS.
(4.99 ft)1.52 m (5.91 ft)
1.8 m
WL 100
F_AC_021200_1_0110101_01_00
Engine and NacelleFan Cowls - GE CF6-80E1
FIGURE-2-12-0-991-011-A01
2-12-0Page 16
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
50°
GROUND
CLOSED
WL 100
WL 100
VIEW ON REAR OFENGINE
(8.17 ft)2.49 m
(7.55 ft)2.3 m
1.72 m(5.64 ft)
2 m(6.56 ft)
NOTE:APPROXIMATE DIMENSIONS.
F_AC_021200_1_0120101_01_00
Engine and NacelleThrust Reverser Cowls - GE CF6-80E1
FIGURE-2-12-0-991-012-A01
2-12-0Page 17
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-1 Auxiliary Power Unit
**ON A/C A330-200 A330-200F A330-300
Auxiliary Power Unit
1. GeneralThe Auxiliary Power Unit (APU) and its related mechanical components are installed at the rear partof the fuselage in the tailcone section. The APU compartment is a fireproof area (identified as theFire Zone).The APU is a pneumatic and shaft-power gas-turbine engine and is used for the ground and in-flightpower supply of the aircraft.
The APU supplies:- mechanical shaft-power to operate a generator- bleed-air to the Main Engine Start (MES) and the Environmental Control System (ECS).
A part of the automatic system, with the pneumatic and the electromechanical controls, operates thestart and the acceleration functions of the APU.An air intake system with a flap-type door is installed in front of the APU compartment. The exhaustgases pass overboard at the end of the fuselage cone.
2. PowerplantThe APU is the Garrett Gas-Turbine Compressor Power-unit (GTCP) 331-350C with a single shaftengine.
The engine is the primary component of the APU, which is of the modular design. The modules ofthe engine are:- The power section- The load compressor- The accessory drive gearbox with LRU(s).
The power section has a two-stage centrifugal compressor, a reverse-flow annular combustionchamber and a three-stage axial turbine. The power section directly operates the one-stagecentrifugal load-compressor which supplies the bleed-air to the pneumatic system. The inlet guidevanes as part of the load compressor, control the airflow.The power section also operates the gearbox which is attached to the load compressor. The followingLRU’s are mounted on the gearbox :- the APU generator,- the starter motor,- the oil pump,- the Fuel Control Unit (FCU),- the cooling air fan.The APU has a gearbox-driven oil-cooled AC generator.
2-12-1Page 1
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The cooling air and ventilation system of the APU supplies the air for cooling of the APU and theequipment on the APU. It also supplies the air for ventilation of the APU compartment.
3. Control circuitThe Electronic Control Box (ECB), which controls the Fuel Control Unit (FCU) and the Inlet GuideVanes (IGV), keeps the APU at a constant speed. The control circuit is used to start the APU, toshut it down, to control it and to prevent internal failure.
4. Controls and IndicationThe primary APU controls and indications are installed in the overhead panel, on the center pedestalpanel and on the forward center panel. External APU panels are also installed on the nose landinggear and on the refuel/defuel panel, to initiate an APU emergency shut-down.
2-12-1Page 2
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
FR106A
FR103
FR101
FR95
FR94
FR92
FR91 317AL
315AL
313AL
Z310
A B
A
316AR
F_AC_021201_1_0020101_01_00
Auxiliary Power UnitAccess Doors (Sheet 1 of 2)FIGURE-2-12-1-991-002-A01
2-12-1Page 3
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
FIRE EXTINGUISHERBOTTLE
AIR INTAKE DUCT
APU
FIRE WALL
BLEED AIR LINE
OIL COOLER OUTLET
EXHAUST MUFFLER
FIXED DIVERTER
GUTTER
FR90
FR92
FR95
FR106A
FIRE WALL
FR101
B
AIR INTAKE
FORWARD
REAR
F_AC_021201_1_0020102_01_00
Auxiliary Power UnitGeneral Layout (Sheet 2 of 2)FIGURE-2-12-1-991-002-A01
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0 Levelling, symmetry and Alignment
**ON A/C A330-200 A330-200F A330-300
Leveling, Symmetry and Alignment
**ON A/C A330-200 A330-300
1. Quick LevelingThere are three alternative procedures to level the aircraft:- Quick leveling procedure with Air Data/Inertial Reference System (ADIRS)- Quick leveling procedure with a spirit level in the passenger compartment- Quick leveling procedure with a spirit level in the FWD cargo compartment.
**ON A/C A330-200F
2. Quick LevelingThere are three alternative procedures to level the aircraft:- Quick leveling procedure with Air Data/Inertial Reference System (ADIRS)- Quick leveling procedure with a spirit level in the Main Deck cargo compartment- Quick leveling procedure with a spirit level in the FWD cargo compartment.
**ON A/C A330-200 A330-200F A330-300
3. Precision LevelingFor precise leveling, it is necessary to install sighting rods in the receptacles located under thefuselage (points 12 and 13 for longitudinal leveling) and under the wings (points 2LH and 2RH forlateral leveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until thereference marks on the sighting rods are aligned in the sighting plane (aircraft level).
4. Symmetry and Alignment CheckPossible deformation of the aircraft is measured by photogrammetry.
2-13-0Page 1
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
RIB12
FR57 FR58
RIB12
13
2 RH
12
2 LH
FR38 FR39
F_AC_021300_1_0010101_01_00
Location of Leveling PointsFIGURE-2-13-0-991-001-A01
2-13-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FR57.4 FR58
RIB12
RIB12
FR38 FR39
12
2 LH
2 RH
13
F_AC_021300_1_0020101_01_00
Location of Leveling PointsFIGURE-2-13-0-991-002-A01
2-13-0Page 3
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
FR57 FR58RIB12
RIB12
FR38 FR39
132 LH
2 RH
12
F_AC_021300_1_0030101_01_00
Location of Leveling PointsFIGURE-2-13-0-991-003-A01
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0 Jacking for Maintenance
**ON A/C A330-200 A330-200F A330-300
Jacking for Maintenance
**ON A/C A330-200
1. Aircraft Jacking Points for Maintenance
A. General
(1) The A330-200 can be jacked:- At not more than 152 000 kg (335 103 lb)- Within the limits of the permissible wind speed when the aircraft is jacked outside a
closed environment.
B. Primary Jacking Points
(1) The aircraft is provided with three primary jacking points:- One located under the forward fuselage (after FR10A)- Two located under the wings (one under each wing), at the intersection of RIB10 and
the rear of the spar-datum.
(2) Three jack adapters (ground equipment) are used as intermediary parts between theaircraft jacking points and the jacks:- One male spherical jack adapter at the forward fuselage- Two female spherical jack pad adapters at the wings (one at each wing).
C. Auxiliary Jacking Point (Safety Stay)
(1) When the aircraft is on jacks, a safety stay is placed under the fuselage at FR87 to preventtail tipping caused by accidental displacement of the aircraft center of gravity.
(2) The safety point must not be used for lifting the aircraft.
(3) One male spherical stay adapter (ground equipment) is used as an intermediary partbetween the aircraft safety point and the stay.
**ON A/C A330-300
2. Aircraft Jacking Points for Maintenance
A. General
(1) The A330-300 can be jacked:- At not more than 152 000 kg (335 103 lb)- Within the limits of the permissible wind speed when the aircraft is jacked outside a
closed environment.
B. Primary Jacking Points
(1) The aircraft is provided with three primary jacking points:- One located under the forward fuselage (after FR10A)
2-14-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Two located under the wings (one under each wing), at the intersection of RIB10 andthe rear of the spar-datum.
(2) Three jack adapters (ground equipment) are used as intermediary parts between theaircraft jacking points and the jacks:- One male spherical jack adapter at the forward fuselage- Two female spherical jack pad adapters at the wings (one at each wing).
C. Auxiliary Jacking Point (Safety Stay)
(1) When the aircraft is on jacks, a safety stay is placed under the fuselage at FR85 to preventtail tipping caused by accidental displacement of the aircraft center of gravity.
(2) The safety point must not be used for lifting the aircraft.
(3) One male spherical stay adapter (ground equipment) is used as an intermediary partbetween the aircraft safety point and the stay.
**ON A/C A330-200F
3. Aircraft Jacking Points for Maintenance
A. General
(1) The A330-200F can be jacked:- At not more than 136 000 kg (299 829 lb)- Within the limits of the permissible wind speed when the aircraft is jacked outside a
closed environment.
B. Primary Jacking Points
(1) The aircraft is provided with three primary jacking points:- One located under the forward fuselage (at FR10A), covered by nose fairing panel
125AL.- Two located under the wings (one under each wing), at the intersection of RIB10 and
the rear of the spar-datum.
(2) Three jack adapters (ground equipment) are used as intermediary parts between theaircraft jacking points and the jacks:- One male spherical jack adapter at the forward fuselage- Two female spherical jack pad adapters at the wings (one at each wing).
C. Auxiliary Jacking Point (Safety Stay)
(1) When the aircraft is on jacks, a safety stay is placed under the fuselage at FR87 to preventtail tipping caused by accidental displacement of the aircraft center of gravity.
(2) The safety point must not be used for lifting the aircraft.
(3) One male spherical stay adapter (installed on the aircraft) is used as an intermediary partbetween the aircraft safety point and the stay.
2-14-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
4. Jacks and Safety Stay
A. Jack Design
(1) The maximum eligible loads given in the table (Ref. Fig. Jacking Point Location) are themaximum loads applicable on jack fittings.
(2) In fully retracted position (jack stroke at minimum), the height of the jack is such that thejack may be placed beneath the aircraft under the most adverse conditions, namely, tiresdeflated and shock absorbers depressurized, with sufficient clearance between the aircraftjacking point and the jack upper end.
(3) The lifting jack stroke enables the aircraft to be jacked up so that the Fuselage DatumLine (FDL) may be positioned up to 7.2 m (23.62 ft) from the ground to allow all requiredmaintenance procedures and in particular, the removal/installation of the landing-gearshock absorbers.
B. Safety StayThe stay stroke enables the aircraft tail to be supported up to the Fuselage Datum Line (FDL)positioned 7.2 m (23.62 ft) from the ground.
**ON A/C A330-200F
5. Jacks and Safety Stay
A. Jack Design
(1) The maximum eligible loads given in the table (Ref. Fig. Jacking Point Location) are themaximum loads applicable on jack fittings.
(2) In fully retracted position (jack stroke at minimum), the height of the jack is such that thejack may be placed beneath the aircraft under the most adverse conditions, namely, tiresdeflated and shock absorbers depressurized, with sufficient clearance between the aircraftjacking point and the jack upper end.
(3) The lifting jack stroke enables the aircraft to be jacked up so that the Fuselage Datum line(FDL) may be positioned up to 7.2 m (23.62 ft) from the ground to allow all requiredmaintenance procedures and in particular, the removal/installation of the landing-gearshock absorbers.
(4) At the forward jacking point, specific jack dimensions are necessary (Ref. Fig. SpecificJack-Nose Dimensions):- Maximum jack tube diameter 320 mm (12.6 in)- Maximum threaded rod diameter 160 mm (6.3 in)- Minimum threaded rod length 250 mm (9.8 in).
B. Safety StayThe stay stroke enables the aircraft tail to be supported up to the Fuselage Datum Line (FDL)positioned 7.2 m (23.62 ft) from the ground.
2-14-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
FWD JACKINGPOINT
SAFETYSTAY
Y
B’
B
WING JACKINGPOINT
X
SAFETY STAY
WING JACKINGPOINT
C
B’
B
FORWARD FUSELAGEJACKING POINT A
3.58
28.35
28.35
51.54
11.75
93.01
93.01
169.09
0
8.51
−8.51
0
0
27.92
−27.92
0
MAXIMUMLOAD ELIGIBLE
m ft
12 300
daN
YX
81 084
81 084
4 500
m ft
CA
NOTE:SAFETY STAY IS NOT USED FOR JACKING.
WING JACKINGPOINT
F_AC_021400_1_0010101_01_00
Jacking for MaintenanceJacking Points Location
FIGURE-2-14-0-991-001-A01
2-14-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
SAFETY STAY
WING JACKINGPOINT
C
B’
B
FORWARD FUSELAGEJACKING POINT A
3.58 11.75 0
8.51
−8.51
0
0
27.92
−27.92
0
MAXIMUMLOAD ELIGIBLE
m ft daN
YX
m ft
31.55
31.55
55.81
103.51
103.51
183.1
12 300
81 084
81 084
4 500
Y
X
B
A C
NOTE:SAFETY STAY IS NOT USED FOR JACKING.
FWD JACKINGPOINT
SAFETYSTAY
WING JACKINGPOINT
WING JACKINGPOINT
B’
F_AC_021400_1_0010201_01_00
Jacking for MaintenanceJacking Points Location
FIGURE-2-14-0-991-001-B01
2-14-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
SAFETY STAY
WING JACKINGPOINT
C
B’
B
FORWARD FUSELAGEJACKING POINT A
3.57
28.35
28.35
51.54
11.71
93.01
93.01
169.09
0
8.51
−8.51
0
0
27.92
−27.92
0
MAXIMUMLOAD ELIGIBLE
m ft
11 246
daN
YX
65 389
65 389
4 500
m ft
Y
B’
X
NOTE:SAFETY STAY IS NOT USED FOR JACKING.
FWD JACKINGPOINT
SAFETYSTAY
WING JACKINGPOINT
B
WING JACKINGPOINT
CA
F_AC_021400_1_0010301_01_00
Jacking for MaintenanceJacking Points Location
FIGURE-2-14-0-991-001-C01
2-14-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
Z−2157.8
Z−2136
FR10A
AFR10A
A
FWD
B
ADAPTOR −JACK NOSE
B
SPHERICALRADIUS 19 mm (0.75 in)
F_AC_021400_1_0020101_01_00
Jacking for MaintenanceForward Jacking Point
FIGURE-2-14-0-991-002-A01
2-14-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Z−2156.8
Z−2135
FR10AA
FR10A
ADAPTOR −JACK NOSE
B
SPHERICALRADIUS 19 mm (0.75 in)
A
FWD
B
F_AC_021400_1_0020201_01_00
Jacking for MaintenanceForward Jacking Point
FIGURE-2-14-0-991-002-B01
2-14-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
A
A
RIB10
RIB10
LOWER SURFACE
EXAMPLE
Z−790.3
Z−700.6
SPHERICALRADIUS 32 mm
(1.26 in)
JACKING PADSET−WING
OUTER SKIN
RIB10OUTER SKIN
B
B
A
DATUM INTERSECTIONAT MID REAR SPAR DATUM
F_AC_021400_1_0030101_01_00
Jacking for MaintenanceWing Jacking Points
FIGURE-2-14-0-991-003-A01
2-14-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
A
A RIB10
RIB10
LOWER SURFACE
EXAMPLE
Z−1019.7
Z−930
SPHERICALRADIUS 32 mm
(1.26 in)
JACKING PADSET−WING
OUTER SKIN
RIB10OUTER SKIN
B
B
A
DATUM INTERSECTIONAT MID REAR SPAR DATUM
F_AC_021400_1_0030201_01_00
Jacking for MaintenanceWing Jacking Points
FIGURE-2-14-0-991-003-B01
2-14-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
FR87
A
SPHERICALRADIUS 19 mm (0.75 in)
Z 83.4
Z 116.7
A
FR87
B
FWD
ADAPT−SUPP, AFT JACK
B
F_AC_021400_1_0040101_01_00
Jacking for MaintenanceAuxiliary Jacking Point - Safety Stay
FIGURE-2-14-0-991-004-A01
2-14-0Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FR85
A
SPHERICALRADIUS 19 mm (0.75 in)
Z−474.0
Z−440.7
A
B
FWD
FR85
ADAPT−SUPP, AFT JACK
B
F_AC_021400_1_0040201_01_00
Jacking for MaintenanceAuxiliary Jacking Point - Safety Stay
FIGURE-2-14-0-991-004-B01
2-14-0Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
FR87
A
SPHERICALRADIUS 19 mm (0.75 in)
Z−117.7
Z−84.4
A
B
FWD
FR87
ADAPT−SUPP, AFT JACK
B
F_AC_021400_1_0040301_01_00
Jacking for MaintenanceAuxiliary Jacking Point - Safety Stay
FIGURE-2-14-0-991-004-C01
2-14-0Page 13
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
MAKE SURE THAT THE JACK YOU USE IS APPLICABLE FOR THIS AIRCRAFT.IF THE JACK DIMENSIONS ARE NOT IN THE RANGE FOR THIS AIRCRAFT,DAMAGE TO THE AIRCRAFT STRUCTURE CAN OCCUR.
MAX 320 mm(12.6 in)
CAUTION:
H MIN 250 mm (9.84 in)THREADED ROD EXTENSION
A
A
(6.3 in)
MAX 160 mm
FR10A FR11
F_AC_021400_1_0220101_01_00
Jacking for MaintenanceSpecific Jack-Nose DimensionsFIGURE-2-14-0-991-022-A01
2-14-0Page 14
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
L
AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 152 000 kg (335 103 lb)
2.59 m(8.5 ft)
4.46 m(14.63 ft)
5.68 m(18.64 ft)
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES
2.26 m(7.4 ft)
4.1 m(13.45 ft)
5.07 m(16.63 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6.5 m (21.33 ft) FOR LANDINGGEARS EXTENSION/RETRACTION
4.37 m(14.34 ft)
5.8 m(19.03 ft)
6.38 m(20.93 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7.2 m (23.62 ft) FOR LANDINGGEARS REMOVAL/INSTALLATION
5.07 m(16.63 ft)
6.5 m(21.33 ft)
7.08 m(19.19 ft)
L M N
AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 124 500 kg (274 475 lb)
2.61 m(8.56 ft)
4.51 m(14.8 ft)
5.85 m(19.19 ft)
FUSELAGE
N
DATUM LINE
M
F_AC_021400_1_0050101_01_00
Jacking for MaintenanceJacking Dimensions
FIGURE-2-14-0-991-005-A01
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
N
AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 152 000 kg (335 103 lb)
2.52 m(8.27 ft)
2.2 m(7.22 ft)
4.37 m(14.34 ft)
5.07 m(16.63 ft)
2.5 m(8.20 ft)
4.46 m(14.63 ft)
5.39 m(17.68 ft)
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES
4.1 m(13.45 ft)
4.77 m(15.65 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6.5 m (21.33 ft) FOR LANDINGGEARS EXTENSION/RETRACTION
5.8 m(19.03 ft)
6.06 m(19.88 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7.2 m (23.62 ft) FOR LANDINGGEARS REMOVAL/INSTALLATION
6.5 m(21.33 ft)
6.76 m(22.18 ft)
L M N
AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 127 000 kg (279 986 lb)
4.51 m(14.8 ft)
5.57 m(18.27 ft)
FUSELAGEDATUM LINE
L
M
F_AC_021400_1_0050201_01_00
Jacking for MaintenanceJacking Dimensions
FIGURE-2-14-0-991-005-B01
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Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 136 000 kg (299 829 lb)
3.04 m(9.97 ft)
3.07 m(10.07 ft)
4.37 m(14.34 ft)
5.06 m(16.6 ft)
3.05 m(10.01 ft)
4.42 m(14.5 ft)
5.39 m(17.68 ft)
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES
4.54 m(14.9 ft)
4.75 m(15.58 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6.52 m (21.39 ft) FOR LANDINGGEARS EXTENSION/RETRACTION
5.58 m(18.31 ft)
6.38 m(20.93 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7.2 m (23.62 ft) FOR LANDINGGEARS REMOVAL/INSTALLATION
6.26 m(20.54 ft)
7.06 m(23.16 ft)
L M N
AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 109 000 kg (240 304 lb)
4.53 m(14.86 ft)
5.58 m(18.31 ft)
FUSELAGEDATUM LINE
M
N
L
F_AC_021400_1_0050301_01_00
Jacking for MaintenanceJacking Dimensions
FIGURE-2-14-0-991-005-C01
2-14-0Page 17
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
AT 26.5% RC . THE REACTION AT THE WING JACKING POINTS IS 127 000 kg(63 500 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINT
IS 8 000 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT
ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 135 000 kg AND CENTER OF GRAVITYAB
CD
BE IN EXCESS OF 60 km/h.
EXAMPLE:
0 6 8 10 12 14 16 18 20
80
90
100
110
120
130
140
150
160
170 40
2015
LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1 000)
10
LOA
D O
N W
ING
JA
CK
ING
PO
INT
S (
kg x
1 0
00)
45
50
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
kg x
1 0
00)
2 4
80
90
100
110
120
130
140
150
160
170
22
20 30 40 50 60 70 80
2530
35
TIP UPSECURITYMARGIN
PERMISSIBLE WIND SPEED (km/h)
AIRCRAFT CG (%RC)
B
A
C
D
F_AC_021400_1_0060101_01_00
Jacking for MaintenanceLoad at the Aircraft Jacking Points
FIGURE-2-14-0-991-006-A01
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Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
0 6 8 10 12 14 16 18 20
80
90
100
110
120
130
140
150
160
170 4035
2520
1510
45 20 30 40 50 60 70
50
2 4
80
90
100
110
120
130
140
150
160
170
EXAMPLE:
AT 22.8% RC . THE REACTION AT THE WING JACKING POINTS IS 136 000 kg(68 000 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINT
IS 9 000 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT
ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 145 000 kg AND CENTER OF GRAVITYAB
CD
BE IN EXCESS OF 60 km/h.
TIP UPSECURITYMARGIN
LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1 000)
LOA
D O
N W
ING
JA
CK
ING
PO
INT
S (
kg x
1 0
00)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
kg x
1 0
00)
PERMISSIBLE WIND SPEED (km/h)
30
A
B
D
C
AIRCRAFT CG (%RC)
F_AC_021400_1_0060201_01_00
Jacking for MaintenanceLoad at the Aircraft Jacking Points
FIGURE-2-14-0-991-006-B01
2-14-0Page 19
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-1 Jacking for Wheel Change
**ON A/C A330-200 A330-200F A330-300
Jacking for Wheel Change
1. GeneralTo replace either the wheel or brake unit assemblies on any of the landing gears, it is necessary to liftthe landing gear with a jack.The landing gear can be lifted by a pillar jack or with a cantilever jack.The possible damage conditions than can be found on the landing-gear wheel units are shown inFigures ”MLG Jacking Point Heights” and ”NLG Jacking Point Heights”.
NOTE : You can lift the aircraft at the Maximum Take-Off Weight (MTOW).
2. Main Landing Gear (MLG)To lift the MLG bogie with jacks, a dome shaped pad (PN MS33559 TYPE IV) is installed below theFWD and AFT ends of each bogie beam. Each pair of wheels and brake units can be replaced on theend of the bogie that is lifted.Both FWD and AFT ends of the bogie beam can be lifted together, but the bogie beam must be keptlevel during the lift to prevent damage.The MLG has a pitch trimmer installed. If an MLG has all four tires deflated or shredded, replace thewheel assemblies in this sequence:- Replace the wheel assemblies on the AFT axle,- Replace the wheel assemblies on the FWD axle.
If the FWD axle is lifted first the pitch trimmer contacts the outstop. Further jacking will cause thewhole bogie to be lifted.Important dimensions on heights of the MLG when lifted are shown in Figure ”MLG Jacking PointHeights”.The maximum height of the bogie beam when lifted must not exceed 650 mm (25.6 in).The reaction loads at each jack position are shown in Figure ”MLG Jacking Point Loads”.
NOTE : The load at each jacking position is the load required to give 25.4 mm (1 in) clearancebetween the ground and the tire.
3. Nose Landing Gear (NLG)To lift the NLG axle with a jack, a dome shaped pad (PN MS33559 Type II) is installed between thewheels.Important dimensions on heights of the NLG when lifted are shown in Figure ”NLG Jacking PointHeights”.The reaction loads at the jack position are shown in Figure ”NLG Jacking Point Loads”.
NOTE : The load at each jacking position is the load required to give 25.4 mm (1 in) clearancebetween the ground and the tire.
2-14-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
AFT WHEELS JACKED UPFWD WHEELS INSTALLED AND INFLATED
FWD WHEELS JACKED UPAFT WHEELS INSTALLED AND INFLATED
JACKING POINT570 mm
(22.44 in)
MAX DIAMETER1 443.7 mm(56.84 in)
25.4 mm(1 in)
NORMAL ATTITUDE
JACKING POINT376 mm(14.8 in)
25.4 mm(1 in)
FWD
FWD
FWD
JACKING POINT376 mm(14.8 in)
JACKING POINT570 mm
(22.44 in)
F_AC_021401_1_0010102_01_00
Jacking for Wheel ChangeMLG Jacking Point Heights (Sheet 1 of 3)
FIGURE-2-14-1-991-001-A01
2-14-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
FWD AXLEBOTH TIRES SHREDDED OR DEFLATED
AFT AXLEBOTH TIRES SHREDDED OR DEFLATED
FWD AND AFT AXLEBOTH TIRES SHREDDED OR DEFLATED
JACKING POINT376 mm(14.8 in)JACKING POINT
145.9 mm(5.74 in)
JACKING POINT376 mm(14.8 in) JACKING POINT
145.5 mm(5.73 in)
JACKING POINT157 mm(6.18 in)
JACKING POINT157 mm(6.18 in)
FWD
FWD
FWD
F_AC_021401_1_0010103_01_00
Jacking for Wheel ChangeMLG Jacking Point Heights (Sheet 2 of 3)
FIGURE-2-14-1-991-001-A01
2-14-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
AFT AXLEBOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
JACKING POINT376 mm(14.8 in) JACKING POINT
118.8 mm(4.68 in)
FWD
FWD AND AFT AXLESTIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
JACKING POINT130 mm(5.12 in)
JACKING POINT130 mm(5.12 in)
FWD
JACKING POINT376 mm(14.8 in)JACKING POINT
118.8 mm(4.68 in)
FWD
FWD AXLEBOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
F_AC_021401_1_0010104_01_00
Jacking for Wheel ChangeMLG Jacking Point Heights (Sheet 3 of 3)
FIGURE-2-14-1-991-001-A01
2-14-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
1 FLAT TIRE110 mm(4.33 in)180 mm MAX
(7.09 in)
(1 in)25.4 mm
400 mm
(15.75 in)
170 mm(6.69 in) FWD
F_AC_021401_1_0020101_01_00
Jacking for Wheel ChangeJacking of the NLG (Sheet 1 of 2)
FIGURE-2-14-1-991-002-A01
2-14-1Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
1 083 mm(42.64 in)
270 mm(10.63 in)
NORMAL ATTITUDE
TWO TIRES DEFLATED OR SHREDDED
HEIGHT OF JACKING POINT TO GROUNDTO CHANGE/REPLACE THE WHEEL ASSEMBLY
297.5 mm(11.71 in)
JACKING POINT290 mm
(11.42 in)
JACKING POINT148.5 mm(5.85 in)
JACKING POINT400 mm
(15.75 in)
25.4 mm(1 in)
FWD
FWD
FWD
F_AC_021401_1_0020102_01_00
Jacking for Wheel ChangeNLG Jacking Point Heights (Sheet 2 of 2)
FIGURE-2-14-1-991-002-A01
2-14-1Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
AIRCRAFT GROSS WEIGHT
280 320 360 400 440 480 520
120 140 160 180 200 220 24050
60
70
80
90
100
110
120
130
260
560
(x 1 000 kg)
(x 1 000 lb)
35% MAC30% MAC25% MAC20% MAC15% MAC
41% MACCG POSITION
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
F_AC_021401_1_0030101_01_00
Jacking for Wheel ChangeMLG Jacking Point Loads
FIGURE-2-14-1-991-003-A01
2-14-1Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
AIRCRAFT GROSS WEIGHT
120 140 160 180 200 220 24050
60
70
80
90
100
110
120
130
260(x 1 000 kg)
(x 1 000 lb)
35% MAC30% MAC25% MAC18% MAC
40% MACCG POSITION
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
280 320 360 400 440 480 520 560
F_AC_021401_1_0030201_01_00
Jacking for Wheel ChangeMLG Jacking Point Loads
FIGURE-2-14-1-991-003-B01
2-14-1Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
10
15
20
25
30
35
40
45
50
55
60
65
140 160 180 200 220 240120 260(x 1 000 kg)
280 320 360 400 440 480 520 560
(x 1 000 lb)
AIRCRAFT GROSS WEIGHT
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
20% MAC25% MAC30% MAC35% MAC41% MAC
15% MACCG POSITION
6
8
10
12
14
16
18
20
22
24
26
28
30
4
F_AC_021401_1_0040101_01_00
Jacking for Wheel ChangeNLG Jacking Point Loads
FIGURE-2-14-1-991-004-A01
2-14-1Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
15
20
25
30
35
40
45
50
55
60
65
140 160 180 200 220 240120 260(x 1 000 kg)
280 320 360 400 440 480 520 560
(x 1 000 lb)
AIRCRAFT GROSS WEIGHT
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
6
8
10
12
14
16
18
20
22
24
26
28
30
70
75
32
34
36
30% MAC35% MAC40% MAC
18% MACCG POSITION
25% MAC
F_AC_021401_1_0040201_01_00
Jacking for Wheel ChangeNLG Jacking Point Loads
FIGURE-2-14-1-991-004-B01
2-14-1Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-2 Support of Aircraft
**ON A/C A330-200 A330-200F A330-300
Support of Aircraft
1. Support of AircraftWhen it is necessary to support the aircraft in order to relieve the loads on the structure for theaccomplishment of modifications or major work, it is advisable to provide adapters under the wingsand the fuselage for an alternative means of lifting.
The aircraft must not be lifted or supported by the wings or fuselage alone. It is important to supportthe aircraft fuselage and wings at the same time to prevent structural damage.
A. Shoring CradlesShoring cradles are used when it is necessary to stress-jack the aircraft to carry out maintenanceand repair work. These are used to oppose the deflections of the wings and reduce the stressesto an acceptable level at the area of maintenance and repair.
The shoring cradles, each with two adjustable pads, 152.4 mm (6 in) square, are positioned atfour locations under each wing.
The adjustable pads are faced with thin rubber and are in contact with the wing profile at thedatum intersections of the ribs and the front and rear spars (F/S and R/S).
2-14-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
FR80
FR72
FR58
FR26
FR17
FR11
RIB6
RIB16
RIB21
RIB31
NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
(SAFETY STAY)FR87
RIB6
RIB16
RIB21
RIB31
FR53.2
F_AC_021402_1_0010101_01_00
Support of AircraftLocation of Shoring Cradles (Sheet 1 of 2)
FIGURE-2-14-2-991-001-A01
2-14-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
FR7
FR17
FR20
FR53.8 FR59 FR76
FR29
FR36
FR39.1
A
LH SHOWN
(9.02 ft)2.75 m
(15.09 ft)4.6 m
(6.89 ft)2.1 m
EXAMPLE
A
B
RH SYMMETRICAL
B B
F_AC_021402_1_0010102_01_00
Support of AircraftLocation of Auxiliary Jacking Points (Sheet 2 of 2)
FIGURE-2-14-2-991-001-A01
2-14-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FR85
FR80
FR72
FR58
FR26
FR17
FR11
(SAFETY STAY)
NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
RIB6
RIB16
RIB21
RIB31
FR53.2
RIB6
RIB16
RIB21
RIB31
F_AC_021402_1_0010201_01_00
Support of AircraftLocation of Shoring Cradles (Sheet 1 of 2)
FIGURE-2-14-2-991-001-B01
2-14-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FR7
FR17
FR20
FR26.1
FR39.1 FR53.8 FR59 FR76
FR36
A
LH SHOWN
(9.02 ft)2.75 m
(15.09 ft)4.6 m
(6.89 ft)2.1 m
EXAMPLE
A
B
RH SYMMETRICAL
B B
F_AC_021402_1_0010202_01_00
Support of AircraftLocation of Auxiliary Jacking Points (Sheet 2 of 2)
FIGURE-2-14-2-991-001-B01
2-14-2Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
FR80
FR72
FR26
FR17
FR11
(SAFETY STAY)FR87
NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
RIB6
RIB16
RIB21
RIB31
FR58
FR53.2
RIB6
RIB16
RIB21
RIB31
F_AC_021402_1_0010301_01_00
Support of AircraftLocation of Shoring Cradles (Sheet 1 of 2)
FIGURE-2-14-2-991-001-C01
2-14-2Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
FR17
FR20
FR53.8 FR59 FR76
FR29
FR36
FR39.1FR7
A
LH SHOWN
(9.02 ft)2.75 m
(15.09 ft)4.6 m
(6.89 ft)2.1 m
EXAMPLE
A
B
RH SYMMETRICAL
B B
F_AC_021402_1_0010302_01_00
Support of AircraftLocation of Auxiliary Jacking Points (Sheet 2 of 2)
FIGURE-2-14-2-991-001-C01
2-14-2Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0 General Information
**ON A/C A330-200 A330-200F A330-300
General Information
1. This section gives standard day temperatures.
Section 3-2 indicates payload range information at specific altitudes recommended for long rangecruise with a given fuel reserve condition.
Section 3-3 represents FAR/JAR takeoff runway length requirements at ISA and ISA +15˚C(+27˚F) for engine conditions for FAA/EASA certification :
- PRATT & WHITNEY (PW 4000).- ROLLS-ROYCE (RR Trent 700).- GENERAL ELECTRIC (GE CF6-80E1). (A330-200 and A330-300 only)
Section 3-4 represents FAR/JAR landing runway length requirements for FAA/EASA certification.
Section 3-5 indicates final approach speeds.
Standard day temperatures for the altitude shown are tabulated below :
Standard day temperatures for the altitude
Altitude Standard Day Temperature
FEET METERS ˚F ˚C0 0 59.0 15.02000 610 51.9 11.14000 1219 44.7 7.16000 1829 37.6 3.18000 2438 30.5 -0.8
3-1-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-0 Payload / Range
**ON A/C A330-200 A330-200F A330-300
Payload / Range
1. Payload / Range
3-2-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1 ISA Conditions
**ON A/C A330-200 A330-300
ISA Conditions
1. This section gives the payload / range at ISA conditions for pax version.
3-2-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
170
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0010101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE-3-2-1-991-001-A01
3-2-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
170
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0020101_01_01
PAYLOAD / RANGERR TRENT 700 Series EngineFIGURE-3-2-1-991-002-A01
3-2-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
0102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
170
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0030101_01_01
PAYLOAD / RANGEGE CF6-80E1 Series EngineFIGURE-3-2-1-991-003-A01
3-2-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
175
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0040101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE-3-2-1-991-004-A01
3-2-1Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
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INF
OR
MA
TIO
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ING
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ALS
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HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0 lb
)
RA
NG
E(n
m)
RA
NG
E(k
m)
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0050101_01_01
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
175
TM
AX
TA
KE
−O
FF
WE
IGH
T :
233
T
PAYLOAD / RANGERR TRENT 700 Series EngineFIGURE-3-2-1-991-005-A01
3-2-1Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
175
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0060101_01_01
PAYLOAD / RANGEGE CF6-80E1 Series EngineFIGURE-3-2-1-991-006-A01
3-2-1Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
ISA Conditions
1. This section gives the payload / range at ISA conditions for cargo version.
3-2-1Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
173
TM
AX
TA
KE
−O
FF
WE
IGH
T :
233
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0070101_01_01
PAYLOAD / RANGERR TRENT 700 Series EngineFIGURE-3-2-1-991-007-A01
3-2-1Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
178
TM
AX
TA
KE
−O
FF
WE
IGH
T :
227
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0080101_01_01
PAYLOAD / RANGERR TRENT 700 Series EngineFIGURE-3-2-1-991-008-A01
3-2-1Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
173
TM
AX
TA
KE
−O
FF
WE
IGH
T :
233
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0090101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE-3-2-1-991-009-A01
3-2-1Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
178
TM
AX
TA
KE
−O
FF
WE
IGH
T :
227
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0100101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE-3-2-1-991-010-A01
3-2-1Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-0 FAR / JAR Takeoff Weight Limitation
**ON A/C A330-200 A330-200F A330-300
FAR / JAR Takeoff Weight Limitation
1. FAR / JAR Takeoff Weight Limitation
3-3-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1 ISA Conditions
**ON A/C A330-200 A330-200F A330-300
FAR / JAR Takeoff Weight Limitation
1. This section gives the takeoff weight limitation at ISA conditions.
3-3-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
02
46
8
0 2 4 6 8
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
V.M
.C
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
F_AC_030301_1_0010101_01_01
Takeoff Weight LimitationISA Conditions - PW 4000 Series Engine
FIGURE-3-3-1-991-001-A01
3-3-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
20 4 6 8
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
V.M
.C
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
F_AC_030301_1_0020101_01_01
Takeoff Weight LimitationISA Conditions - RR TRENT 700 Series Engine
FIGURE-3-3-1-991-002-A01
3-3-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)V
.M.C
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION0 2 4 6 8
F_AC_030301_1_0030101_01_01
Takeoff Weight LimitationISA Conditions - GE CF6-80E1 Series Engine
FIGURE-3-3-1-991-003-A01
3-3-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2 ISA +15˚C (ISA +27˚F) Conditions
**ON A/C A330-200 A330-200F A330-300
ISA +15 ˚C (ISA +27 ˚F) Conditions
1. This section gives the takeoff weight limitation at ISA +15˚C (ISA +27˚F) conditions.
3-3-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
0 2 4 6 8
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
V.M
.C
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
F_AC_030302_1_0010101_01_01
FAR / JAR Takeoff Weight LimitationISA +15˚C (ISA +27˚F) Conditions - PW 4000 Series Engine
FIGURE-3-3-2-991-001-A01
3-3-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
0 2 4 6 8
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
V.M
.C
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
02
46
8
F_AC_030302_1_0020101_01_01
FAR / JAR Takeoff Weight LimitationISA +15˚C (ISA +27˚F) Conditions - RR TRENT 700 Series Engine
FIGURE-3-3-2-991-002-A01
3-3-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
0 2 4 6 8
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
V.M
.C
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
F_AC_030302_1_0030101_01_01
FAR / JAR Takeoff Weight LimitationISA +15˚C (ISA +27˚F) Conditions - GE CF6-80E1 Series Engine
FIGURE-3-3-2-991-003-A01
3-3-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-0 FAR / JAR Landing Field Length
**ON A/C A330-200 A330-200F A330-300
Landing Field Length
1. Landing Field Length
3-4-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1 ISA Conditions All series engines
**ON A/C A330-200 A330-200F A330-300
ISA Conditions All series engine
1. This section gives the landing field length.
3-4-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
.T
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.F
AR
/JA
R L
AN
DIN
GLE
NG
TH
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
(100
0 m
)(1
000
Ft) 15
050
020
025
040
045
030
035
0
230
7010
020
015
0
3456782.
5 1
1.52
24
68
10S
EA
LE
VE
L
(100
0 F
t)A
IRF
IELD
ELE
VA
TIO
N
F_AC_030401_1_0010101_01_01
ISA
CO
ND
ITIO
NS
CO
NF
. FU
LL
FAR / JAR Landing Field LengthISA Conditions - PW 4000 Series Engine
FIGURE-3-4-1-991-001-A01
3-4-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
.T
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.F
AR
/JA
R L
AN
DIN
GLE
NG
TH
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
(100
0 m
)(1
000
Ft)
46
810
150
500
200
250
400
450
300
350
230
7010
020
015
0
3456782.
5 1
1.52
SE
A L
EV
EL
2
AIR
FIE
LD E
LEV
AT
ION
(100
0 F
t)
F_AC_030401_1_0020101_01_01
ISA
CO
ND
ITIO
NS
CO
NF
. FU
LL
FAR / JAR Landing Field LengthISA Conditions - RR TRENT 700 Series Engine
FIGURE-3-4-1-991-002-A01
3-4-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
.T
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.F
AR
/JA
R L
AN
DIN
GLE
NG
TH
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
(100
0 m
)(1
000
Ft)
46
810
150
500
200
250
400
450
300
350
230
7010
020
015
0
3456782.
5 1
1.52
SE
A L
EV
EL
2
AIR
FIE
LD E
LEV
AT
ION
(100
0 F
t)
F_AC_030401_1_0030101_01_01
ISA
CO
ND
ITIO
NS
CO
NF
. FU
LL
FAR / JAR Landing Field LengthISA Conditions - GE CF6-80E1 Series Engine
FIGURE-3-4-1-991-003-A01
3-4-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0 Final Approach Speed
**ON A/C A330-200 A330-200F A330-300
Final Approach Speed
**ON A/C A330-200
1. Final Approach Speed
A. This section gives the final approach speed. This is the indicated airspeed at threshold in thelanding configuration, at the certificated maximum flap setting and maximum landing weight, instandard atmospheric conditions. The approach speed is used to classify the aircraft into anAircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.
B. The final approach speed is 136 kt at a Maximum Landing Weight (MLW) of 182 000 kg (401241 lb) and classifies the aircraft into the Aircraft Approach Category C.
NOTE : This value is given for information only.
**ON A/C A330-200F
2. Final Approach Speed
A. This section gives the final approach speed. This is the indicated airspeed at threshold in thelanding configuration, at the certificated maximum flap setting and maximum landing weight, instandard atmospheric conditions. The approach speed is used to classify the aircraft into anAircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.
B. The final approach speed is 139 kt at a Maximum Landing Weight (MLW) of 187 000 kg (412264 lb) and classifies the aircraft into the Aircraft Approach Category C.
NOTE : This value is given for information only.
**ON A/C A330-300
3. Final Approach Speed
A. This section gives the final approach speed. This is the indicated airspeed at threshold in thelanding configuration, at the certificated maximum flap setting and maximum landing weight, instandard atmospheric conditions. The approach speed is used to classify the aircraft into anAircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.
B. The final approach speed is 137 kt at a Maximum Landing Weight (MLW) of 187 000 kg (412264 lb) and classifies the aircraft into the Aircraft Approach Category C.
NOTE : This value is given for information only.
3-5-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A330-200 A330-200F A330-300
General Information
1. This section provides airplane turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.
In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the using airlines prior to layout planning.
4-1-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0 Turning Radii
**ON A/C A330-200 A330-200F A330-300
Turning Radii
1. This section gives the turning radii.
4-2-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
NOTE:FOR TURNING RADII VALUES, REFER TO SHEET 2.
72°
65°
60°
55°
R1
R5
R2
R3
R4
R6
F_AC_040200_1_0040101_01_03
Turning Radii(Sheet 1)
FIGURE-4-2-0-991-004-A01
4-2-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
19.420
TYPE OFTURN
267.7222
A330−300 TURNING RADII
m
ft78.4257
76.9252
R4WING
102.7337
R5NOSE
78.9259
R6TAIL
85.9282
R1RMLG
R2LMLG
R3NLG
24.225252.1171
62.8206
62.4205
87.1286
64.9213
71.2234
29.030241.4136
52.1171
52.8173
76.5251
55.9183
61.4201
33.835233.5110
44.2145
46.1151
68.7225
49.6163
54.4178
38.640227.490
38.1125
41.1135
62.7206
45.1148
49.1161
43.245222.674
33.3109
37.5123
58.0190
41.9137
45.2148
47.850218.6
6129.396
34.6114
54.0177
39.5130
42.0138
52.255215.350
26.085
32.5107
50.7166
37.6123
39.5130
56.360212.5
4123.276
30.8101
48.0158
36.2119
37.4123
60.165210.233
20.969
29.697
45.8150
35.2115
35.8117
63.87228.127
18.862
28.594
43.7143
34.4113
34.4113
48.250118.360
29.095
34.4113
53.7176
39.3129
41.7137
52.955114.849
25.584
32.2106
50.3165
37.4123
39.1128
57.660111.738
22.473
30.4100
47.2155
35.9118
36.9121
62.16519.130
19.765
29.095
44.6146
34.7114
35.1115
67.87216.020
16.755
27.691
41.6136
33.7111
33.1109
m
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION.TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; AND NO DIFFERENTIAL BRAKING AT ALL.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYINGDIFFERENTIAL BRAKING DURING THE WHOLE TURN. F_AC_040200_1_0020101_01_03
Turning Radii(Sheet 2)
FIGURE-4-2-0-991-002-A01
4-2-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
19.220
TYPE OFTURN
259.3195
A330−200/−200F TURNING RADII
m
ft70.0230
68.0223
R4WING
94.4310
R5NOSE
69.9229
R6TAIL
79.1260
R1RMLG
R2LMLG
R3NLG
23.925245.7150
56.4185
55.3181
80.9265
57.8190
66.6219
28.630236.3119
47.0154
46.8154
71.6235
49.9164
58.4192
33.335229.496
40.1132
40.9134
64.7212
44.4146
52.5172
38.040224.079
34.7114
36.5120
59.4195
40.5133
48.2158
42.545219.865
30.5100
33.2109
55.3181
37.7124
45.0148
46.950216.454
27.189
30.8101
51.9170
35.5116
42.4139
51.255213.544
24.179
28.894
49.1161
33.9111
40.4133
55.160211.136
21.872
27.490
46.8154
32.7107
38.8127
59.66528.628
19.363
26.085
44.4146
31.6104
37.2122
62.07227.424
18.159
25.483
43.2142
31.2102
36.5120
48.450115.350
26.085
30.098
50.9167
34.9115
41.7137
52.255112.842
23.577
28.493
48.5159
33.6110
39.9131
57.76019.631
20.367
26.587
45.4149
32.1105
37.9124
62.26517.324
18.059
25.383
43.1141
31.1102
36.5120
68.17214.515
15.250
24.179
40.4133
30.299
34.9115
m
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION.TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; AND NO DIFFERENTIAL BRAKING AT ALL.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYINGDIFFERENTIAL BRAKING DURING THE WHOLE TURN. F_AC_040200_1_0030101_01_03
Turning Radii(Sheet 2)
FIGURE-4-2-0-991-003-A01
4-2-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A330-200 A330-200F A330-300
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
NOTE:TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLETURN; AND NO DIFFERENTIAL BRAKING AT ALL.
A(MINIMUM TURNING WIDTH)
62.165 (MAX)
TYPE OFTURN
113.444
A330−300 MINIMUM TURNING RADII
m
ft49.0161
29.095
R4WING
44.6146
R5NOSE
34.7114
R6TAIL
35.1115
R3NLG
60.165 (MAX)214.648
50.7166
29.697
45.8150
35.2115
35.8117
m
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
25.483
25.483
AX Y
Y
72 (MAX)
72 (MAX)
2
1
63.8
67.8m
ftm
ft
10.434
44.6146
27.691
41.6136
33.7111
33.1109
12.541
47.6156
28.594
43.7143
34.4113
34.4113
25.483
25.483
OUTSIDE FACEOF TIRE
X
R3
R5
R6
R4
F_AC_040300_1_0010101_01_05
Minimum Turning RadiiFIGURE-4-3-0-991-001-A01
4-3-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
NOTE:TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLETURN; AND NO DIFFERENTIAL BRAKING AT ALL.
A(MINIMUM TURNING WIDTH)
62.265 (MAX)
TYPE OFTURN
111.738
A330−200/−200F MINIMUM TURNING RADII
m
ft43.6143
25.383
R4WING
43.1141
R5NOSE
31.1102
R6TAIL
36.5120
R3NLG
59.665 (MAX)213.043
45.6150
26.085
44.4146
31.6104
37.2122
m
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
22.273
22.273
AX Y
72 (MAX)
72 (MAX)
2
1
62.0
68.1m
ftm
ft
8.929
39.7130
24.179
40.4133
30.299
34.9115
11.839
43.8144
25.483
43.2142
31.2102
36.5120
22.273
22.273
R6
R4
R5
Y
R3OUTSIDE FACE
OF TIRE
X
F_AC_040300_1_0070101_01_01
Minimum Turning RadiiFIGURE-4-3-0-991-007-A01
4-3-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A330-200 A330-200F A330-300
Visibility from Cockpit in Static Position.
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
25°
20°
13.75 m(45.11 ft)
6.67 m(21.88 ft)
VISUAL ANGLES IN VERTICALPLANE THROUGH PILOTEYE POSITION.
DIMENSIONS ARE APPROXIMATE
2.4 m(7.87 ft)
115°
CAPTAIN FIELD OF VIEW
135°
115°
MAX AFT VISION WITH HEAD TURNEDAROUND SPINAL COLUMN.WING TIP CAN BE SEEN WHEN HEAD IS MOVEDTO THE SIDE.
VISUAL ANGLES IN HORIZONTALPLANE THROUGH PILOTEYE POSITION.
FIRST OFFICERFIELD OF VIEW
0.53 m(1.74 ft)
62°
42°
30°36°
30°
VISUAL ANGLES IN PLANEPERPENDICULAR TOLONGITUDINAL AXIS.
62°
42°
WITH HEAD MOVED125 mm (5 in) OUTBOARD
135°
36°
NOT TO BE USED FORLANDING APPROACH VISIBILITY
NOTE:PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
ZONE THAT CANNOT BE SEENF_AC_040400_1_0010101_01_01
Visibility from Cockpit in Static PositionFIGURE-4-4-0-991-001-A01
4-4-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
25°
20°
15.75 m(51.67 ft)
6.67 m(21.88 ft)
VISUAL ANGLES IN VERTICALPLANE THROUGH PILOTEYE POSITION.
DIMENSIONS ARE APPROXIMATE
2.4 m(7.87 ft)
115°
CAPTAIN FIELD OF VIEW
135°
115°
MAX AFT VISION WITH HEAD TURNEDAROUND SPINAL COLUMN.WING TIP CAN BE SEEN WHEN HEAD IS MOVEDTO THE SIDE.
VISUAL ANGLES IN HORIZONTALPLANE THROUGH PILOTEYE POSITION.
FIRST OFFICERFIELD OF VIEW
0.53 m(1.74 ft)
62°
42°
30°36°
30°
VISUAL ANGLES IN PLANEPERPENDICULAR TOLONGITUDINAL AXIS.
62°
42°
WITH HEAD MOVED125 mm (5 in) OUTBOARD
135°
36°
NOT TO BE USED FORLANDING APPROACH VISIBILITY
NOTE:PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
ZONE THAT CANNOT BE SEENF_AC_040400_1_0030101_01_01
Visibility from Cockpit in Static PositionFIGURE-4-4-0-991-003-A01
4-4-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
CA
PT
AIN
WIN
DS
HIE
LDC
AP
TA
IN S
LID
ING
WIN
DO
WC
AP
TA
INF
IXE
D W
IND
OW
WIN
G T
IPV
ISIB
LE
CA
PT
AIN
’S F
IELD
OF
VIE
W S
HO
WN
, TH
RO
UG
H C
AP
TA
IN W
IND
OW
S O
NLY
.F
IRS
T O
FF
ICE
R F
IELD
OF
VIE
W S
YM
ME
TR
ICA
L.
EX
AM
PLE
: WH
EN
CA
PT
AIN
TU
RN
S H
IS H
EA
D B
Y 8
5° L
EF
T, V
ISIB
ILIT
YW
ILL
BE
43°
UP
AN
D 3
0° D
OW
N T
HR
OU
GH
TH
E S
LID
ING
WIN
DO
W F
RA
ME
.
A33
0/A
340
50°
40°
30°
20°
10°
0°10
°20
°30
°40
°50
°60
°70
°80
°90
°10
0°11
0°12
0°13
0°14
0°
30°
20°
10°
0°10°
20°
30°
40°
43°
PIL
OT
EY
E P
OS
ITIO
N(C
AP
TA
IN P
OS
ITIO
N)
F_AC_040400_1_0060101_01_00
Binocular Visibility Through Windows from Captain Eye PositionFIGURE-4-4-0-991-006-A01
4-4-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A330-200 A330-200F A330-300
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A330-200 A330-200F A330-300
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
APPROX 10.6 m(35 ft)
(15 ft)APPROX 4.7 m
45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
F_AC_040501_1_0010101_01_01
135˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-1-991-001-A01
4-5-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
TURN R = 45 m(150 ft)
FILLET R = 25.5 m(85 ft)
APPROX 1.3 m
ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE
(4 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
45 m(150 ft)
RUNWAY
23 m(75 ft)
NLG PATH
MLG PATH
CENTERLINE
TAXIWAYCENTERLINE
F_AC_040501_1_0060101_01_00
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-006-A01
4-5-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
FAA LEAD−IN FILLET
L = 75 m (250 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
(19 ft)APPROX R = 5.9 m
APPROX 11.3 m(37 ft)
45 m(150 ft)
23 m(75 ft)
NLG PATH
MLG PATH
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
F_AC_040501_1_0020101_01_01
135˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-1-991-002-A01
4-5-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
FAA LEAD−IN FILLET
L = 75 m (250 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
(15 ft)APPROX 4.5 m
45 m(150 ft)
23 m(75 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
F_AC_040501_1_0070101_01_00
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-007-A01
4-5-1Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A330-200 A330-200F A330-300
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
45 m(150 ft)
23 m(75 ft)
(45 ft)APPROX 13.8 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
(37 ft)APPROX 11.2 m
NLG PATH
MLG PATH
F_AC_040502_1_0010101_01_01
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-2-991-001-A01
4-5-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m(75 ft)
TURN R = 45 m(150 ft)
(17 ft)APPROX 5.1 m
FILLET R = 25.5 m(85 ft)
45 m(150 ft) NLG PATH
MLG PATH
F_AC_040502_1_0080101_01_00
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-008-A01
4-5-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
(45 ft)APPROX 13.6 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m
45 m(150 ft)
23 m(75 ft)
(47 ft)APPROX 14.3 m
FAA LEAD−IN FILLETL = 75 m (250 ft)
NLG PATH
MLG PATH
(150 ft)
F_AC_040502_1_0020101_01_01
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-2-991-002-A01
4-5-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
(24 ft)APPROX 7.3 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
(150 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m(75 ft)
NLG PATH
MLG PATH
45 m
F_AC_040502_1_0090101_01_00
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-009-A01
4-5-2Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A330-200 A330-200F A330-300
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
R4 = 41.6 m(136 ft)
R6 = 33.1 m(109 ft)
R3 = 27.6 m(91 ft)
R5 = 33.7 m(111 ft)
4.5 m(15 ft)
4.5 m(15 ft)
NLG PATH
MLG PATH
NOSE TIP PATH
WING TIP PATH
TAIL TIP PATHNOTE:
TYPE 1 VALUES FOR MAX STEERING ANGLE = 72°.
RUNWAY CENTERLINE
IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
APPROX 55.2 m(181 ft)
F_AC_040503_1_0130101_01_01
180˚ Turn on a RunwayFIGURE-4-5-3-991-013-A01
4-5-3Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
R4 = 40.4 m(133 ft)
R6 = 34.9 m(115 ft)
R3 = 24.1 m(79 ft)
R5 = 30.2 m(99 ft)
NLG PATH
MLG PATH
NOSE TIP PATH
WING TIP PATH
TAIL TIP PATHNOTE:
TYPE 1 VALUES FOR MAX STEERING ANGLE = 72°.
APPROX 50.5 m(166 ft)
4.5 m(15 ft)
RUNWAY CENTERLINE
IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
4.5 m(15 ft)
F_AC_040503_1_0140101_01_01
180˚ Turn on a RunwayFIGURE-4-5-3-991-014-A01
4-5-3Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4 135˚ Turn - Taxiway to Taxiway
**ON A/C A330-200 A330-200F A330-300
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway.
4-5-4Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
FILLET R = 25.5 m(85 ft)
APPROX 13.6 m(45 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
APPROX 5.3 m(17 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
TAXIWAY CENTERLINE
(75 ft)23 m
NLG PATH
MLG PATH
F_AC_040504_1_0030101_01_01
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-4-991-003-A01
4-5-4Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
(75 ft)23 m
FILLET R = 25.5 m(85 ft)
APPROX 2.5 m(8 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE
TAXIWAY CENTERLINE
23 m(75 ft)
NLG PATH
MLG PATH
F_AC_040504_1_0070101_01_00
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-4-991-007-A01
4-5-4Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
(75 ft)23 m
FILLET R = 25.5 m(85 ft)
APPROX 13 m(43 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
APPROX 6.3 m(21 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
TAXIWAY CENTERLINE
NLG PATH
MLG PATH
F_AC_040504_1_0040101_01_01
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-4-991-004-A01
4-5-4Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
FILLET R = 25.5 m(85 ft)
APPROX 5.5 m(18 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
TAXIWAY CENTERLINE 23 m(75 ft)
(75 ft)23 m
NLG PATH
MLG PATH
F_AC_040504_1_0080101_01_00
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-4-991-008-A01
4-5-4Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5 90˚ Turn - Taxiway to Taxiway
**ON A/C A330-200 A330-200F A330-300
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-5Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
TAXIWAY CENTERLINE
(75 ft)
TAXIWAY CENTERLINEAPPROX 12.2 m
(40 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
APPROX 10.4 m(34 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m
23 m(75 ft)
NLG PATH
MLG PATH
F_AC_040505_1_0030101_01_01
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-5-991-003-A01
4-5-5Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
APPROX 3.8 m(12 ft)
4.5 m (15 ft) EDGE CLEARANCEADDITIONAL FILLET TO MEET
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
TAXIWAY CENTERLINE
(75 ft)23 m NLG PATH
MLG PATH
TAXIWAY CENTERLINE
23 m(75 ft)
F_AC_040505_1_0100101_01_00
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-5-991-010-A01
4-5-5Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
TAXIWAY CENTERLINE
TAXIWAY CENTERLINE
APPROX 13 m(43 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
APPROX 14.4 m(47 ft)
(75 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m
23 m(75 ft)
NLG PATH
MLG PATH
F_AC_040505_1_0040101_01_01
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE-4-5-5-991-004-A01
4-5-5Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
23 m(75 ft)
TAXIWAY CENTERLINE(20 ft)APPROX 6.2 m
FILLET R = 25.5 m(85 ft)
TAXIWAY CENTERLINE
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m(75 ft)
TURN R = 45 m(150 ft)
NLG PATH
MLG PATH
F_AC_040505_1_0110101_01_00
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-5-991-011-A01
4-5-5Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A330-200 A330-200F A330-300
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
4-6-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
6.1 m(20 ft)
6.1 m(20 ft)
COORDINATE WITH USING AIRPLANE FOR SPECIFICPLANNED OPERATING PROCEDURES.
NOTES:
12.2 m(40 ft)
45 m(150 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
23 m(75 ft)
190 m(625 ft)
90 m(300 ft)
HOLDINGPOINT
F_AC_040600_1_0010101_01_01
97.3 m(319 ft)
Runway Holding Bay (Apron)FIGURE-4-6-0-991-001-A01
4-6-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0 Aircraft Parking
**ON A/C A330-200 A330-200F A330-300
Airplane Parking
1. The following figures and charts show the rectangular space required for parking against the terminalbuilding.
The rectangle includes allowance for swinging the airplane on arrival and departure.- Steering Geometry- Minimum Parking Space Requirements
4-7-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
73.85
PARKING45° ENTRY PUSH OUT
PARKINGSTRAIGHT ENTRY PUSH BACK
PARKING90° ENTRY PUSH OUT
67.2356
.53 68
.26
82.5
7
96.76
F_AC_040700_1_0010101_01_00
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-001-A01
4-7-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
100.7773
.85
PARKINGPARALLEL IN POWER OUT
PARKING45° ENTRY POWER OUT
95.89
72.0
2
F_AC_040700_1_0020101_01_00
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-002-A01
4-7-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
0
20
40
60
80
100
120
140
160
180
200
220
240
260
280
300
10
20
30
40
50
60
70
80
90
100
0 10 20 30 40 50 60 70 80 90 100 110
0 20 40 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340
DISTANCE ALONG TERMINAL (m)
DISTANCE ALONG TERMINAL (ft)
(m)
DISTANCE OUTFROM TERMINAL
45° ENTRY PUSH OUT
STRAIGHT ENTRY PUSH BACK
PARALLEL IN POWER OUT
45° ENTRY POWER OUT
90° ENTRY PUSH OUT
F_AC_040700_1_0040101_01_00
Airplane ParkingMinimum Parking Space Requirements
FIGURE-4-7-0-991-004-A01
4-7-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
PARKINGSTRAIGHT ENTRY PUSH BACK
93.68
82.1
6
PARKING90° ENTRY PUSH OUT
63.89 75.3053
.39 66
.14
PARKING45° ENTRY PUSH OUT
F_AC_040700_1_0030101_01_00
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-003-A01
4-7-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
73.8
5PARKING
PARALLEL IN POWER OUT
PARKING45° ENTRY POWER OUT
99.42
95.89
71.3
6
F_AC_040700_1_0050101_01_00
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-005-A01
4-7-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F
0
20
40
60
80
100
120
140
160
180
200
220
240
260
280
300
10
20
30
40
50
60
70
80
90
100
0 10 20 30 40 50 60 70 80 90 100 110
0 20 40 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340
DISTANCE ALONG TERMINAL (m)
DISTANCE ALONG TERMINAL (ft)
(m)
DISTANCE OUTFROM TERMINAL
PARALLEL IN POWER OUT45° ENTRY POWER OUT
90° ENTRY PUSH OUT
STRAIGHT ENTRY PUSH BACK
45° ENTRY PUSH OUT
F_AC_040700_1_0060101_01_00
Airplane ParkingMinimum Parking Space Requirements
FIGURE-4-7-0-991-006-A01
4-7-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
**ON A/C A330-200 A330-200F A330-300
TERMINAL SERVICING
1. Terminal servicing
This chapter provides typical ramp layouts, corresponding minimum turnaround time estimations,locations of ground service points and service requirements.The information given in this chapter reflects ideal conditions. Actual ramp layouts and servicerequirements may vary according to local regulations, airline procedures and the airplane condition.
Section 5.1 shows typical ramp layouts for passenger aircraft at the gate or on an Open Apron andfreighter aircraft on an Open Apron.
Section 5.2 shows the minimum turnaround schedules for full servicing arrangements (turnroundstations).
Section 5.3 shows the minimum turnaround schedule for reduced servicing arrangements (en routestations).
Section 5.4 gives the locations of ground service connections, the standard of connections used andtypical capacities and requirements.
Section 5.5 provides the engine starting pneumatic requirements for different engine types anddifferent ambient temperatures.
Section 5.6 provides the air conditioning requirements for heating and cooling (pull-down and pull-up)using ground conditioned air for different ambient temperatures.
Section 5.7 provides the air conditioning requirements for heating and cooling to maintain a constantcabin air temperature using low pressure conditioned air.
Section 5.8 shows the ground towing requirements taking into account different ground surface andaircraft conditions.
5-0-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-0 Aircraft Servicing Arrangements
**ON A/C A330-200 A330-300
Airplane Servicing Arrangements
1. This section provides typical ramp layouts, showing the various GSE items in position during typicalturnaround scenarios for the passenger aircraft.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.
The associated turnaround station is given in the section 5-2-1 for Full Servicing Turn Round Charts.
The associated minimum turnaround time for Transit Turn Round Charts is given in a section 5-3-1.
5-1-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Airplane Servicing Arrangements
1. Airplane Servicing Arrangements
This section provides typical ramp layouts, showing the various GSE items in position during typicalturnaround scenarios for the passenger aircraft.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.
The associated turnaround station is given in the section 5-2-1 for Full Servicing Turn Round Charts.
5-1-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A330-200 A330-200F A330-300
Symbols Used on Servicing Diagrams
1. This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC AIR CONDITIONING UNITAS AIR START UNIT
BULK BULK TRAINCAT CATERING TRUCK
CB CONVEYOR BELTCLEAN CLEANING TRUCK
FUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNIT
LD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLE
MD CL (A330-200F only) MAIN DECK CARGO LOADER
PBB PASSENGER BOARDING BRIDGEPS PASSENGER STAIRS
TOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE
5-1-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2 Typical Ramp Layout - Open Apron
**ON A/C A330-200 A330-300
Typical Ramp Layout - Open Apron
1. This section gives the typical servicing arrangements on the open apron, for the passenger version ofthe aircraft.The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (24.61 ft) fromthe aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheelchocks in position on landing gears).
5-1-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
GPU
TOW
PS CAT
PS CAT
AS
CATPS
AC LD CL
LD CL
LV
WVULD BULK
FUEL
ULD
FUEL
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
CB
STAND SAFETY LINE
F_AC_050102_1_0010101_01_02
Typical Ramp LayoutOpen Apron
FIGURE-5-1-2-991-001-A01
5-1-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
GPU
TOW
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
CATPS
PS CAT
CATPS
AS
ULD
ULD
CB BULK
LV
FUELFUEL
ACLD CL
LD CL
WV
STAND SAFETY LINE
F_AC_050102_1_0070101_01_01
Typical Ramp LayoutOpen Apron
FIGURE-5-1-2-991-007-A01
5-1-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Typical Ramp Layout - Open Apron
1. This section gives the typical servicing arrangements on the open apron, for the cargo version of theaircraft.The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (24.61 ft) fromthe aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheelchocks in position on landing gears).
5-1-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
WV
PS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
GPU
AS
LD CL
ULD
BULKULDCB
FUELFUEL
TOW
STAND SAFETY LINE
MD CL
LV
ULDLD CL
AC
F_AC_050102_1_0020101_01_03
Typical Ramp LayoutOpen Apron
FIGURE-5-1-2-991-002-A01
5-1-2Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3 Typical Ramp Layout - Gate
**ON A/C A330-200 A330-300
Typical Ramp Layout - Gate
1. This section gives the typical servicing arrangements in the gate area for the passenger version of theaircraft, with two Passenger Boarding Bridges.The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (24.61 ft) fromthe aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheelchocks in position on landing gears).
5-1-3Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
CAT
CAT
CLEAN CAT
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
GP
U
AS
AC
ULDLD CL
LD CL
ULD
LV
BULKCB
FUELFUEL
PBB
PBB
TOW
WV
STAND SAFETY LINE
F_AC_050103_1_0010101_01_02
Typical Ramp LayoutGate
FIGURE-5-1-3-991-001-A01
5-1-3Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
AS
GP
U
AC LD CL
CAT
CAT
CAT
LD CL
LV
CLEAN
WV
BULK
ULD
CB
FUEL FUEL
PBB
PBB
TOW
ULD
STAND SAFETY LINE
F_AC_050103_1_0060101_01_01
Typical Ramp LayoutGate
FIGURE-5-1-3-991-006-A01
5-1-3Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0 Terminal Operations - Full Servicing
**ON A/C A330-300
Terminal Operations -- Full Servicing Turn-Round Time
1. This section provides typical turn-round time chart showing the typical times for ramp activitiesduring aircraft turn-round.Actual times may vary due to each operator’s specific practice and operating conditions.
2. Assumptions for full servicing turn-round time chart
A. PASSENGER HANDLING332 pax (30 B/C + 302 Y/C)All passengers deboard and board the aircraft2 Passenger Boarding Bridges (PBB) used at doors L1 and L2Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board
Deboarding:- 166 pax at door L1 (30 B/C and 136 Y/C)- 166 pax at door L2 (166 Y/C)- Deboarding rate = 25 pax/min per door- Priority deboarding for premium passengers
Boarding:- 166 pax at door L1 (30 B/C and 136 Y/C)- 166 pax at door L2 (166 Y/C)- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min
B. CARGO2 cargo loaders + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min
Cargo exchange:- 6 LD3 + 2 pallets in AFT cargo compartment- 12 LD3 + 2 pallets in FWD cargo compartment- 1 000 kg (2 205 lb) in bulk cargo compartment
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Pallet off-loading/loading times:- Off-loading = 2.4 min/pallet
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Loading = 2.8 min/pallet
Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t
C. REFUELLINGBlock-fuel quantity for nominal range through 2 nozzles90 000 l (23 775 US gal) at 50 psi (3.45 bar)Dispenser positioning/removal = 3 min
D. CLEANINGPerformed in available time
E. CATERING3 catering trucks for servicing galleys at doors R1, R2 and R4Equipment positioning + door opening = 5 minEquipment removal + door closing = 3 minFull Size Trolley Equivalent (FSTE) to unload and load: 39 FSTE- 8 FSTE at door R1- 13 FSTE at door R2- 18 FSTE at door R4Time for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING/SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min
Vehicle positioning/removal = 2 min (except for fuel and catering trucks)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesPotable water servicing: 100% uplift, 700 l (185 US gal) at 60 l/min (15.85 US gal/min)Toilet servicing: draining + rinsing
5-2-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
TRT: 55 min
100 20 30 40 50 60 70
AT L1DEBOARDING/BOARDING
HEADCOUNTING
CATERING AT R2
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
DEBOARDING/BOARDINGAT L2
CATERING AT R4
CARGO AFT CC
CATERING AT R1
AVAILABLE TIME
F_AC_050200_1_0010201_01_00
Full Servicing Turn-Round Time ChartFIGURE-5-2-0-991-001-B01
5-2-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
Terminal Operations -- Full Servicing Turn-Round Time
1. This section provides typical turn-round time chart showing the typical times for ramp activitiesduring aircraft turn-round.Actual times may vary due to each operator’s specific practice and operating conditions.
2. Assumptions for full servicing turn-round time chart
A. PASSENGER HANDLING293 pax (30 B/C + 263 Y/C)All passengers deboard and board the aircraft2 Passenger Boarding Bridges (PBB) used at doors L1 and L2Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board
Deboarding:- 146 pax at door L1 (30 B/C and 116 Y/C)- 147 pax at door L2 (147 Y/C)- Deboarding rate = 25 pax/min per door- Priority deboarding for premium passengers
Boarding:- 146 pax at door L1 (30 B/C and 116 Y/C)- 147 pax at door L2 (147 Y/C)- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min
B. CARGO2 cargo loaders + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min
Cargo exchange:- 6 LD3 + 2 pallets in AFT cargo compartment- 8 LD3 + 2 pallets in FWD cargo compartment- 1 000 kg (2 205 lb) in bulk cargo compartment
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Pallet off-loading/loading times:- Off-loading = 2.4 min/pallet- Loading = 2.8 min/pallet
5-2-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t
C. REFUELLINGBlock-fuel quantity for nominal range through 2 nozzles90 000 l (23 775 US gal) at 50 psi (3.45 bar)Dispenser positioning/removal = 3 min
D. CLEANINGPerformed in available time
E. CATERING3 catering trucks for servicing galleys at doors R1, R2 and R4Equipment positioning + door opening = 5 minEquipment removal + door closing = 3 minFull Size Trolley Equivalent (FSTE) to unload and load: 36 FSTE- 10 FSTE at door R1- 9 FSTE at door R2- 17 FSTE at door R4Time for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING/SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min
Vehicle positioning/removal = 2 min (except for fuel and catering trucks)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesPotable water servicing: 100% uplift, 700 l (185 US gal) at 60 l/min (15.85 US gal/min)Toilet servicing: draining + rinsing
5-2-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
TRT: 51 min
100 20 30 40 50 60 70
AT L1DEBOARDING/BOARDING
HEADCOUNTING
CATERING AT R2
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
DEBOARDING/BOARDINGAT L2
CATERING AT R4
CARGO AFT CC
CATERING AT R1
AVAILABLE TIME
F_AC_050200_1_0080101_01_00
Full Servicing Turn-Round Time ChartFIGURE-5-2-0-991-008-A01
5-2-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Terminal Operations - Full Servicing Turn-Round Time
1. This section provides typical turn-round time chart showing the typical times for ramp activitiesduring aircraft turn-round.Actual times may vary due to each operator’s specific practice and operating conditions.
2. Assumptions for full servicing turn-round time chart
A. COURIER HANDLING4 CouriersDoor used: L1
B. CARGO100% cargo exchangeMain deck cargo compartment: 22 palletsLower deck AFT cargo compartment: 4 palletsLower deck FWD cargo compartment: 2 LD3 + 4 palletsLower deck bulk cargo compartment: 1 000 kg (2 205 lb)
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Pallet off-loading/loading times:- Off-loading = 2.4 min/pallet- Loading = 2.8 min/pallet
Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t
C. REFUELLINGBlock-fuel quantity for nominal range through 2 nozzles90 000 l (23 775 US gal) at 50 psi (3.45 bar)Dispenser positioning/removal = 3 min
D. CLEANINGPerformed in available time
E. CATERINGCatering of galley (if installed) is performed through door L1 (standard units only) and inavailable time.
F. GROUND HANDLING/SERVICINGStart of operations:- Stairs: t0 = 0- Others: t0 + 1 min
5-2-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Vehicle positioning/removal = 2 min (fuel truck excluded)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesPotable water servicing: 100% uplift, 700 l (185 US gal) at 60 l/min (15.85 US gal/min)Toilet servicing: draining + rinsing
5-2-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
GSE POSITIONING/REMOVAL
ACTIVITY
TRT: 62 min
100 20 30 40 50 60 70
AT L1DEBOARDING/BOARDING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CATERING AT L1
CARGO AFT CC
CLEANING
CARGO MD
AVAILABLE TIME
AVAILABLE TIME
F_AC_050200_1_0090101_01_00
Full Servicing Turn-Round Time ChartFIGURE-5-2-0-991-009-A01
5-2-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0 Terminal Operations - Transit
**ON A/C A330-300
Terminal Operations - Minimum Servicing Turn-Round Time
1. This section provides typical turn-round time chart showing the typical times for ramp activitiesduring aircraft turn-round.Actual times may vary due to each operator’s specific practice and operating conditions.
2. Assumptions for minimum servicing turn-round time chart
A. PASSENGER HANDLING332 pax (30 B/C + 302 Y/C)50% of passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board
Deboarding:- 166 pax at door L1- Deboarding rate = 25 pax/min per door
Boarding:- 166 pax at door L1- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min
B. CARGO1 cargo loader + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min
Cargo exchange:- 5 LD3 in AFT cargo compartment- 500 kg (1 102 lb) in bulk cargo compartment
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t
C. REFUELLINGRefuelling through 2 nozzles30% of max capacity at 50 psi (3.45 bar)
5-3-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Dispenser positioning/removal = 3 min
D. CLEANINGPerformed in available time
E. CATERING1 catering truck for servicing galleys as requiredEquipment positioning + door opening = 5 minEquipment removal + door closing = 3 minPerformed in available timeTime for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING/SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min
Vehicle positioning/removal = 2 min (except for fuel and catering trucks)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesNo potable water servicingNo toilet servicing
5-3-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
TRT: 34 min
50 10 15 20 25 30 35
AT L1DEBOARDING/BOARDING
HEADCOUNTING
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CATERING
CARGO AFT CC
40
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
AVAILABLE TIME
F_AC_050300_1_0010201_01_00
Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-001-B01
5-3-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
Terminal Operations - Minimum Servicing Turn-Round Time
1. This section provides typical turn-round time chart showing the typical times for ramp activitiesduring aircraft turn-round.Actual times may vary due to each operator’s specific practice and operating conditions.
2. Assumptions for minimum servicing turn-round time chart
A. PASSENGER HANDLING293 pax (30 B/C + 263 Y/C)50% of passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board
Deboarding:- 147 pax at door L1- Deboarding rate = 25 pax/min per door
Boarding:- 147 pax at door L1- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min
B. CARGO1 cargo loader + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min
Cargo exchange:- 5 LD3 in AFT cargo compartment- 500 kg (1 102 lb) in bulk cargo compartment
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t
C. REFUELLINGRefuelling through 2 nozzles30% of max capacity at 50 psi (3.45 bar)Dispenser positioning/removal = 3 min
5-3-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
D. CLEANINGPerformed in available time
E. CATERING1 catering truck for servicing galleys as requiredEquipment positioning + door opening = 5 minEquipment removal + door closing = 3 minPerformed in available timeTime for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING/SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min
Vehicle positioning/removal = 2 min (except for fuel and catering trucks)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesNo potable water servicingNo toilet servicing
5-3-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
TRT: 32 min
50 10 15 20 25 30 35
AT L1DEBOARDING/BOARDING
HEADCOUNTING
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CATERING
CARGO AFT CC
40
AVAILABLE TIME
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
F_AC_050300_1_0040101_01_00
Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-004-A01
5-3-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1 Ground Service Connections Layout
**ON A/C A330-200 A330-300
Ground Service Connections Layout
1. This section gives the ground service connections layout.
5-4-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
1 17 2 3 6 7 11 3 14 15 16
16
15
143131017
111217
8
17
76
517
1 2 3 4
17
8
67
9
9
1 − OXYGEN SYSTEM2 − GROUND ELECTRICAL POWER CONNECTORS3 − POTABLE WATER DRAIN4 − LOW PRESSURE AIR PRE−CONDITIONING
AND ENGINE STARTING6 − ENGINE OIL FILLING7 − IDG OIL FILLING8 − PRESSURE REFUEL/DEFUEL COUPLINGS9 − OVERWING REFUEL
5 − HIGH PRESSURE AIR PRE−CONDITIONING12 − HYD RESERVOIR AIR PRESSURIZATION AND
GROUND POWER SUPPLY (BLUE)
14 − POTABLE WATER SERVICE PANEL15 − TOILET AND WASTE SERVICE PANEL16 − APU OIL FILLING17 − GROUNDING POINTS
13 − REFUEL/DEFUEL PANEL
11 − HYD RESERVOIR FILLING AND GROUND POWER SUPPLY (GREEN)
10 − HYDRAULIC GROUND POWER SUPPLY (YELLOW)
F_AC_050401_1_0010101_01_01
Ground Service Connections LayoutFIGURE-5-4-1-991-001-A01
5-4-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Ground Service Connections Layout
1. This section gives the ground service connections layout.
5-4-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
1 − OXYGEN SYSTEM2 − GROUND ELECTRICAL POWER CONNECTORS3 − LOW PRESSURE AIR PRE−CONDITIONING4 − HIGH PRESSURE AIR PRE−CONDITIONING
5 − ENGINE OIL FILLING6 − IDG OIL FILLING7 − PRESSURE REFUEL/DEFUEL COUPLINGS8 − OVERWING REFUEL9 − HYDRAULIC GROUND POWER SUPPLY (YELLOW)
AND ENGINE STARTING11 − HYD RESERVOIR AIR PRESSURIZATION AND
GROUND POWER SUPPLY (BLUE)
13 − POTABLE WATER SERVICE PANEL14 − TOILET AND WASTE SERVICE PANEL15 − APU OIL FILLING16 − GROUNDING POINTS
12 − REFUEL/DEFUEL PANEL
10 − HYD RESERVOIR FILLING AND GROUND POWER SUPPLY (GREEN)
14 16 2 1 13 5 6 10 15
15
16 2 1
14 13 3 4
56
7
816
56
78
16
16
129
11
16
10
F_AC_050401_1_0020101_01_02
Ground Service Connections LayoutFIGURE-5-4-1-991-002-A01
5-4-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2 Grounding Points
**ON A/C A330-200 A330-200F A330-300
Grounding Points
**ON A/C A330-200 A330-200F
1. Grounding Points.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
On Nose Landing Gear leg :6.67 m(21.88 ft) on centerline
1.40 m(4.59 ft)
On left Main Landing Gearleg :
28.37 m(93.08 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
On right Main LandingGear leg :
28.37 m(93.08 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).
B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for :- refuel/defuel operations.- maintenance operations.- bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.
**ON A/C A330-300
2. Grounding Points.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
5-4-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE : Meters (ft)
On Nose Landing Gear leg :6.67 m(21.88 ft) on centerline
1.40 m(4.59 ft)
On left Main Landing Gearleg :
31.53 m(103.44 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
On right Main LandingGear leg :
31.53 m(103.44 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).
B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for :- refuel/defuel operations.- maintenance operations.- bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.
5-4-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
(1)(2)
LANDINGGEAR
GROUND CABLE(OPTIONAL)
GROUNDINGPOINT
GROUNDINGPOINT
NOSE GEAR MAIN GEAR
AA
A
F_AC_050402_1_0010101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-001-A01
5-4-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
NOTE:
RIB22
RIB23
A
A
R SIDE SYMETRICAL
B
A
B
F_AC_050402_1_0020101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-002-A01
5-4-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3 Hydraulic System
**ON A/C A330-200 A330-200F A330-300
Hydraulic System
1. Ground Service Panels
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM GROUND
Green System:(Access Door197CB)
41.3 m(135.5 ft)
- 1.34 m(4.4 ft)
2.23 m(7.32 ft)
Yellow System:(Access Door196BB)
35.4 m(116.14 ft)
1.3 m(4.27 ft)
- 1.95 m(6.4 ft)
Blue System:(Access Door195BB)
34.41 m(112.89 ft)
- 1.28 m(4.2 ft)
1.94 m(6.36 ft)
2. Reservoir Pressurization
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM GROUND
One 1/4 in. self-sealing connectioncommon to the 3reservoirs(Blue SystemGround ServicePanel):(Access Door195BB)
34.47 m(113.09 ft)
- 1.41 m(4.63 ft)
1.89 m(6.2 ft)
**ON A/C A330-200 A330-200F
3. Accumulator Charging
Five connections (one for each accumulator):
5-4-3Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEANHEIGHTFROM
GROUNDYellow SystemAccumulator:(Access Door 196BB)
35.55 m(116.63 ft)
1.43 m(4.69 ft)
-1.91 m(6.27 ft)
Green SystemAccumulator:(Access Door 197CB)
41.52 m(136.22 ft)
-1.33 m(4.36 ft)
2.19 m(7.19 ft)
Blue System Accumulator:(Access Door 195BB)
34.54 m(113.32 ft)
-1.38 m(4.53 ft)
1.9 m(6.23 ft)
Blue System BrakeAccumulator:(Access Door 195BB)
34.54 m(113.32 ft)
-1.24 m(4.07 ft)
1.9 m(6.23 ft)
**ON A/C A330-300
4. Accumulator Charging
Five connections (one for each accumulator):
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEANHEIGHTFROM
GROUNDYellow SystemAccumulator:(Access Door 196BB)
35.55 m(116.63 ft)
1.43 m(4.69 ft)
-1.91 m(6.27 ft)
Green SystemAccumulator:(Access Door 197CB)
41.52 m(136.22 ft)
-1.33 m(4.36 ft)
2.19 m(7.19 ft)
Blue System Accumulator:(Access Door 195BB)
34.54 m(113.32 ft)
-1.38 m(4.53 ft)
1.9 m(6.23 ft)
Blue System BrakeAccumulator:(Access Door 195BB)
34.54 m(113.32 ft)
-1.18 m(3.87 ft)
1.9 m(6.23 ft)
5-4-3Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
5. Reservoir Filling
Two connections (one self-sealing connection for pressurized supply on the Green system groundservice panel).
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEANHEIGHTFROM
GROUNDOne handpump fillingconnection(Access Door 197CB)
41.31 m(135.53 ft)
-1.3 m
(4.27 ft)2.11 m(6.92 ft)
6. Reservoir Drain
One 3/8 in. self-sealing connection on the reservoir for:
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEANHEIGHTFROM
GROUND
Yellow System29.03 m(95.24 ft)
2.12 m(6.96 ft)
-2.4 m
(7.87 ft)
Green System33.17 m
(108.83 ft)-
0.7 m(2.3 ft)
3.8 m(12.47 ft)
Blue System29.03 m(95.24 ft)
-2.12 m(6.96 ft)
2.4 m(7.87 ft)
7. Ground Test
Three 1 in. self-sealing connections and three 1-1/2 in. self-sealing connections (one pair per system).
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEAN HEIGHTFROM
GROUNDGreen System GroundService Panel:(Access Door 197CB)
34.92 m(114.57 ft)
-1.35 m(4.43 ft)
2.2 m(7.22 ft)
5-4-3Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEAN HEIGHTFROM
GROUNDYellow System GroundService Panel:(Access Door 196BB)
29.03 m(95.24 ft)
1.3 m(4.27 ft)
-2 m
(6.56 ft)
Blue System GroundService Panel:(Access Door 195BB)
28.03 m(91.96 ft)
-1.28 m(4.2 ft)
2 m(6.56 ft)
5-4-3Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
MAN SELECTORVALVE−RSVR
FILLING
LEVER HANDPUMP
GND CNCTR−SELFSEALING RSVR
FILLING
HAND PUMPRSVR FILLING
FILTER−RSVRFILLING
RSVRFILLING VALVE
GND CNCTR−SELFSEALING, G SUCTION
GND CNCTR−SELFSEALING, G DELIVERY
VALVE−MANDEPRESS, G−RSVR
HYDRSVR FILLINGADJUSTMENT
INDICATOR
PRESS GAGEG POWER ACCU
GND CNCTRNITROGEN CHARGING
G POWER ACCU
FWD
A
FR53.4 FR53.5197CB
A
F_AC_050403_1_0010101_01_00
Ground Service ConnectionsGreen System Ground Service Panel
FIGURE-5-4-3-991-001-A01
5-4-3Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
PRESS GAGEB POWER ACCU
GND CNCTRNITROGENCHARGING
B POWER ACCU
GND CNCTRSELF−SEALING,
B SUCTION
VALVE−MANDEPRESS, B RSVR
GND CNCTR−SELFSEALING,
B DELIVERY
GND CNCTRSELF−SEALING,
B/Y RSVR PRESS
GND CNCTRSELF−SEALING,G RSVR PRESS
PRESS GAGESPARK BRK ACCU
PARK BRK ACCU
FWD
A
195BBFR44 FR45
A
F_AC_050403_1_0020101_01_00
Ground Service ConnectionsBlue System Ground Service Panel
FIGURE-5-4-3-991-002-A01
5-4-3Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
SIGHTGLASSCARGO DOOR
SELECTOR MANIFOLD
HAND PUMPCARGO DOORS, Y RAT STOW PANEL
GND CNCTR−SELFSEALING, Y SUCTION
VALVE−MANDEPRESS, Y RSVR
GND CNCTR−SELFSEALING, Y DELIVERY
PRESS GAGEY POWER ACCU
GND CNCTRNITROGEN CHARGING
Y POWER ACCU
FWD
A
196BBFR46FR47
A
F_AC_050403_1_0030101_01_00
Ground Service ConnectionsYellow System Ground Service Panel
FIGURE-5-4-3-991-003-A01
5-4-3Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4 Electrical System
**ON A/C A330-200 A330-200F A330-300
Electrical System
**ON A/C A330-200 A330-300
1. Electrical System
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
A/C External Power:Access Door 121EL
7.2 m(23.62 ft) On centerline
1.98 m(6.50 ft)
NOTE : Distances are approximate.
2. Technical Specifications
A. External Power Receptacles:- Two standard ISO 461 receptacles - 90 kVA each.
B. Power Supply:- Three-phase, 115 V, 400 Hz.
C. Electrical Connectors for Servicing:- AC outlets: HUBBELL 5258- DC outlets: HUBBELL 7472.
D. Electrical Loads in Ground ConfigurationIn ground configuration, in addition to the power necessary for maintenance, all the circuits,except those which are directly connected to the engines, are supplied as in flight. In theseconditions, the maximum power on the ground is approximately 105 kVA; this value does nottake into account the supply of the galleys, which according to the aircraft interior layout, mayreach 90 kVA.
E. Electrical Power necessary for Maintenance at Line Stop and Workshops:- Hydraulic electric-pumps: 20 × 3 kVA- Air Conditioning/ventilation: 49.5 kVA- Fuel pumps: 11.2 kVA- Lighting (commercial): 13.1 kVA- Lighting (technical): 2 kVA- Ice and rain protection: 11.3 kVA- Cargo loading: 12.6 kVA- AFS, flight controls, ADS, recorders: 3 kVA- Communications: 3.2 kVA
5-4-4Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Radio navigation: 1 kVA.
**ON A/C A330-200F
3. Electrical System
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
A/C External Power:Access Door 125EL
7.2 m(23.62 ft) On centerline
2.29 m(7.51 ft)
NOTE : Distances are approximate.
4. Technical Specifications
A. External Power Receptacles:- Two standard ISO 461 receptacles - 90 kVA each.
B. Power Supply:- Three-phase, 115 V, 400 Hz.
C. Electrical Connectors for Servicing:- AC outlets: HUBBELL 5258- DC outlets: HUBBELL 7472.
D. Electrical Loads in Ground ConfigurationIn ground configuration, in addition to the power necessary for maintenance, all the circuits,except those which are directly connected to the engines, are supplied as in flight. In theseconditions, the maximum power on the ground is approximately 105 kVA; this value does nottake into account the supply of the galleys, which according to the aircraft interior layout, mayreach 90 kVA.
E. Electrical Power necessary for Maintenance at Line Stop and Workshops:- Hydraulic electric-pumps: 20 × 3 kVA- Air Conditioning/ventilation: 49.5 kVA- Fuel pumps: 11.2 kVA- Lighting (commercial): 13.1 kVA- Lighting (technical): 2 kVA- Ice and rain protection: 11.3 kVA- Cargo loading: 12.6 kVA- AFS, flight controls, ADS, recorders: 3 kVA- Communications: 3.2 kVA- Radio navigation: 1 kVA.
5-4-4Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
B
FWD
FR19 FR18
B
A
A121EL
GROUND CONNECTOR925VU
F_AC_050404_1_0050101_01_00
Ground Service ConnectionsElectrical Service Panel
FIGURE-5-4-4-991-005-A01
5-4-4Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
EXTERNAL POWER RECEPTACLES
A
B
FWD
GROUND CONNECTOR
B
FR17
FR19125EL
FR17 FR19
A
925VU
F_AC_050404_1_0010201_01_00
Ground Service ConnectionsElectrical Service Panel
FIGURE-5-4-4-991-001-B01
5-4-4Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5 Oxygen System
**ON A/C A330-200 A330-200F A330-300
Oxygen System
**ON A/C A330-200 A330-300
1. Oxygen System
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEAN HEIGHTFROM
GROUNDOxygen Replenishment(Option 1):Access Door 811
2.5 m(8.2 ft)
0.53 m(1.74 ft)
-3.2 m(10.5 ft)
Oxygen Replenishment(Option 2):Access Door 811
2.5 m(8.2 ft)
0.68 m(2.23 ft)
- 3.2 m(10.5 ft)
- 0 -- Basic: External charging in the avionic compartment- 1 -- Option- 2 -- Option.Zero, one or two service connections (external charging in the avionics compartment) MS22066 Std.
NOTE : Internal charging connection provided.
**ON A/C A330-200F
2. Oxygen System
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Oxygen Replenishment:Access Panel 132NW
11.26 m(36.94 ft)
2.5 m(8.2 ft)
- 4.2 m(13.78 ft)
- Basic: External charging in the FWD cargo compartment.One service connection (external charging in the FWD cargo compartment) MS22066 Std.
NOTE : Internal charging connection provided.
5-4-5Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
BA
B
OXYGENFILLING PORT
TESTPORT
FR7
FR10
Z120
A
811
FWD
FR4
FR7
NOTE:THE NUMBER OF OXYGEN CYLINDERS DEPENDS ON THE SYSTEM CONFIGURATION.
F_AC_050405_1_0010101_01_00
Ground Service ConnectionsOxygen System
FIGURE-5-4-5-991-001-A01
5-4-5Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
OXYGENFILLING PORT
TESTPORTB
A
FR26
FR29
B
FR26132NW
NOTE:THE NUMBER OF OXYGEN CYLINDERS DEPENDS ON THE SYSTEM CONFIGURATION.
FR20
FR39.2
Z130
A
F_AC_050405_1_0020101_01_00
Ground Service ConnectionsOxygen System
FIGURE-5-4-5-991-002-A01
5-4-5Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6 Fuel System
**ON A/C A330-200 A330-200F A330-300
Fuel System
**ON A/C A330-200
1. Refuel/Defuel Access
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel Coupling,Left (Optional):Access Door 522HB
26.8 m(87.93 ft)
-12.6 m(41.34 ft)
5 m(16.4 ft)
Refuel/Defuel Coupling,Right:Access Door 622HB
26.8 m(87.93 ft)
12.6 m(41.34 ft)
-5 m(16.4 ft)
Overwing GravityRefuel Cap
31.3 m(102.69 ft)
17.2 m(56.43 ft)
17.2 m(56.43 ft)
5.8 m(19.03 ft)
A. Four standard 2.5 in. ISO 45 connections.
B. Two service connections (gravity refuel).
2. Refuel/Defuel Control Panel
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel ControlPanel:Access Door 198DB
31.1 m(102.03 ft)
0.8 m(2.62 ft)
-1.9 m(6.23 ft)
A. Flow rate: 1580 l/min (417 US gal/min) per connection.
B. Maximum pressure: 50 psi (3.45 bar).
5-4-6Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3. Overpressure Protector and NACA Flame Arrestor
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Overpressure Protector36.3 m(119.09 ft)
27.17 m(89.14 ft)
27.17 m(89.14 ft)
5.75 m(18.86 ft)
NACA Flame Arrestor35.94 m(117.91 ft)
26.53 m(87.04 ft)
26.53 m(87.04 ft)
5.7 m(18.7 ft)
**ON A/C A330-300
4. Refuel/Defuel Access
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel Coupling,Left (Optional):Access Door 522HB
30 m(98.43 ft)
-12.6 m(41.34 ft)
5 m(16.4 ft)
Refuel/Defuel Coupling,Right:Access Door 622HB
30 m(98.43 ft)
12.6 m(41.34 ft)
-5 m(16.4 ft)
Overwing GravityRefuel Cap
34.5 m(113.19 ft)
17.2 m(56.43 ft)
17.2 m(56.43 ft)
5.8 m(19.03 ft)
A. Four standard 2.5 in. ISO 45 connections.
B. Two service connections (gravity refuel).
5. Refuel/Defuel Control Panel
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel ControlPanel:Access Door 198DB
34.3 m(112.53 ft)
0.8 m(2.62 ft)
-1.9 m(6.23 ft)
A. Flow rate: 1580 l/min (417 US gal/min) per connection.
B. Maximum pressure: 50 psi (3.45 bar).
5-4-6Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6. Overpressure Protector and NACA Flame Arrestor
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Overpressure Protector39.48 m(129.53 ft)
27.17 m(89.14 ft)
27.17 m(89.14 ft)
5.75 m(18.86 ft)
NACA Flame Arrestor39.12 m(128.35 ft)
26.53 m(87.04 ft)
26.53 m(87.04 ft)
5.7 m(18.7 ft)
**ON A/C A330-200F
7. Refuel/Defuel Access
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel Coupling,Left (Optional):Access Door 522HB
26.8 m(87.93 ft)
-12.6 m(41.34 ft)
5.1 m(16.73 ft)
Refuel/Defuel Coupling,Right:Access Door 622HB
26.8 m(87.93 ft)
12.6 m(41.34 ft)
-5.1 m(16.73 ft)
Overwing GravityRefuel Cap
31.3 m(102.69 ft)
17.2 m(56.43 ft)
17.2 m(56.43 ft)
6.1 m(20.01 ft)
A. Four standard 2.5 in. ISO 45 connections.
B. Two service connections (gravity refuel).
8. Refuel/Defuel Control Panel
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel ControlPanel:Access Door 198DB
31.1 m(102.03 ft)
0.8 m(2.62 ft)
-1.9 m(6.23 ft)
A. Flow rate: 1580 l/min (417 US gal/min) per connection.
B. Maximum pressure: 50 psi (3.45 bar).
5-4-6Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
9. Overpressure Protector and NACA Flame Arrestor
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUND
Overpressure Protector36.3 m(119.09 ft)
27.17 m(89.14 ft)
27.17 m(89.14 ft)
5.75 m(18.86 ft)
NACA Flame Arrestor35.94 m(117.91 ft)
26.53 m(87.04 ft)
26.53 m(87.04 ft)
5.7 m(18.7 ft)
5-4-6Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
OVERPRESSURE PROTECTOR
A
NACA FLAME ARRESTOR
FWD
LH SIDE SHOWNRH SIDE SYMMETRICAL
A
A
RIB36
RIB37
RIB38
550EB(650EB)
550DB(650DB)
B
C
B
C
F_AC_050406_1_0020101_01_00
Overpressure Protector and NACA Flame ArrestorFIGURE-5-4-6-991-002-A01
5-4-6Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7 Pneumatic System
**ON A/C A330-200 A330-200F A330-300
Pneumatic System
**ON A/C A330-200 A330-200F
1. High Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEANHEIGHTFROM
GROUND20.72 m(67.98 ft)
-0.84 m(2.76 ft)
1.96 m(6.43 ft)HP Connectors:
Access door 193CB 21.08 m(69.16 ft)
- 0.84 m(2.76 ft)
1.94 m(6.36 ft)
A. Connectors:- Two standard 3 in. ISO 2026 connections.
2. Low Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEANHEIGHTFROM
GROUND19.29 m(63.29 ft)
-0.31 m(1.02 ft)
2.08 m(6.82 ft)LP Connectors:
Access door 191EB 19.29 m(63.29 ft)
- 0.76 m(2.49 ft)
2.11 m(6.92 ft)
A. Connectors:- Two standard 8 in. SAE AS4262 connections.
5-4-7Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
3. High Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEANHEIGHTFROM
GROUND23.9 m(78.41 ft)
- 0.84 m(2.76 ft)
1.79 m(5.87 ft)HP Connectors:
Access door 193CB 24.25 m(79.56 ft)
-0.84 m(2.76 ft)
1.79 m(5.87 ft)
A. Connectors:- Two standard 3 in. ISO 2026 connections.
4. Low Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEANHEIGHTFROM
GROUND22.48 m(73.75 ft)
-0.31 m(1.02 ft)
1.86 m(6.1 ft)LP Connectors:
Access door 191EB 22.48 m(73.75 ft)
-0.76 m(2.49 ft)
0.76 m(2.49 ft)
A. Connectors:- Two standard 8 in. SAE AS4262 connections.
5-4-7Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
193CB
191EB
A
B
A
FR40
HP CONNECTOR
B
LP CONNECTOR
F_AC_050407_1_0010101_01_00
Ground Service ConnectionsLP and HP Ground Connectors
FIGURE-5-4-7-991-001-A01
5-4-7Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8 Potable Water System
**ON A/C A330-300
Potable Water System
1. Potable Water System
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEANHEIGHTFROM
GROUND
Potable-Water Service Panel:Access Door 164AR
48.15 m(157.97 ft)
0.51 m(1.67 ft)
-3.15 m(10.33 ft)
FWD Drain Panel:Access Door 133BL
14.7 m(48.23 ft)
-0.6 m(1.97 ft)
1.9 m(6.23 ft)
AFT Drain Panel:Access Door 154AR
40.18 m(131.82 ft)
0.72 m(2.36 ft)
-2.46 m(8.07 ft)
NOTE : Distances are approximate.
2. Technical Specifications
A. Connections
(1) On the potable-water service panel (Access Door 164AR):- One heated 3/4 in. quick release filling connection- One heated 3/4 in. overflow and discharge connection- One ground pressurization connection.
(2) On the FWD drain panel (Access Door 133BL):- One standard 3/4 in. drain connection with back-up mechanical control.
(3) On the AFT drain panel (Access Door 154AR):- One standard 3/4 in. drain connection with back-up mechanical control- One standard 3/4 in. overflow and discharge connection with back-up mechanical
control.
B. Capacity- 700 l (184.92 US gal) standard- 1050 l (277.38 US gal) standard option.
C. Filling Pressure and Flow Rate
FWD tank:- Filling pressure: 50/125 psi (3.45/8.62 bar)- Flow rate: 45/73 l/min (11.89/19.28 US gal/min).
5-4-8Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AFT tank:- Filling pressure: 50/125 psi (3.45/8.62 bar)- Flow rate: 56/85 l/min (14.79/22.45 US gal/min).
5-4-8Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
164AR
154AR
133BL
A
B
C
DRAIN VALVECONTROL HANDLE
DRAIN NIPPLE
OVERFLOWNIPPLE
(FILL/DRAIN VALVE)OVERFLOW CONTROL HANDLE
(FILLING LINE DRAIN VALVE)DRAIN CONTROL HANDLE
DRAIN NIPPLE
FWD POTABLE−WATER DRAIN PANELAFT POTABLE−WATER DRAIN PANEL
CB
FR29
FR28
FR57.2
FR57.1
OVERFLOW NIPPLE
CAP
NIPPLE
CONTROL HANDLEFILL/DRAIN MAINTENANCE DOOR
LIMIT−SWITCH
FILL/DRAIN
A
POTABLE−WATER SERVICE PANEL
ASSEMBLY
GROUND AIRCONNECTION
FR70
FR69
F_AC_050408_1_0010101_01_00
Ground Service ConnectionsPotable-Water Ground Service Panels
FIGURE-5-4-8-991-001-A01
5-4-8Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
Potable Water System
1. Potable Water System
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEANHEIGHTFROM
GROUND
Potable-Water Service Panel:Access Door 164AR
48.15 m(157.97 ft)
0.51 m(1.67 ft)
-3.15 m(10.33 ft)
FWD Drain Panel:Access Door 133BL
14.7 m(48.23 ft)
- 0.6 m(1.97 ft)
1.9 m(6.23 ft)
AFT Drain Panel:Access Door 154AR
40.18 m(131.82 ft)
0.72 m(2.36 ft)
-2.46 m(8.07 ft)
NOTE : Distances are approximate.
2. Technical Specifications
A. Connections
(1) On the potable-water service panel (Access Door 164AR):- One heated 3/4 in. quick release filling connection- One heated 3/4 in. overflow and discharge connection- One ground pressurization connection.
(2) On the FWD drain panel (Access Door 133BL):- One standard 3/4 in. drain connection with back-up mechanical control.
(3) On the AFT drain panel (Access Door 154AR):- One standard 3/4 in. drain connection with back-up mechanical control- One standard 3/4 in. overflow and discharge connection with back-up mechanical
control.
B. Capacity- 700 l (184.92 US gal) standard- 1050 l (277.38 US gal) standard option.
C. Filling Pressure and Flow Rate
FWD tank:- Filling pressure: 50/125 psi (3.45/8.62 bar)- Flow rate: 45/73 l/min (11.89/19.28 US gal/min).
AFT tank:
5-4-8Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Filling pressure: 50/125 psi (3.45/8.62 bar)- Flow rate: 56/85 l/min (14.79/22.45 US gal/min).
5-4-8Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
164AR
154AR
133BL
A
B
C
DRAIN VALVECONTROL HANDLE
DRAIN NIPPLE
OVERFLOWNIPPLE
(FILL/DRAIN VALVE)OVERFLOW CONTROL HANDLE
(FILLING LINE DRAIN VALVE)DRAIN CONTROL HANDLE
DRAIN NIPPLE
FWD POTABLE−WATER DRAIN PANELAFT POTABLE−WATER DRAIN PANEL
CB
FR35
FR34
FR57
FR56
OVERFLOW NIPPLE
CAP
NIPPLE
CONTROL HANDLEFILL/DRAIN MAINTENANCE DOOR
LIMIT−SWITCH
FILL/DRAIN
APOTABLE−WATER SERVICE PANEL
ASSEMBLY
GROUND AIRCONNECTION
FR70
FR69
F_AC_050408_1_0030101_01_00
Ground Service ConnectionsPotable-Water Ground Service Panels
FIGURE-5-4-8-991-003-A01
5-4-8Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Potable Water System
1. Potable Water System
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
RH SIDE LH SIDE
MEANHEIGHTFROM
GROUND
Potable-Water Service Panel:Access Door 133BL
14.03 m(46.03 ft)
-0.76 m(2.49 ft)
2.64 m(8.66 ft)
NOTE : Distances are approximate.
2. Technical Specifications
A. Connections
(1) On the potable-water service panel (Access Door 133BL):- One heated 3/4 in. quick release filling connection- One heated 3/4 in. overflow and discharge connection- One ground pressurization connection.
(2) On the drain panel (Access Door 133BL):- One standard 3/4 in. drain connection with back-up mechanical control.
B. Capacity- 100 l (26.42 US gal).
C. Filling Pressure and Flow Rate- Filling pressure: 50 psi (3.45 bar)- Flow rate: 45 l/min (11.89 US gal/min).
5-4-8Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
OVERFLOW NIPPLE
CAP
NIPPLE
CONTROL HANDLEFILL/DRAIN
MAINTENANCE DOORLIMIT−SWITCH
FILL/DRAIN
APOTABLE−WATER SERVICE PANEL
ASSEMBLY
FR34
FR33
133BL
A
F_AC_050408_1_0040101_01_00
Ground Service ConnectionsPotable-Water Ground Service Panel
FIGURE-5-4-8-991-004-A01
5-4-8Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9 Oil System
**ON A/C A330-200 A330-200F A330-300
Oil System
1. Engine Oil Tank and IDG for PW 4000 series engine.
A. Engine Oil Replenishment :
One gravity filling cap and one pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
Engine Oil Filling:25.7 m
(84.32 ft)10.6 m
(34.78 ft)8.07 m
(26.48 ft)2.23 m(7.32 ft)
(1) Tank capacity :- Full level : 8.00 US gal (30.28 l).- Usable : 5.75 US gal (21.77 l).
B. IDG Oil Replenishment :
One pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
IDG Oil Pressure FillingConnection:
26.16 m(85.83 ft)
10.07 m(33.04 ft)
8.66 m(28.41 ft)
1.50 m(4.92 ft)
- Max delivery pressure required : 40 psi (2.76 bar).- Max OIL capacity of the IDG : 1.1 US gal (4.16 l).
2. Engine Oil Tank and IDG for RR Trent 700 series engine
A. Engine Oil Replenishment :
One gravity filling cap.
One ozone self sealing pressure fill and overfill connector per engine.
5-4-9Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
Engine Oil Filling:23.9 m
(78.41 ft)7.92 m
(25.98 ft)10.82 m(35.50 ft)
2.05 m(6.73 ft)
(1) Tank capacity :- Full level : 7.18 US gal (27.18 l.- Usable : 6.00 US gal (22.71 l).
B. IDG Oil Replenishment :
One ozone self sealing pressure fill and overfill connector per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
IDG Oil Pressure FillingConnection:
24.38 m(79.99 ft)
9.65 m(31.66 ft)
9.09 m(29.82 ft)
0.8 m(2.62 ft)
- Max delivery pressure required : 40 psi (2.76 bar).- Max OIL capacity of the IDG : 1.12 US gal (4.24 l).
**ON A/C A330-200 A330-300
3. Engine Oil Tank and IDG for GE CF6-80E1 series engine
A. Engine Oil Replenishment :
One gravity filling cap and one pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
Engine Oil Filling:24.93 m(81.79 ft)
10.00 m(32.81 ft)
8.73 m(28.64 ft)
1.71 m(5.61 ft)
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Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(1) Tank capacity :- Full level : 6.49 US gal (24.57 l).- Usable : 6.09 US gal (23.05 l).
B. IDG Oil Replenishment :
One pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
IDG Oil Pressure FillingConnection:
23.03 m(75.56 ft)
7.96 m(26.12 ft
10.77 m(35.33 ft)
2.35 m(7.71 ft)
- Max delivery pressure required : 40 psi (2.76 bar).- Max OIL capacity of the IDG : 1.1 US gal (4.16 l).
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Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
YELLOW
GREEN
OIL LEVELSIGHTGLASS
OIL TANKCAP
DUSTCOVER
OVERFLOWCONNECTOR
PRESSUREFILL
VALVE
PRESSUREFILL
CONNECTOR
OIL TANK
FULL
1 QT
2 QT
3 QT
FULL
−1 QT
−2 QT
−3 QT
AB
B
FULL
−1 QT
−2 QT
−3 QTCLOSE
OPEN
A
F_AC_050409_1_0010101_01_00
Ground Service ConnectionsEngine Oil Tank - PW 4000 series engine
FIGURE-5-4-9-991-001-A01
5-4-9Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
1 OIL FILLER CAP
2 OVERFLOW COUPLING
3 PRESSURE FILLCOUPLING
D5324
A
B
B
FULL FULL
LIT
RE
S R
EQ
UIR
ED
US
QU
AR
TZ
RE
QU
IRE
D
5
4
3
2
1
5
4
3
2
1
A
F_AC_050409_1_0020101_01_00
Ground Service ConnectionsEngine Oil Tank - RR Trent 700 series engine
FIGURE-5-4-9-991-002-A01
5-4-9Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
SIGHT GLASS
TANK FULL
TANK NOT FULLSCUPPER
DRAIN
RELIEFVALVE
OVERFILLPORT
ENGINEOIL TANKFILLER CAP
PRESSUREFILL PORT
5000EN
ENGINE OILTANK
A
B
B
A
F_AC_050409_1_0030101_01_00
Ground Service ConnectionsEngine Oil Tank - GE CF6-80E1 series engine
FIGURE-5-4-9-991-003-A01
5-4-9Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
RED
YELLOW
GREEN
RED
2
1
PRESSUREFILL VALVE
CONNECTOR
OVERFLOWDRAIN VALVECONNECTOR
OIL LEVELSIGHTGLASS
OIL DIFFERENTIALPRESSUREINDICATOR
A
B
A
B
OVER FULL
ADDOIL
F_AC_050409_1_0040101_01_00
Ground Service ConnectionsIDG Oil Tank - PW 4000 series engine
FIGURE-5-4-9-991-004-A01
5-4-9Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
OVER FULL
ADDOIL
RED
YELLOW
GREEN
RED
1 SIGHT GLASS
2 DRAIN PLUG
3 OVERFILL DRAIN CONNECTOR
4 PRESSURE FILL CONNECTOR
A
A
F_AC_050409_1_0050101_01_00
Ground Service ConnectionsIDG Oil Tank - RR Trent 700 series engine
FIGURE-5-4-9-991-005-A01
5-4-9Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
1
A
A
B
PRESSUREFILL VALVE
CONNECTOR
OVERFLOWDRAIN VALVECONNECTOR
5
3
B
A
F_AC_050409_1_0060101_01_00
Ground Service ConnectionsIDG Oil Tank - GE CF6-80E1 series engine
FIGURE-5-4-9-991-006-A01
5-4-9Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
APU Oil System
**ON A/C A330-200 A330-200F
1. APU Oil SystemAPU oil gravity filling cap.
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM GROUND
APU OilReplenishment:Access Doors316AR, 315AL
55 m(180.45 ft)
-0.4 m(1.31 ft)
8 m(26.25 ft)
A. Tank capacity (usable):- APU Type: 331-350: 7.3 l (1.93 US gal).
**ON A/C A330-300
2. APU Oil SystemAPU oil gravity filling cap.
DISTANCEFROM AIRCRAFT CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM GROUND
APU OilReplenishment:Access Doors316AR, 315AL
60.3 m(197.83 ft)
- 0.4 m(1.31 ft)
8 m(26.25 ft)
A. Tank capacity (usable):- APU Type: 331-350: 7.3 l (1.93 US gal).
5-4-9Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
F_AC_050409_1_0070101_01_01
FR95
316AR
315AL
FR101
A
PRESSURE FILLOVERFLOW PORT
OIL SCUPPER
GRAVITY FILLPORT
LUBRIFICATION OIL FILTER
GENERATOR SCAVENGE OIL FILTER
OIL PUMPMODULE5100KT9
A
B
OIL FILLERCAP
OVERFLOW PORT
PRESSUREFILL PORT
OIL SIGHTGLASS
OIL SCUPPER
GRAVITY FILL PORT
B
DO NOT REMOVE OILFILLER CAP WHEN OILLEVEL IS ABOVE FULLMARK ON SIGHT GLASS
FWD
Ground Service ConnectionsAPU Oil Servicing
FIGURE-5-4-9-991-007-A01
5-4-9Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10 Vacuum Toilet System
**ON A/C A330-200 A330-200F A330-300
Vacuum Toilet System
**ON A/C A330-200
1. Vacuum Toilet System
DISTANCEFROM AIRPLANE CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUNDWaste Water GroundService Panel:Access Door 171AL
44.66 m(146.52 ft)
-0.09 m(0.3 ft)
3.6 m(11.81 ft)
A. Waste water ground service panel comprising:- Standard: One standard 4 in. drain connection and two 1 in. flushing connections- Standard option: One standard 4 in. drain connection and three 1 in. flushing connections.
B. Capacity waste tanks:- Standard: 700 l (184.92 US gal)- Standard option: 1050 l (277.38 US gal).
C. Chemical fluid:- Standard: 36 l (9.51 US gal)- Standard option: 54 l (14.27 US gal).
**ON A/C A330-300
2. Vacuum Toilet System
DISTANCEFROM AIRPLANE CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUNDWaste Water GroundService Panel:Access Door 171AL
50 m(164.04 ft)
-0.09 m(0.3 ft)
3.6 m(11.81 ft)
A. Waste water ground service panel comprising:- Standard: One standard 4 in. drain connection and two 1 in. flushing connections- Standard option: One standard 4 in. drain connection and three 1 in. flushing connections.
B. Capacity waste tanks:- Standard: 700 l (184.92 US gal)
5-4-10Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Standard option: 1050 l (277.38 US gal).
C. Chemical fluid:- Standard: 36 l (9.51 US gal)- Standard option: 54 l (14.27 US gal).
**ON A/C A330-200F
3. Vacuum Toilet System
DISTANCEFROM AIRPLANE CENTERLINE
AFT OF NOSERH SIDE LH SIDE
MEAN HEIGHTFROM
GROUNDWaste Water GroundService Panel 1:Access Door 121EL
5.49 m(18.01 ft)
-1.43 m(4.69 ft)
2.95 m(9.68 ft)
Waste Water GroundService Panel 2:Access Door 121FL
5.98 m(19.62 ft)
-1.69 m(5.54 ft)
3.15 m10.33 ft)
A. There are two waste water ground service panels:- First panel: One standard connection Roylyn 1 in. for flushing and filling- Second panel: One standard Taco type valve 4 in. for draining.
NOTE : Handle used for drainage is located on the first panel.
B. Capacity waste tanks:- Standard: 35 l (9.25 US gal).
C. Chemical fluid:- Standard: 9.5 l (2.51 US gal).
5-4-10Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
LIMIT SWITCHWASTE−PANEL
RINSE CONNECTIONTANK 2 FILL AND
TANK 1 FILL ANDRINSE CONNECTION
WASTEDRAIN−LINE VALVE
DRAIN−VALVECONTROL LEVERS
FR75
FR59
FR74 FR73
A
A
FWD
171AL
OPEN
CLOSE
LH RH
F_AC_050410_1_0010101_01_00
Ground Service ConnectionsWaste Water Ground Service Panel
FIGURE-5-4-10-991-001-A01
5-4-10Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
FR14
FR16
FR20
FR12
121FL121EL
A
B
FR15A FR16LIMIT SWITCH
WASTE−PANEL
WASTEDRAIN−LINE VALVE
A
FWD
DRAIN−VALVECONTROL LEVER LIMIT SWITCH
WASTE−PANEL
TANK FILL ANDRINSE CONNECTION
DRAINAGE OFLEAK PROTECTION
B
FWD
FR14A FR15
OPEN
CLOSE
F_AC_050410_1_0040101_01_00
Ground Service ConnectionsWaste Water Ground Service Panel
FIGURE-5-4-10-991-004-A01
5-4-10Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A330-200 A330-200F A330-300
Engine Starting Pneumatic Requirements
1. The purpose of this section is to provide the minimum air data requirements at the aircraftconnection, needed to start the engine within no more than 90 seconds, at sea level (0 feet), for a setof Outside Air Temperatures (OAT).
ABBREVIATION DEFINITION
A/C Aircraft
ASU Air Start UnitHPGC High Pressure Ground Connection
OAT Outside Air Temperature
A. Air data (discharge temperature, absolute discharge pressure) are given at the HPGC.
B. For the requirements below, the configuration with two HPGC is used. Using one connector only(for a given mass flow rate and discharge pressure from the ASU) will increase the pressure lossin the ducts of the bleed system and therefore lower the performances at the engine starter.
C. For a given OAT the following charts are used to determine an acceptable combination for airdischarge temperature, absolute discharge pressure and mass flow rate.
D. This section is addressing requirements for the ASU only, and is not representative of the startperformance of the aircraft using the APU or engine cross bleed procedure.
E. To protect the A/C, the charts feature, if necessary:- The maximum discharge pressure at the HPGC- The maximum discharge temperature at the HPGC.
5-5-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
AIR
FLO
W (
kg/m
in)
AIR
FLO
W (
lb/m
in)
AB
SO
LUT
E P
RE
SS
UR
E (
psia
)
0 10 20 30 40 50 60
GE CF6−80E1 SERIES/SEA LEVELSTARTING TIME: LESS THAN 70 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
OUTSIDE AIR TEMPERATURE OAT (° C)
OUTSIDE AIR TEMPERATURE OAT (° F)
−10−20−30−40−50
0 20 40 60 80 100 120 140−20−40
NOTE:IN CASE THE ACTUAL DISCHARGE TEMPERATURE OF THE ASU DIFFERS SUBSTANTIALLY FROM THE ONES GIVEN IN THE CHARTS, A SIMPLE INTERPOLATION (LINEAR) IS SUFFICIENT TO DETERMINE THE REQUIRED AIR DATA.
EXAMPLE:FOR AN OAT OF 15° C (59° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 150° C (302° F) AT HPGC:− THE REQUIRED PRESSURE AT HPGC IS 23.75 psia− THE REQUIRED AIRFLOW AT HPGC IS 43 kg/min.
EXAMPLE:FOR AN OAT OF 15° C (59° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 195° C (383° F) AT HPGC, INTERPOLATING BETWEEN THE LINES 150° C (302° F) AND 220° C (428° F) RESULTS IN:− A REQUIRED PRESSURE AT HPGC OF 22.5 psia− A REQUIRED AIRFLOW AT HPGC OF 39.5 kg/min.
40
35
30
25
20
30 35 40
40
45
50
55
60
65
70
75
90
100
110
120
130
140
150
160
352520
80
ABSOLUTE PRESSURE (psia)
OAT = 100° C (212° F)OAT = 150° C (302° F)OAT = 220° C (428° F) MAX.
F_AC_050500_1_0010101_01_01
Example for Use of the ChartsFIGURE-5-5-0-991-001-A01
5-5-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
AIR
FLO
W (
kg/m
in)
AIR
FLO
W (
lb/m
in)
AB
SO
LUT
E P
RE
SS
UR
E (
psia
)
GE CF6−80E1 SERIES/SEA LEVELSTARTING TIME: LESS THAN 70 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
OUTSIDE AIR TEMPERATURE OAT (° C)
OUTSIDE AIR TEMPERATURE OAT (° F)0 20 40 60 80 100 120 140−20−40
30 35 40
40
45
50
55
60
65
70
75
90
100
110
120
130
140
150
160
352520
80
40
0 10 20 30 40 50 60−10−20−30−40−50
35
30
25
20
ABSOLUTE PRESSURE (psia)
OAT = 100° C (212° F)OAT = 150° C (302° F)OAT = 220° C (428° F) MAX.
F_AC_050500_1_0040101_01_00
Engine Starting Pneumatic RequirementsGE CF6-80E1 Series EngineFIGURE-5-5-0-991-004-A01
5-5-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
AIR
FLO
W (
kg/m
in)
AIR
FLO
W (
lb/m
in)
AB
SO
LUT
E P
RE
SS
UR
E (
psia
)
ROLLS ROYCE TRENT 700 SERIES/SEA LEVELSTARTING TIME: LESS THAN 90 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
OUTSIDE AIR TEMPERATURE OAT (° C)
OUTSIDE AIR TEMPERATURE OAT (° F)
190
200
210
220
230
240
8045
180
50 55 60
90
100
110
120
130
140
65
4040
60
55
50
45
3020100−10−20−30−40−50−60
0 20 40 60 80 100−20−40−60
ABSOLUTE PRESSURE (psia)
OAT = 85° C (185° F)OAT = 150° C (302° F)OAT = 220° C (428° F) MAX.
F_AC_050500_1_0050101_01_00
Engine Starting Pneumatic RequirementsRolls Royce Trent 700 Series Engine
FIGURE-5-5-0-991-005-A01
5-5-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
AIR
FLO
W (
kg/m
in)
AIR
FLO
W (
lb/m
in)
AB
SO
LUT
E P
RE
SS
UR
E (
psia
)
PRATT & WHITNEY PW4000 SERIES/SEA LEVELSTARTING TIME: LESS THAN 80 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
OUTSIDE AIR TEMPERATURE OAT (° C)
OUTSIDE AIR TEMPERATURE OAT (° F)0 20 40 60 80 100 120 140−20−40
6030
140
70
80
90
100
110
120
35 40 45 50 55
160
180
200
220
240
260
50
0 10 20 30 40 50 60−10−20−30−40−50
45
40
35
30
ABSOLUTE PRESSURE (psia)
OAT = 85° C (185° F)OAT = 135° C (275° F)OAT = 220° C (428° F) MAX.
F_AC_050500_1_0060101_01_00
Engine Starting Pneumatic RequirementsPratt & Whitney PW4000 Series Engine
FIGURE-5-5-0-991-006-A01
5-5-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A330-200 A330-200F A330-300
Ground Pneumatic Power Requirements
1. GeneralThis section describes the required performance for the ground equipment to maintain the cabintemperature at 27˚C (80.6˚F) after boarding (Section 5.7 - steady state), and provides the timeneeded to cool down or heat up the aircraft cabin to the required temperature (Section 5.6 - dynamiccases with aircraft empty).
ABBREVIATION DEFINITION
A/C Aircraft
AHM Aircraft Handling Manual
GC Ground ConnectionGSE Ground Service Equipment
IFE In-Flight Entertainment
LP Low PressureOAT Outside Air Temperature
A. The air flow rates and temperature requirements for the GSE, provided in Sections 5.6 and 5.7,are given at A/C ground connection.
NOTE : The maximum air flow is driven by pressure limitation at the ground connection.
B. The air flow rates and temperature requirements for the GSE are given for the A/C in theconfiguration ”2 LP ducts connected”.
NOTE : The cooling capacity of the equipment (kW) is only indicative and is not sufficient byitself to ensure the performance (outlet temperature and flow rate combinations arethe requirements needed for ground power).An example of cooling capacity calculation is given in Section 5.7.
C. For temperatures at ground connection below +2˚C (+35.6˚F) (Subfreezing), the groundequipment shall be compliant with the Airbus document ”Subfreezing PCA Carts -- ComplianceDocument for Suppliers” (contact Airbus to obtain this document) defining all the requirementswith which Subfreezing Pre-Conditioning Air equipment must comply to allow its use on Airbusaircraft. These requirements are in addition to the functional specifications included in the IATAAHM997.
2. Ground Pneumatic Power RequirementsThis section provides the ground pneumatic power requirements for:- Heating (pull up) the cabin, initially at OAT, up to 21˚C (69.8˚F) FIGURE 5---0-99--001-A- Cooling (pull down) the cabin, initially at OAT, down to 27˚C (80.6˚F) FIGURE 5---0-99--003-
A.
5-6-0Page 1
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@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
30 60 90 120 1500.8
1.2
1.4
1.6
1.8
2.2
2.4
2.0
2.5
3.0
3.5
4.0
4.5
5.0
AIR
FLO
W A
T G
C (
kg/s
)
AIR
FLO
W A
T G
C (
lb/s
)
PULL UP PERFORMANCE
TIME TO HEAT CABIN TO +21° C (+69.8° F) ON GROUND (min)
OAT ISA −38° C (−36.4° F); GC OUTLET +70° C (+158° F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
40 50 70 80 100 110 130 140
MAXIMUM AIR FLOW
1.0
2.0
F_AC_050600_1_0010101_01_00
Ground Pneumatic Power RequirementsHeating
FIGURE-5-6-0-991-001-A01
5-6-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
NOTE:ONLY SUPPLY TEMPERATURE ABOVE +2° C (+35.6° F) (NO SUBFREEZING) FOR THE A330−200F.
30 60 90 120 1500.8
1.2
1.4
1.6
1.8
2.2
2.4
2.0
2.5
3.0
3.5
4.0
4.5
5.0
AIR
FLO
W A
T G
C (
kg/s
)
AIR
FLO
W A
T G
C (
lb/s
)
PULL DOWN PERFORMANCE
TIME TO COOL CABIN TO +27° C (+80.6° F) ON GROUND (min)
OAT ISA +23° C (+73.4° F); GC OUTLET +2° C (+35.6° F); EMPTY CABIN; IFE OFF; SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
OAT ISA +23° C (+73.4° F); GC OUTLET −10° C (+14° F); EMPTY CABIN; IFE OFF; SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
40 50 70 80 100 110 130 140
MAXIMUM AIR FLOW
2.0
1.0
F_AC_050600_1_0030101_01_00
Ground Pneumatic Power RequirementsCooling
FIGURE-5-6-0-991-003-A01
5-6-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A330-200 A330-200F A330-300
Preconditioned Airflow Requirements
1. This section provides the preconditioned airflow rate and temperature needed to maintain the cabintemperature at 27 ˚C (80.6 ˚F).
These settings are not intended to be used for operation (they are not a substitute for the settingsgiven in the AMM). They are based on theoretical simulations and give the picture of a real steadystate. The purpose of the air conditioning operation (described in the AMM) is to maintain the cabintemperature below 27 ˚C (80.6 ˚F) during boarding (therefore it is not a steady state).
5-7-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
AIR
FLO
W A
T G
C (
kg/s
)
−150.8
AIR
FLO
W A
T G
C (
lb/s
)
1.0
1.2
1.4
1.6
1.8
2.0
2.2
2.4
−10 −5 0 5 10 15 20 25 30 35 40 45 50 55 60
2.0
2.5
3.0
3.5
4.0
4.5
5.0
0 10 20 30 40 50 60 70 80
INLET TEMPERATURE AT GC (° C)
INLET TEMPERATURE AT GC (° F)
MAXIMUM AIRFLOW
COOLING/HEATING PERFORMANCE
SETTINGS NOTINTENDED TO BE USED
FOR OPERATION
OAT ISA; EMPTY CABIN; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON; GALLEYS ON
OAT ISA −38° C (−36.4° F); EMPTY CABIN; IFE OFF; LIGHTS ON; NO SOLAR LOAD; RECIRCULATIONFANS ON; GALLEYS OFF
C H
EXAMPLE:COOLING CAPACITY CALCULATION:FOR THE CONDITIONS "C", THE COOLING CAPACITY OF 1.9 kg/s x 1 kJ/(kg.° C) x (27− 5) = 41.8 kW(OR 12.5 TONS COOLING CAPACITY) IS NEEDED TO MAINTAIN THE CABIN TEMPERATURE AT 27° C (80.6° F)(1.9 kg/s AT 5° C (41° F) FOR AIR AT GC INLET).
NOTE:ONLY SUPPLY TEMPERATURE ABOVE +2° C (+35.6° F) (NO SUBFREEZING) FOR THE A330−200F.
90 100 110 120 130 140
F_AC_050700_1_0010101_01_03
Preconditioned Airflow RequirementsFIGURE-5-7-0-991-001-A01
5-7-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A330-200 A330-200F A330-300
Ground Towing Requirements
1. This section provides information on aircraft towing.
The A330 is designed with means for conventional or towbarless towing.Information/procedures can be found for both in chapter 9 of the Aircraft Maintenance Manual.Status on towbarless towing equipment qualification can be found in SIL 09-002.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a towbar attached to the nose gear leg (refer to AMM chapter 9 for conditions andlimitations). One towbar fitting is installed at the front of the leg (optional towing fitting for towingfrom the rear of the NLG available).The Main Landing Gears have attachment points for towing or debogging (for details, refer tochapter 7 of the Aircraft Recovery Manual).
This section shows the chart to determine the draw bar pull and tow tractor mass requirements as afunction of the following physical characteristics:- Aircraft weight,- Number of engines at idle,- Slope.
The chart is based on the A330 engine type with the biggest idle thrust.The chart is therefore valid for all A330 models.
2. Towbar design guidelines
The aircraft towbar shall comply with the following standards:- SAE AS 1614, ”Main Line Aircraft TowBar Attach Fitting Interface”,- SAE ARP 1915, ”Aircraft TowBar”,- ISO 8267-1, ”Aircraft - Towbar attachment fitting - Interface requirements - Part 1: Main line
aircraft”,- ISO 9667, ”Aircraft ground support equipment - Towbars”,- IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Towbar”.
A conventional type towbar is required which should be equipped with a damping system (to protectthe nose gear against jerks) and with towing shear pins:- A traction shear pin calibrated at 28 620 daN (64 340 lbf),- A torsion pin calibrated at 3 130 m.daN (276 991 lbf.in).The towing head is designed according to SAE AS 1614, cat. III.
5-8-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
50
45
40
35
30
25
20
15
10
5
00 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0
TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]
DRAWBAR PULL [ t ]
WET C
ONCRETE =
0.57
HARD SNOW = 0.2
ICE = 0.05
DRY CO
NCRETE
=
0.8
A/C WEIGHT [ t ]
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A330 AT 230 t, AT 1.5% SLOPE,1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (230 t),− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),− FROM THIS POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL NO OF ENGINES AT IDLE = 2,− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER OF ENGINES (1),− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (18.8 t),− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (32.9 t).
AT IDLE
F_AC_050800_1_0020101_01_01
230210190170150130110
18.8
32.9
1 ENGINE ON
230 tons1.5% SLOPE
BREAKWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 1 500 daN
Ground Towing RequirementsFIGURE-5-8-0-991-002-A01
5-8-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0 De-Icing and External Cleaning
**ON A/C A330-200 A330-200F A330-300
De-Icing and External Cleaning
1. De-Icing and External Cleaning on GroundThe mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heightsup to approximately 17 m (56 ft).
**ON A/C A330-200 A330-200F
2. De-Icing
Wing Top Surface(Both Sides)
Wingtip Devices(Both Inside andOutside Surfaces)
(Both Sides)
HTP Top Surface(Both Sides)
VTP(Both Sides)AIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A330-200/-200F306 3 294 11 118 65 700 106 1 141
Fuselage Top Surface(Top Third - 120˚ Arc)
Nacelle and Pylon(Top Third - 120˚ Arc)
(All Engines)Total De-Iced AreaAIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2
A330-200/-200F 288 3 100 46 495 821 8 837
NOTE : Dimensions are approximate.
**ON A/C A330-300
3. De-Icing
Wing Top Surface(Both Sides)
Wingtip Devices(Both Inside andOutside Surfaces)
(Both Sides)
HTP Top Surface(Both Sides)
VTP(Both Sides)AIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A330-300 306 3 294 11 118 65 700 91 980
5-9-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Fuselage Top Surface(Top Third - 120˚ Arc)
Nacelle and Pylon(Top Third - 120˚ Arc)
(All Engines)Total De-Iced AreaAIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2
A330-300 319 3 434 46 495 838 9 020
NOTE : Dimensions are approximate.
**ON A/C A330-200
4. External Cleaning
Wing Top Surface(Both Sides)
Wing LowerSurface
(Including FlapTrack Fairing)(Both Sides)
Wingtip Devices(Both Inside andOutside Surfaces)
(Both Sides)
HTP Top Surface(Both Sides)
HTP LowerSurface
(Both Sides)AIRCRAFTTYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2 m2 ft2
A330-200/-200F306 3 294 345 3 714 11 118 65 700 65 700
VTP(Both Sides)
Fuselage andBelly Fairing
Nacelle and Pylon(All Engines) Total Cleaned AreaAIRCRAFT
TYPEm2 ft2 m2 ft2 m2 ft2 m2 ft2
A330-200/-200F106 1 141 877 9 440 154 1 658 1 940 20 882
NOTE : Dimensions are approximate.
**ON A/C A330-300
5. External Cleaning
Wing Top Surface(Both Sides)
Wing LowerSurface
(Including FlapTrack Fairing)(Both Sides)
Wingtip Devices(Both Inside andOutside Surfaces)
(Both Sides)
HTP Top Surface(Both Sides)
HTP LowerSurface
(Both Sides)AIRCRAFTTYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2 m2 ft2
A330-300 306 3 294 345 3 714 11 118 65 700 65 700
5-9-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
VTP(Both Sides)
Fuselage andBelly Fairing
Nacelle and Pylon(All Engines) Total Cleaned AreaAIRCRAFT
TYPEm2 ft2 m2 ft2 m2 ft2 m2 ft2
A330-300 91 980 971 10 452 154 1 658 2 016 21 700
NOTE : Dimensions are approximate.
5-9-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities and Temperatures
1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway, Maximum Takeoff conditions.
6-1-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities Contours - Ground Idle Power
1. This section gives engine exhaust velocities contours at ground idle power
6-1-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
0 60 (18) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
NA
IRP
LAN
EC L
CO
NV
ER
SIO
N F
AC
TO
R1
MP
H =
1.6
km
/h
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
60 (18)
40 (12) 20 (6)
G−
0022
6 (0
000)
102
MP
H68
MP
H51
MP
H34
MP
H13
6 M
PH
34 M
PH
51 M
PH
68 M
PH
102
MP
H13
6 M
PH
ALL
VE
LOC
ITY
VA
LUE
S A
RE
IN S
TA
TU
TE
MIL
ES
PE
R H
OU
R.
GR
OU
ND
IDLE
PO
WE
R, S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
DS
TA
ND
AR
D D
AY
, ZE
RO
RA
MP
GR
AD
IEN
T E
NG
INE
TY
PE
.
F_AC_060101_1_0010101_01_00
Engine Exhaust VelocitiesGround Idle Power - PW 4000 series engine
FIGURE-6-1-1-991-001-A01
6-1-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
ft
ft
m
m
00
00
0
0
FEET
METERS
50
ELEVATION
100 150
15 30 45
205
5 20
PLAN
200 fps 100 fps 50 fps
200 fps 100 fps 50 fps
10
15
20
40
60
10
15
20
25
60
40
80
(100 fps = 68 MPH = 109 kmph)
(100 fps = 68 MPH = 109 mph)
F_AC_060101_1_0020101_01_00
Engine Exhaust VelocitiesGround Idle Power - RR Trent 700 series engine
FIGURE-6-1-1-991-002-A01
6-1-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
0
0
ft
0
ft
25
25
50
50
ELEVATION
PLAN
m
15
0
10
5
m
15
0
10
5
0 50 100 150 200FEET
METERS15 30 45 60
V=51.3V=95.3
(100 fps = 68 MPH = 109 kmph)
(100 fps = 68 MPH= 109 kmph)
ft/s6535 MPH
10556 km/h
F_AC_060101_1_0030101_01_01
Engine Exhaust VelocitiesGround Idle Power - GE CF6-80E1 series engine
FIGURE-6-1-1-991-003-A01
6-1-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Temperatures Contours - Ground Idle Power
1. This section gives engine exhaust temperatures contours at ground idle power.
6-1-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
AIR
PLA
NE
C L
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
125°
F(5
2°C
)
0 60 (18) 40 (12) 20 (6)
060 (18) 40 (12) 20 (6)
150°
F(6
6°C
)
150°
F(6
6°C
)12
5°F
(52°
C)
100°
F(3
8°C
)
100°
F(3
8°C
)
G−
0022
9 (1
294)
TE
MP
ER
AT
UR
ES
AR
E IN
DE
GR
EE
S F
AH
RE
NH
EIT
(D
EG
RE
ES
C)
GR
OU
ND
IDLE
PO
WE
R −
SE
A L
EV
EL
ST
AT
IC, Z
ER
O W
IND
,S
TA
ND
AR
D D
AY
, ZE
RO
RA
MP
GR
AD
IEN
T E
NG
INE
TY
PE
.
PLA
N
F_AC_060102_1_0010101_01_00
Engine Exhaust TemperaturesGround Idle Power - PW 4000 series engine
FIGURE-6-1-2-991-001-A01
6-1-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
FEET
METERS
50 100 150
15 30 45
ELEVATION
PLAN
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
0
113°F(45°C)
95°F(35°C)
77°F(25°C)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
113°F(45°C)
95°F(35°C)
77°F(25°C)
F_AC_060102_1_0020101_01_00
Engine Exhaust TemperaturesGround Idle Power - RR Trent 700 series engine
FIGURE-6-1-2-991-002-A01
6-1-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
ELEVATION
PLAN
50 100 150FEET
METERS 15 30 45
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
141°F(60°C)
91°F(31°C)
116°F(47°C)
141°F(60°C)
116°F(47°C)
91°F(31°C)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
0
F_AC_060102_1_0030101_01_01
Engine Exhaust TemperaturesGround Idle Power - GE CF6-80E1 series engine
FIGURE-6-1-2-991-003-A01
6-1-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities Contours - Breakaway Power
1. This section gives engine exhaust velocities contours at breakaway power
6-1-3Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
60 (18) 40 (12) 20 (6) 0 60 (1
8) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
PLA
NA
IRP
LAN
EC L
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
CO
NV
ER
SIO
N F
AC
TO
R
136
MP
H10
2 M
PH
68 M
PH
51 M
PH
34 M
PH
G−
0324
7 (0
000)
ALL
VE
LOC
ITY
VA
LUE
S A
RE
IN S
TA
TU
TE
MIL
ES
PE
R H
OU
R.
GR
OU
ND
IDLE
PO
WE
R −
SE
A L
EV
EL
ST
AT
IC, Z
ER
O W
IND
ST
AN
DA
RD
DA
Y, Z
ER
O R
AM
P G
RA
DIE
NT
EN
GIN
E T
YP
E.
136
MP
H10
2 M
PH
68 M
PH
51 M
PH
34 M
PH
1 M
PH
= 1
.6 k
m/h
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
F_AC_060103_1_0010101_01_00
Engine Exhaust VelocitiesBreakaway Power - PW 4000 series engine
FIGURE-6-1-3-991-001-A01
6-1-3Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
ELEVATION
200 fps 100 fps 50 fps
(100 fps = 68 MPH = 109 kmph)
200 fps 100 fps 50 fps
(100 fps = 68 MPH = 109 kmph)ft
ft
m
m
00
00
0
0
FEET
METERS
50 100
15 30
205
5 20
PLAN
10
15
20
40
60
10
15
20
25
60
40
80
150 200 250 300
6045 75 90
F_AC_060103_1_0020101_01_00
Engine Exhaust VelocitiesBreakaway Power - RR Trent 700 series engine
FIGURE-6-1-3-991-002-A01
6-1-3Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
0
0
ft
2550
ELE
VA
TIO
N
PLA
N
m15 010 5
010
0F
EE
T
ME
TE
RS
30
02550m
15 010 5
200
60
300
400
500
600
9012
015
018
0
105
MP
H65
MP
H35
MP
H
210
MP
H14
5 M
PH
105
MP
H65
MP
H35
MP
H
210
MP
H14
5 M
PH
51.3
V=
V=
154
V=
213
V=
308
(100
fps
= 6
8 M
PH
= 1
09 m
ph)
(100
fps
= 6
8 M
PH
= 1
09 m
ph)
ft
ft/s
65 105
145
210
3510
516
923
333
8
56V
=95
.3M
PH
km/h
F_AC_060103_1_0030101_01_01
Engine Exhaust VelocitiesBreakaway Power - GE CF6-80E1 series engine
FIGURE-6-1-3-991-003-A01
6-1-3Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Temperatures Contours - Breakaway Power
1. This section gives engine exhaust temperatures contours at breakaway power.
6-1-4Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
60 (18) 40 (12) 20 (6) 0 60 (1
8) 40 (12) 20 (6)
0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
GR
OU
ND
PLA
NE
PLA
NA
IRP
LAN
EC L
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
100°
F(3
8°C
)12
5°F
(52°
C)
(66°
C)
125°
F(5
2°C
)15
0°F
(66°
C)
NO
TE
:T
EM
PE
RA
TU
RE
S A
RE
IN D
EG
RE
ES
FA
HR
EN
HE
IT (
DE
GR
EE
S C
)G
RO
UN
D ID
LE P
OW
ER
− S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
D,
ST
AN
DA
RD
DA
Y, Z
ER
O R
AM
P G
RA
DIE
NT
EN
GIN
E T
YP
E.
G−
0324
6 (0
000)
100°
F(3
8°C
)
150°
F
ELE
VA
TIO
N
F_AC_060104_1_0010101_01_00
Engine Exhaust TemperaturesBreakaway Power - PW 4000 series engine
FIGURE-6-1-4-991-001-A01
6-1-4Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
ELEVATION
0
FEET
METERS
50 100 150
15 30 45
PLAN
113°F(45°C)
95°F(35°C)
77°F(25°C)
113°F(45°C)
77°F(25°C)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
95°F(35°C)
F_AC_060104_1_0020101_01_00
Engine Exhaust TemperaturesBreakaway Power - RR Trent 700 series engine
FIGURE-6-1-4-991-002-A01
6-1-4Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
0
0
ft
0
ft
25
25
50
50
ELEVATION
PLAN
m
15
0
10
5
m
15
0
10
5
0 50 100 150 200FEET
METERS 15 30 45 60
341°F(172°C)
141°F(60°C)
241°F(116°C)
116°F(47°C)
91°F(31°C)
341°F(172°C)
141°F(60°C)
241°F(116°C)
116°F(47°C)
91°F(31°C)
F_AC_060104_1_0030101_01_01
Engine Exhaust TemperaturesBreakaway Power - GE CF6-80E1 series engine
FIGURE-6-1-4-991-003-A01
6-1-4Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power
6-1-5Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
0 60 (18) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
NA
IRP
LAN
EC L
CO
NV
ER
SIO
N F
AC
TO
R1
MP
H =
1.6
km
/h
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
ALL
VE
LOC
ITY
VA
LUE
S A
RE
IN S
TA
TU
TE
MIL
ES
PE
R H
OU
R.
TA
KE
OF
F P
OW
ER
− S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
DS
TA
ND
AR
D D
AY
, ZE
RO
RA
MP
GR
AD
IEN
T E
NG
INE
TY
PE
.
60 (18) 40 (12) 20 (6)
682
MP
H47
7 M
PH
341
MP
H20
4 M
PH
102
MP
H
477
MP
H34
1 M
PH
204
MP
H10
2 M
PH
34 M
PH
TO
740
ft22
5 m
682
MP
H34
MP
HT
O 7
40 ft
225
m
G−
0022
8 (1
294)
68 M
PH
460
ft14
0 m
68 M
PH
460
ft14
0 m
F_AC_060105_1_0010101_01_00
Engine Exhaust VelocitiesTakeoff Power - PW 4000 series engine
FIGURE-6-1-5-991-001-A01
6-1-5Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
50 fp
s
0
FE
ET
ME
TE
RS
ELE
VA
TIO
N
PLA
N
60
5
101520
250
200
150
100
0
7560
4530
150
m
40 20Ft
50 fp
s
(100
fps
= 6
8 M
PH
= 1
09 k
mph
)
TO
1175
ft35
8 m
TO
1175
ft35
8 m
05
1015
m
40 20Ft
2060
30 25
100
80
50
(100
fps
= 6
8 M
PH
= 1
09 k
mph
)
200
fps
100
fps
200
fps
100
fps
D29
81A
300
90
350
105
TO
470
ft14
3 m
TO
470
ft14
3 m
F_AC_060105_1_0020101_01_00
Engine Exhaust VelocitiesTakeoff Power - RR Trent 700 series engine
FIGURE-6-1-5-991-002-A01
6-1-5Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
0
0
ft
2550
ELE
VA
TIO
N
PLA
N
m15 010 5
010
0F
EE
T
ME
TE
RS
30
0
ft
2550m
15 010 5
200
60
300
400
500
600
9012
015
018
0
105
MP
H65
MP
H35
MP
H
105
MP
H65
MP
H35
MP
H
V=
V=
V=
154
V=
213
V=
308
(100
fps
= 6
8 M
PH
= 1
09 k
m/h
)
(100
fps
= 6
8 M
PH
= 1
09 k
m/h
)
65 105
145
210
105
169
233
338
35 M
PH
56 k
m/h
51.3
ft/s
95.3
F_AC_060105_1_0030101_01_00
Engine Exhaust VelocitiesTakeoff Power - GE CF6-80E1 series engine
FIGURE-6-1-5-991-003-A01
6-1-5Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power
6-1-6Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
0
60 (18) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
NA
IRP
LAN
EC L
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
60(1
8) 40(1
2) 20 (6)
G−
0023
1 (0
000)
TE
MP
ER
AT
UR
ES
AR
E IN
DE
GR
EE
S F
AH
RE
NH
EIT
(D
EG
RE
ES
C).
TA
KE
OF
F P
OW
ER
− S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
D,
ST
AN
DA
RD
DA
Y, Z
ER
O R
AM
P G
RA
DIE
NT
EN
GIN
E T
YP
E.
250°
F(1
21°
C)
150°
F(6
6°C
)12
5°F
(52°
C)
200°
F(9
3°C
)30
0°F
(149
°C
)10
0°F
(38°
C)
250°
F(1
21°
C)
150°
F(6
6°C
)12
5°F
(52°
C)
200°
F(9
3°C
)30
0°F
(149
°C
)10
0°F
(38°
C)
F_AC_060106_1_0010101_01_00
Engine Exhaust TemperaturesTakeoff Power - PW 4000 series engine
FIGURE-6-1-6-991-001-A01
6-1-6Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
ftft
mm
00
00
FE
ET
ME
TE
RS
50ELE
VA
TIO
N
100
150
200
250
300
350
1530
4560
7590
105
205
101520 25 20 15 105
80 60 40 20
TO
430
ft(1
31 m
)
TO
430
ft(1
31 m
)
PLA
N
4060
113°
F(4
5°C
)77
°F
(25°
C)
95°
F(3
5°C
)
0 0
113°
F(4
5°C
)77
°F
(25°
C)
95°
F(3
5°C
)
F_AC_060106_1_0020101_01_00
Engine Exhaust TemperaturesTakeoff Power - RR Trent 700 series engine
FIGURE-6-1-6-991-002-A01
6-1-6Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
0
ft
0
ft
252550 50
ELE
VA
TIO
N
PLA
N
m
15 0
10
5
m
15 0
10
5
5010
015
020
0F
EE
T
ME
TE
RS
1530
4560
250
300
7590
341°
F(1
72°
C)
241°
F(1
16°
C)
141°
F(6
0°C
)11
6°F
(47°
C)
91°
F(3
1°C
)
341°
F(1
72°
C)
241°
F(1
16°
C)
141°
F(6
0°C
)11
6°F
(47°
C)
91°
F(3
1°C
)
00
F_AC_060106_1_0030101_01_00
Engine Exhaust TemperaturesTakeoff Power - GE CF6-80E1 series engine
FIGURE-6-1-6-991-003-A01
6-1-6Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-0 Airport and Community Noise
**ON A/C A330-200 A330-200F A330-300
Airport and Community Noise Data
1. Airport and Community Noise Data
This section gives data concerning engine maintenance run-up noise to permit evaluation of possibleattenuation requirements.
6-2-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-1 Noise Data
**ON A/C A330-200 A330-200F A330-300
Noise Data
1. Noise Data for PW 4000 series engine
A. Description of test conditions :
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Engine parameters : 2 engines running
C. Meteorological data
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows :- Temperature : 24.8 ˚C (76.64 ˚F)- Relative humidity : 46%- Atmospheric pressure : 1000 hPa- Wind speed : Negligible- No rain
2. Noise Data for RR Trent 700 series engine
A. Description of test conditions :
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Engine parameters : 2 engines running
C. Meteorological data
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows :- Temperature : 16.8 ˚C (62.24 ˚F)- Relative humidity : 70%- Atmospheric pressure : 1009 hPa- Wind speed : Negligible- No rain
6-2-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
3. Noise Data for GE CF6-80E1 series engine
A. Description of test conditions :
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Engine parameters : 2 engines running
C. Meteorological data
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows :- Temperature : 24.5 ˚C (76.10 ˚F)- Relative humidity : 47%- Atmospheric pressure : 1003.1 hPa- Wind speed : Negligible- No rain
6-2-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
7880
8284
8688
9092
9496
0°10°20°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
270°
240°
230°
220°
210°
NOISE REFERENCEPOINT
GROUND IDLE
E.P.R.
N1
CURVE
25% 82.4%
MAX THRUST POSSIBLEON BRAKES
1.016 1.337
30°
40°
50°
320°
310°
300°
290°
280°
250°
260°
F_AC_060201_1_0010101_01_00
Airport and Community NoisePW 4000 series engine
FIGURE-6-2-1-991-001-A01
6-2-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
7880
8284
8688
9092
9496
0°10°20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
320°
310°
300°
290°
280°
270°
260°
250°
240°
230°
220°NOISE REFERENCE
POINT
GROUND IDLE
E.P.R.
N1
CURVE
23% 79.5%
MAX THRUST POSSIBLEON BRAKES
1.017 1.43
210°
F_AC_060201_1_0020101_01_00
Airport and Community NoiseRR Trent 700 series engineFIGURE-6-2-1-991-002-A01
6-2-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
7880
8284
8688
9092
9496
0°10°20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
320°
310°
300°
290°
280°
270°
260°
250°
240°
230°
220°
210°
NOISE REFERENCEPOINT
GROUND IDLE
N1
CURVE
26% 99.5%
MAX THRUST POSSIBLEON BRAKES
F_AC_060201_1_0030101_01_00
Airport and Community NoiseGE CF6-80E1 series engineFIGURE-6-2-1-991-003-A01
6-2-1Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A330-200 A330-200F A330-300
Danger Areas of Engines
1. Danger Areas of the Engines.
6-3-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1 Ground Idle Power
**ON A/C A330-200 A330-200F A330-300
Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions
6-3-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
INTAKE SUCTIONDANGER AREA
30°
EXHAUST DANGERAREA
SAFE ENTRYAREA
G−00224(0992)
TO 175 ft AT 34 MPHTO 53.35 m AT 54.4 kph
8.2 m(27 ft)
1.7 m(5.5 ft)
F_AC_060301_1_0010101_01_00
Danger Areas of EnginesPW 4000 series engine
FIGURE-6-3-1-991-001-A01
6-3-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
TO 256 ft (78 m) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA MINIMUM POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
30°
3.75 ft10 ft
D4816
(3 m)(1 m)
F_AC_060301_1_0020101_01_00
Danger Areas of EnginesRR Trent 700 series engineFIGURE-6-3-1-991-002-A01
6-3-1Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
INLET SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST WAKE DANGER. WIND 105 km/h/57 kts OR GREATER
TO
54.90 m/180 ft A
FT
FA
N N
OZ
ZLE
7.62 m(25 ft)
1.25
m(4
.1 ft
)
45°
30°
RAD
IUS
F_AC_060301_1_0030101_01_00
Danger Areas of EnginesGE CF6-80E1 series engineFIGURE-6-3-1-991-003-A01
6-3-1Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2 Breakaway Power
**ON A/C A330-200 A330-200F A330-300
Breakaway Power
1. This section gives danger areas of the engines at breakaway conditions.
6-3-2Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
INTAKE SUCTIONDANGER AREA
EXHAUST DANGERAREA
TO 290 ft AT 34 MPHTO 88.4 m m AT 54.4 kph
(37 ft)11.3 m
G−03248 (0000)
F_AC_060302_1_0010101_01_00
Danger Areas of EnginesPW 4000 series engine
FIGURE-6-3-2-991-001-A01
6-3-2Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
(8 ft)2.4 m
(25 ft)7.6 m
30°TO 150 m (490 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA BREAKAWAY POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
F_AC_060302_1_0020101_01_00
Danger Areas of EnginesRR Trent 700 series engineFIGURE-6-3-2-991-002-A01
6-3-2Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
INLET SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST WAKE DANGER. WIND 105 km/h/57 kts OR GREATER
TO
48.8 m/160 ft A
FT
FA
N N
OZ
ZLE
(50 ft)15.2 m
45°
(5 ft
)1.
5 m
30°
RAD
IUS
F_AC_060302_1_0030101_01_00
Danger Areas of EnginesGE CF6-80E1 series engineFIGURE-6-3-2-991-003-A01
6-3-2Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-3 Takeoff Power
**ON A/C A330-200 A330-200F A330-300
Takeoff Power
1. This section gives danger areas of the engines at max takeoff conditions
6-3-3Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
30°
INTAKE SUCTIONDANGER AREA
EXHAUST DANGERAREA
PW 4164 / PW 4168 −TAKEOFFG − 00225 (0493)
TO 740 ft AT 34 MPHTO 225.5 m AT 54.4 kph
2 m6.5 ft
54 ft16.5 m
F_AC_060303_1_0010101_01_00
Danger Areas of EnginesPW 4000 series engine
FIGURE-6-3-3-991-001-A01
6-3-3Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
30°
TO 2100 ft (640 m) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA TAKE−OFF POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
2.4 m(8 ft)
7.6 m(25 ft)
F_AC_060303_1_0020101_01_00
Danger Areas of EnginesRR Trent 700 series engineFIGURE-6-3-3-991-002-A01
6-3-3Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
INLET SUCTION DANGER AREA
ENTRY CORRIDOR
TO 274.30 m
/900 ft AFT FA
N N
OZZLE
EXHAUST WAKE DANGER. WIND 105 km/h / 57Kts OR GREATER
G_AC_060303_0_F00CAM0_00_00
(6 ft)1.80 m
15.25 m(50 ft)
45°
40°
RADIUS
F_AC_060303_1_0030101_01_00
Danger Areas of EnginesGE CF6-80E1 series engineFIGURE-6-3-3-991-003-A01
6-3-3Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A330-200 A330-200F A330-300
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1 APU
**ON A/C A330-200 A330-200F A330-300
APU - GARRETT
1. This section gives APU exhaust velocities and temperatures
6-4-1Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
20
METERS
0
5 10 15
FEET
0
10 20 30 40 50
0
60
0
10
5
10
20
30
40
METERS FEET
20
METERS
0
5 10 15
FEET
0
10 20 30 40 50
0
60
0
10
5
10
20
30
40
METERS FEET
121°C
93°C
149°C177°C
15 m/s
FD
315.5°C
204°C260°C
427°C
18 m/s24 m/s
30.5 m/s46 m/s
61 m/s
FD
F_AC_060401_1_0010101_01_00
Exhaust Velocities and TemperaturesAPU -- GARRETT GTCP 331-350
FIGURE-6-4-1-991-001-A01
6-4-1Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A330-200 A330-200F A330-300
General Information
1. General Information
A brief description of the pavement charts that follow will help in airport planning.
To aid in the interpolation between the discrete values shown, each aircraft configuration is shownwith a minimum range of five loads on the MLG.
All curves on the charts represent data at a constant specified tire pressure with :- The aircraft loaded to the Maximum Ramp Weight (MRW),- The CG at its maximum permissible aft position.
Pavement requirements for commercial aircraft are derived from the static analysis of loads imposedon the MLG struts.
Landing Gear FootprintSection 7-2-0 presents basic data on the landing gear footprint configuration, MRW and tire sizes andpressures.
Maximum Pavement LoadsSection 7-3-0 shows the maximum vertical and horizontal pavement loads for certain criticalconditions at the tire-ground interfaces.
Landing Gear Loading on PavementSection 7-4-0 contains charts to find these loads throughout the stability limits of the aircraft at reston the pavement.These MLG loads are used as the point of entry to the pavement design charts, which follow,interpolating load values where necessary.
Flexible Pavement Requirements - US Army Corps of Engineers Design MethodSection 7-5-0 uses procedures in Instruction Report No S-77-1 ”Procedures for Development of CBRDesign Curves”, dated June 1977 and as modified according to the methods described in ICAOAerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCNMethod), and utilizing the alpha factors approved by ICAO in October 2007.The report was prepared by the U.S. Army Corps Engineers Waterways Experiment Station, Soils andPavement Laboratory, Vicksburg, Mississippi”. The line showing 10 000 coverages is used to calculateAircraft Classification Number (ACN).
7-1-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Flexible Pavement Requirements - LCN Conversion MethodThe flexible pavement charts in Section 7-6-0 show Load Classification Number (LCN) againstequivalent single wheel load (ESWL), and ESWL against pavement thickness.All LCN curves shown in ’Flexible Pavement Requirements’ were developed from a computer programbased on data in International Civil Aviation Organization (ICAO) document 7920-AN/865/2,Aerodrome manual, Part 2, ”Aerodrome Physical Characteristics”, Second Edition, 1965.
Rigid Pavement Requirements - PCA (Portland Cement Association) Design MethodSection 7-7-0 gives the rigid pavement design curves that have been prepared with the use of theWestergaard Equation.This is in general accordance with the procedures outlined in the Portland Cement Associationpublications, ”Design of Concrete Airport Pavement”, 1973 and ”Computer Program for AirportPavement Design”, (Program PDILB), 1967 both by Robert G. Packard.
Rigid Pavement Requirements - LCN ConversionSection 7-8-0 gives data about the rigid pavement requirements for the LCN Conversion.- For the radius of relative stiffness,- For the radius of relative stiffness (other values of E and µ).All LCN curves shown in Rigid Pavement Requirements - LCN conversion - were developed from acomputer program based on data in International Civil Aviation Organization (ICAO) document 7920-AN/865/2, Aerodrome manual, Part 2, ”Aerodrome Physical Characteristics”, Second Edition, 1965.Rigid Pavement Requirements - LCN Conversion - Radius of Relative Stiffness.The rigid pavement charts show LCN against ESWL, and ESWL against radius of relative stiffness.Rigid Pavement Requirements - LCN Conversion - Radius of Relative Stiffness (other values of E andµ)The rigid pavement charts show LCN against ESWL and ESWL against radius of relative stiffnessaffected by the other values of E and µ.ACN/PCN Reporting SystemSection 7-9-0 provides ACN data prepared according to the ACN/PCN system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations.” Fourth Edition July 2004,incorporating Amendments 1 to 6.The ACN/PCN system provides a standardized international aircraft/pavement rating systemreplacing the various S, T, TT, LCN, AUW, ISWL, etc... rating systems used throughout the world.ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.An aircraft having an ACN equal to or less than the PCN can operate without restriction on thepavement.Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.The derived single wheel load is defined as the load on a single tire inflated to 1.25 Mpa (181 psi)that would have the same pavement requirements as the aircraft.Computationally the ACN/PCN the system uses PCA program PDILB for rigid pavements and S-77-1for flexible pavements to calculate ACN values.
7-1-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The Airport Authority must decide on the method of pavement analysis and the results of theirevaluation shown as follows :
PCNPAVEMENT
TYPESUBGRADECATEGORY
TIRE PRESSURE CATEGORY EVALUATION METHOD
R -- Rigid A -- High W -- No Limit T -- Technical
F -- Flexible B -- Medium X -- To 1.5 Mpa (217 psi) U -- Using Aircraft
C -- Low Y -- To 1.0 Mpa (145 psi)
D -- Ultra Low Z -- To 0.5 Mpa (73 psi)
Section 7-9-0 shows the aircraft ACN values.For flexible pavements, the four subgrade categories are :
- A. High Strength CBR 15
- B. Medium Strength CBR 10
- C. Low Strength CBR 6
- D. Ultra Low Strength CBR 3
For rigid pavements, the four subgrade categories are :
- A. High StrengthSubgrade k
= 150 MN/m3 (550 pci
- B. Medium StrengthSubgrade k
= 80 MN/m3 (300 pci)
- C. Low StrengthSubgrade k
= 40 MN/m3 (150 pci)
- D. Ultra Low StrengthSubgrade k
= 20 MN/m3 (75 pci)
7-1-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A330-200 A330-200F A330-300
Landing Gear Footprint
1. This section gives data about the landing gear footprint in relation with the aircraft MRW and tiresizes and pressures.The landing gear footprint information is given for all the aircraft operational weight variants.
7-2-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
1.39
7 m
1.98
1 m
0.71
0 m
(4.5
83 ft
)(6
.499
ft)
(2.3
29 ft
)
10.6
84 m
22.1
80 m
(35.
052
ft)
(72.
768
ft)
WE
IGH
TM
AX
IMU
MP
ER
CE
NT
AG
EN
OS
E G
EA
R T
IRE
NO
SE
GE
AR
MA
IN G
EA
R T
IRE
MA
IN G
EA
RR
AM
PW
EIG
HT
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
PS
IZE
TIR
EP
RE
SS
UR
ES
IZE
TIR
EP
RE
SS
UR
E
A33
0−20
0W
V02
023
0 90
0 kg
(509
050
lb)
94.7
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
1400
x530
R23
OR
54x2
1−23
(bi
as)
14.2
bar
(206
psi
)
A33
0−20
0W
V02
123
0 90
0 kg
(509
050
lb)
94.7
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
A33
0−20
0W
V02
223
3 90
0 kg
(515
650
lb)
94.6
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
A33
0−20
0W
V02
323
3 90
0 kg
(515
650
lb)
94.6
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
A33
0−20
0W
V02
420
2 90
0 kg
(447
325
lb)
94.9
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
VA
RIA
NT
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
F_AC_070200_1_0030101_01_04
Landing Gear Footprint(Sheet 1 of 2)
FIGURE-7-2-0-991-003-A01
7-2-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
WE
IGH
TM
AX
IMU
MP
ER
CE
NT
AG
EN
OS
E G
EA
R T
IRE
NO
SE
GE
AR
MA
IN G
EA
R T
IRE
MA
IN G
EA
RR
AM
PW
EIG
HT
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
PS
IZE
TIR
EP
RE
SS
UR
ES
IZE
TIR
EP
RE
SS
UR
EV
AR
IAN
T
A33
0−20
0W
V02
522
0 90
0 kg
(487
000
lb)
94.8
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
A33
0−20
0W
V02
619
2 90
0 kg
(425
275
lb)
95.0
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V02
722
0 90
0 kg
(487
000
lb)
94.8
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
023
0 90
0 kg
(509
050
lb)
94.7
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
119
2 90
0 kg
(425
275
lb)
95.0
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
223
3 90
0 kg
(515
650
lb)
94.6
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
321
0 90
0 kg
(464
950
lb)
94.8
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
423
0 90
0 kg
(509
050
lb)
94.7
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
519
2 90
0 kg
(425
275
lb)
95.0
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
623
3 90
0 kg
(515
650
lb)
94.6
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
723
6 90
0 kg
(522
275
lb)
93.4
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
823
8 90
0 kg
(526
675
lb)
92.7
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V05
920
2 90
0 kg
(447
325
lb)
94.9
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V06
022
0 90
0 kg
(487
000
lb)
94.8
%12
.7 b
ar(1
84 p
si)
A33
0−20
0W
V06
123
0 90
0 kg
(509
050
lb)
94.7
%12
.7 b
ar(1
84 p
si)
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
F_AC_070200_1_0030104_01_01
Landing Gear Footprint(Sheet 2 of 2)
FIGURE-7-2-0-991-003-A01
7-2-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
WE
IGH
TM
AX
IMU
MP
ER
CE
NT
AG
EN
OS
E G
EA
R T
IRE
NO
SE
GE
AR
MA
IN G
EA
R T
IRE
MA
IN G
EA
RR
AM
PW
EIG
HT
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
PS
IZE
TIR
EP
RE
SS
UR
ES
IZE
TIR
EP
RE
SS
UR
E
A33
0−20
0FW
V00
023
3 90
0 kg
(515
650
lb)
94.6
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
1400
x530
R23
OR
54x2
1−23
(bi
as)
14.2
bar
(206
psi
)
A33
0−20
0FW
V00
122
7 90
0 kg
(502
425
lb)
94.7
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
A33
0−20
0FW
V00
223
3 90
0 kg
(515
650
lb)
94.6
%10
50x3
95R
1612
.7 b
ar(1
84 p
si)
VA
RIA
NT
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
0.71
0 m
(2.3
29 ft
)
10.6
84 m
22.1
80 m
(35.
052
ft)
(72.
768
ft)
1.39
7 m
1.98
1 m
(4.5
83 ft
)(6
.499
ft)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
F_AC_070200_1_0170101_01_03
Landing Gear FootprintFIGURE-7-2-0-991-017-A01
7-2-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
0.71
0 m
(2.3
29 ft
)
10.6
84 m
25.3
75 m
(35.
052
ft)
(83.
251
ft)
1.39
7 m
1.98
1 m
(4.5
83 ft
)(6
.499
ft)
WE
IGH
TM
AX
IMU
MP
ER
CE
NT
AG
EN
OS
E G
EA
R T
IRE
NO
SE
GE
AR
MA
IN G
EA
R T
IRE
MA
IN G
EA
RR
AM
PW
EIG
HT
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
PS
IZE
TIR
EP
RE
SS
UR
ES
IZE
TIR
EP
RE
SS
UR
E
A33
0−30
0W
V00
021
2 90
0 kg
(469
375
lb)
94.9
%10
50x3
95R
1610
.7 b
ar(1
55 p
si)
1400
x530
R23
OR
54x2
1−23
(bi
as)
13.1
bar
(190
psi
)
A33
0−30
0W
V00
118
4 90
0 kg
(407
625
lb)
95.9
%10
50x3
95R
1610
.7 b
ar(1
55 p
si)
1050
x395
R16
10.7
bar
(155
psi
)
1050
x395
R16
1050
x395
R16
VA
RIA
NT
13.1
bar
(190
psi
)
13.1
bar
(190
psi
)
13.3
bar
(193
psi
)
13.3
bar
(193
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
94.9
%
94.4
%
95.7
%
A33
0−30
0W
V00
221
2 90
0 kg
(469
375
lb)
A33
0−30
0W
V00
321
5 90
0 kg
(475
975
lb)
A33
0−30
0W
V00
420
9 90
0 kg
(462
750
lb)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
F_AC_070200_1_0060101_01_04
Landing Gear Footprint(Sheet 1 of 2)
FIGURE-7-2-0-991-006-A01
7-2-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
WE
IGH
TM
AX
IMU
MP
ER
CE
NT
AG
EN
OS
E G
EA
R T
IRE
NO
SE
GE
AR
MA
IN G
EA
R T
IRE
MA
IN G
EA
RR
AM
PW
EIG
HT
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
PS
IZE
TIR
EP
RE
SS
UR
ES
IZE
TIR
EP
RE
SS
UR
E
1050
x395
R16
VA
RIA
NT
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
13.3
bar
(193
psi
)
13.3
bar
(193
psi
)
14.2
bar
(206
psi
)
14.5
bar
(210
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.5
bar
(210
psi
)
14.5
bar
(210
psi
)
14.5
bar
(210
psi
)
14.5
bar
(210
psi
)
13.3
bar
(193
psi
)
13.3
bar
(193
psi
)
13.3
bar
(193
psi
)
13.3
bar
(193
psi
)
13.3
bar
(193
psi
)
1050
x395
R16
14.5
bar
(210
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
11.4
bar
(165
psi
)
11.6
bar
(168
psi
)
11.4
bar
(165
psi
)
11.4
bar
(165
psi
)
11.6
bar
(168
psi
)
11.6
bar
(168
psi
)
11.6
bar
(168
psi
)
11.6
bar
(168
psi
)
11.6
bar
(168
psi
)
95.6
%
94.0
%
95.6
%
95.7
%
95.6
%
95.6
%
95.7
%
95.5
%
95.5
%
95.7
%
95.6
%
95.5
%
95.7
%
95.5
%
95.7
%
94.7
%
A33
0−30
0W
V00
421
5 90
0 kg
(475
975
lb)
A33
0−30
0W
V01
021
7 90
0 kg
(480
375
lb)
A33
0−30
0W
V01
021
7 90
0 kg
(480
375
lb)
A33
0−30
0W
V01
121
2 90
0 kg
(469
375
lb)
A33
0−30
0W
V01
221
8 90
0 kg
(482
600
lb)
A33
0−30
0W
V01
321
5 90
0 kg
(475
975
lb)
A33
0−30
0W
V01
420
5 90
0 kg
(453
925
lb)
A33
0−30
0W
V02
023
0 90
0 kg
(509
050
lb)
A33
0−30
0W
V02
223
3 90
0 kg
(515
650
lb)
A33
0−30
0W
V02
420
5 90
0 kg
(453
925
lb)
A33
0−30
0W
V02
521
7 90
0 kg
(480
375
lb)
A33
0−30
0W
V05
023
0 90
0 kg
(509
050
lb)
A33
0−30
0W
V05
121
2 90
0 kg
(469
375
lb)
A33
0−30
0W
V05
223
3 90
0 kg
(515
650
lb)
A33
0−30
0W
V05
320
5 90
0 kg
(453
925
lb)
A33
0−30
0W
V05
423
5 90
0 kg
(520
075
lb)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
F_AC_070200_1_0060102_01_00
Landing Gear Footprint(Sheet 2 of 2)
FIGURE-7-2-0-991-006-A01
7-2-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A330-200 A330-200F A330-300
Maximum Pavement Loads
1. This section shows maximum vertical and horizontal pavement loads for some critical conditions atthe tire-ground interfaces.The maximum pavement loads are given for all the aircraft operational weight variants.
7-3-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
12
34
56
VN
GV
MG
(P
ER
ST
RU
T)
H (
PE
R S
TR
UT
)
A33
0−20
0W
V02
0
MO
DE
LM
AX
IMU
MR
AM
PM
OS
T F
WD
C.G
.@
10
ft/s
DE
CE
LER
AT
ION
MA
X A
FT
C.G
.@
10
ft/s
DE
CE
LER
AT
ION
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
WE
IGH
T
230
900
kg(5
09 0
50 lb
)
ST
AT
IC L
OA
D A
TS
TA
TIC
BR
AK
ING
ST
AT
IC L
OA
D A
TS
TE
AD
Y B
RA
KIN
GA
T IN
ST
AN
TA
NE
OU
S
25 1
70 k
g(5
5 50
0 lb
)39
570
kg
(87
225
lb)
109
290
kg(2
40 9
50 lb
)35
880
kg
(79
100
lb)
87 4
30 k
g(1
92 7
50 lb
)
A33
0−20
0W
V02
123
0 90
0 kg
(509
050
lb)
25 1
70 k
g(5
5 50
0 lb
)39
570
kg
(87
225
lb)
109
290
kg(2
40 9
50 lb
)35
880
kg
(79
100
lb)
87 4
30 k
g(1
92 7
50 lb
)
A33
0−20
0W
V02
223
3 90
0 kg
(515
650
lb)
25 1
70 k
g(5
5 50
0 lb
)39
750
kg
(87
625
lb)
110
670
kg(2
43 9
75 lb
)36
350
kg
(80
150
lb)
88 5
40 k
g(1
95 2
00 lb
)
A33
0−20
0W
V02
323
3 90
0 kg
(515
650
lb)
25 1
70 k
g(5
5 50
0 lb
)39
750
kg
(87
625
lb)
110
670
kg(2
43 9
75 lb
)36
350
kg
(80
150
lb)
88 5
40 k
g(1
95 2
00 lb
)
21%
MA
C37
.5%
MA
C
21%
MA
C
21.4
%M
AC
21.4
%M
AC
37.5
%M
AC
37.4
%M
AC
37.4
%M
AC
A33
0−20
0W
V02
420
2 90
0 kg
(447
325
lb)
24 2
20 k
g(5
3 40
0 lb
)36
990
kg
(81
550
lb)
96 3
00 k
g(2
12 3
00 lb
)31
530
kg
(69
500
lb)
77 0
40 k
g(1
69 8
50 lb
)
18%
MA
C38
.4%
MA
C
A33
0−20
0W
V02
522
0 90
0 kg
(487
000
lb)
25 1
60 k
g(5
5 47
5 lb
)38
980
kg
(85
925
lb)
104
650
kg(2
30 7
25 lb
)34
330
kg
(75
675
lb)
83 7
20 k
g(1
84 5
75 lb
)
19.5
7%M
AC
37.8
%M
AC
A33
0−20
0W
V02
619
2 90
0 kg
(425
275
lb)
23 0
50 k
g(5
0 82
5 lb
)35
240
kg
(77
700
lb)
91 6
70 k
g(2
02 1
00 lb
)29
980
kg
(66
100
lb)
73 3
30 k
g(1
61 6
75 lb
)
18%
MA
C38
.8%
MA
C
A33
0−20
0W
V02
722
0 90
0 kg
(487
000
lb)
25 1
60 k
g(5
5 47
5 lb
)38
980
kg
(85
925
lb)
104
650
kg(2
30 7
25 lb
)34
330
kg
(75
675
lb)
83 7
20 k
g(1
84 5
75 lb
)
19.5
7%M
AC
37.8
%M
AC
V(M
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(N
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
GH
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
V(N
G)
V(M
G)
H
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
NO
TE
:
(a)
LOA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
F_AC_070300_1_0010101_01_03
Maximum Pavement Loads(Sheet 1 of 2)
FIGURE-7-3-0-991-001-A01
7-3-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
A33
0−20
0W
V05
119
2 90
0kg
(425
275
lb)
23 0
50 k
g(5
0 82
5 lb
)35
240
kg
(77
700
lb)
91 6
70 k
g(2
02 1
00 lb
)29
980
kg
(66
100
lb)
73 3
30 k
g(1
61 6
75 lb
)
A33
0−20
0W
V05
223
3 90
0 kg
(515
650
lb)
25 1
70 k
g(5
5 50
0 lb
)39
750
kg
(87
625
lb)
110
670
kg(2
43 9
75 lb
)36
350
kg
(80
150
lb)
88 5
40 k
g(1
95 2
00 lb
)
A33
0−20
0W
V05
321
0 90
0 kg
(464
950
lb)
25 1
50 k
g(5
5 45
0 lb
)38
390
kg
(84
625
lb)
100
010
kg(2
20 4
75 lb
)32
770
kg
(72
250
lb)
80 0
10 k
g(1
76 4
00 lb
)
A33
0−20
0W
V05
423
0 90
0 kg
(509
050
lb)
25 1
70 k
g(5
5 50
0 lb
)39
570
kg
(87
225
lb)
109
290
kg(2
40 9
50 lb
)35
880
kg
(79
100
lb)
87 4
30 k
g(1
92 7
50 lb
)
18%
MA
C38
.8%
MA
C
21.4
%M
AC
18%
MA
C
21%
MA
C
37.4
%M
AC
38.1
%M
AC
37.5
%M
AC
A33
0−20
0W
V05
519
2 90
0 kg
(425
275
lb)
23 0
50 k
g(5
0 82
5 lb
)35
240
kg
(77
700
lb)
91 6
70 k
g(2
02 1
00 lb
)29
980
kg
(66
100
lb)
73 3
30 k
g(1
61 6
75 lb
)
18%
MA
C38
.8%
MA
C
A33
0−20
0W
V05
623
3 90
0 kg
(515
650
lb)
25 1
70 k
g(5
5 50
0 lb
)39
750
kg
(87
625
lb)
110
670
kg(2
43 9
75 lb
)36
350
kg
(80
150
lb)
88 5
40 k
g(1
95 2
00 lb
)
21.4
%M
AC
37.4
%M
AC
A33
0−20
0W
V05
723
6 90
0 kg
(522
275
lb)
25 1
70 k
g(5
5 50
0 lb
)39
910
kg
(87
975
lb)
110
670
kg(2
43 9
75 lb
)36
820
kg
(81
175
lb)
88 5
40 k
g(1
95 2
00 lb
)
21.8
%M
AC
33.7
%M
AC
A33
0−20
0W
V05
823
8 90
0 kg
(526
675
lb)
25 1
70 k
g(5
5 50
0 lb
)40
020
kg
(88
225
lb)
110
670
kg(2
43 9
75 lb
)37
130
kg
(81
850
lb)
88 5
40 k
g(1
95 2
00 lb
)
22.0
6%M
AC
31.3
%M
AC
A33
0−20
0W
V05
920
2 90
0 kg
(447
325
lb)
24 2
20 k
g(5
3 40
0 lb
)36
990
kg
(81
550
lb)
96 3
00 k
g(2
12 3
00 lb
)31
530
kg
(69
500
lb)
77 0
40 k
g(1
69 8
50 lb
)
18%
MA
C38
.4%
MA
C
A33
0−20
0W
V06
022
0 90
0 kg
(487
000
lb)
25 1
40 k
g(5
5 42
5 lb
)38
960
kg
(85
900
lb)
104
650
kg(2
30 7
25 lb
)34
330
kg
(75
675
lb)
83 7
20 k
g(1
84 5
75 lb
)
19.6
%M
AC
37.8
%M
AC
A33
0−20
0W
V06
123
0 90
0 kg
(509
050
lb)
25 1
70 k
g(5
5 50
0 lb
)39
570
kg
(87
225
lb)
109
290
kg(2
40 9
50 lb
)35
880
kg
(79
100
lb)
87 4
30 k
g(1
92 7
50 lb
)
21%
MA
C37
.5%
MA
C
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
12
34
56
VN
GV
MG
(P
ER
ST
RU
T)
H (
PE
R S
TR
UT
)
MO
DE
LM
AX
IMU
MR
AM
PS
TA
TIC
LO
AD
AT
MO
ST
FW
D C
.G.
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
TM
AX
AF
T C
.G.
ST
EA
DY
BR
AK
ING
@ 1
0 ft/
sD
EC
ELE
RA
TIO
N
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
WE
IGH
T
NO
TE
:
(a)
LOA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
A33
0−20
0W
V05
023
0 90
0 kg
(509
050
lb)
25 1
70 k
g(5
5 50
0 lb
)39
570
kg
(87
225
lb)
109
290
kg(2
40 9
50 lb
)35
880
kg
(79
100
lb)
87 4
30 k
g(1
92 7
50 lb
)M
AC
37.5
%M
AC
(a)
(a)
21%
F_AC_070300_1_0010107_01_01
Maximum Pavement Loads(Sheet 2 of 2)
FIGURE-7-3-0-991-001-A01
7-3-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
12
34
56
VN
GV
MG
(P
ER
ST
RU
T)
H (
PE
R S
TR
UT
)
A33
0−20
0FW
V00
0
MO
DE
LM
AX
IMU
MR
AM
P
233
900
kg(5
15 6
50 lb
)
ST
AT
IC L
OA
D A
TM
OS
T F
WD
C.G
.
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
TM
AX
AF
T C
.G.
ST
EA
DY
BR
AK
ING
@ 1
0 ft/
sD
EC
ELE
RA
TIO
N
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
WE
IGH
T
25 1
70 k
g(5
5 50
0 lb
)39
750
kg
(87
625
lb)
110
670
kg(2
43 9
75 lb
)36
350
kg
(80
150
lb)
88 5
40 k
g(1
95 2
00 lb
)
21.4
%M
AC
37.4
%M
AC
V(M
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(N
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
GH
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
V(N
G)
V(M
G)
H
A33
0−20
0FW
V00
122
7 90
0 kg
(502
425
lb)
25 1
50 k
g(5
5 45
0 lb
)39
380
kg
(86
825l
b)10
7 90
0 kg
(237
875
lb)
35 4
20 k
g(7
8 10
0 lb
)86
320
kg
(190
300
lb)
20.6
%M
AC
37.6
%M
AC
A33
0−20
0FW
V00
223
3 90
0 kg
(515
650
lb)
25 1
70 k
g(5
5 50
0 lb
)39
750
kg
(87
625
lb)
110
670
kg(2
43 9
75 lb
)36
350
kg
(80
150
lb)
88 5
40 k
g(1
95 2
00 lb
)
21.4
%M
AC
37.4
%M
AC
NO
TE
:
(a)
LOA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
(a)
(a)
(a)
(a)
(a)
(a)
F_AC_070300_1_0060101_01_03
Maximum Pavement LoadsFIGURE-7-3-0-991-006-A01
7-3-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
12
34
56
VN
GV
MG
(P
ER
ST
RU
T)
H (
PE
R S
TR
UT
)
A33
0−30
0W
V00
0
MO
DE
LM
AX
IMU
MR
AM
P
212
900
kg(4
69 3
75 lb
)
ST
AT
IC L
OA
D A
TM
OS
T F
WD
C.G
.
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
TM
AX
AF
T C
.G.
ST
EA
DY
BR
AK
ING
@ 1
0 ft/
sD
EC
ELE
RA
TIO
N
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
WE
IGH
T
24 3
40 k
g(5
3 65
0 lb
)35
930
kg
(79
200
lb)
100
970
kg(2
22 6
00 lb
)33
090
kg
(72
950
lb)
80 7
80 k
g(1
78 1
00 lb
)
15%
MA
C36
.5%
MA
C
15%
MA
C
15%
MA
C
15%
MA
C
A33
0−30
0
A33
0−30
0
A33
0−30
0
WV
001
WV
002
WV
003
184
900
kg(4
07 6
25 lb
)21
200
kg
(46
750
lb)
31 3
70 k
g(6
9 15
0 lb
)88
620
kg
(195
375
lb)
28 7
30 k
g(6
3 35
0 lb
)70
900
kg
(156
300
lb)
212
900
kg(4
69 3
75 lb
)24
340
kg
(53
650
lb)
35 9
30 k
g(7
9 20
0 lb
)10
0 97
0 kg
(222
600
lb)
33 0
90 k
g(7
2 95
0 lb
)80
780
kg
(178
100
lb)
215
900
kg(4
75 9
75 lb
)24
670
kg
(54
400
lb)
36 4
10 k
g(8
0 27
5 lb
)10
1 86
0 kg
(224
575
lb)
33 5
50 k
g(7
3 97
5 lb
)81
490
kg
(179
650
lb)
40.1
%M
AC
36.5
%M
AC
34.8
%M
AC
15%
MA
C
15%
MA
C
15%
MA
C
15%
MA
C
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
WV
004
WV
004
WV
010
WV
010
209
900
kg(4
62 7
50 lb
)35
440
kg
(78
125
lb)
100
430
kg(2
21 4
00 lb
)32
620
kg
(71
925
lb)
80 3
40 k
g(1
77 1
25 lb
)M
AC
24 0
00 k
g(5
2 90
0 lb
)
215
900
kg(4
75 9
75 lb
)36
410
kg
(80
275
lb)
103
250
kg(2
27 6
25 lb
)33
550
kg
(73
975
lb)
82 6
00 k
g(1
82 1
00 lb
)M
AC
24 6
70 k
g(5
4 40
0 lb
)
217
900
kg(4
80 3
75 lb
)36
740
kg
(81
000
lb)
102
390
kg(2
25 7
25 lb
)33
860
kg
(74
650
lb)
81 9
10 k
g(1
80 5
75 lb
)M
AC
24 9
00 k
g(5
4 90
0 lb
)
217
900
kg(4
80 3
75 lb
)36
740
kg
(81
000
lb)
104
180
kg(2
29 6
75 lb
)33
860
kg
(74
650
lb)
83 3
50 k
g(1
83 7
50 lb
)M
AC
24 9
00 k
g(5
4 90
0 lb
)
39.4
%
39.2
%
33.5
%
39.1
3%
V(M
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(N
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
GH
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
V(N
G)
V(M
G)
H
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
NO
TE
:
(a)
LOA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
F_AC_070300_1_0030101_01_03
Maximum Pavement Loads(Sheet 1 of 2)
FIGURE-7-3-0-991-003-A01
7-3-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
12
34
56
VN
GV
MG
(P
ER
ST
RU
T)
H (
PE
R S
TR
UT
)
MO
DE
LM
AX
IMU
MR
AM
PS
TA
TIC
LO
AD
AT
MO
ST
FW
D C
.G.
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
TM
AX
AF
T C
.G.
ST
EA
DY
BR
AK
ING
@ 1
0 ft/
sD
EC
ELE
RA
TIO
N
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
WE
IGH
T
15%
MA
C
15%
MA
C
15%
MA
C
18%
MA
C
18.4
%M
AC
15%
MA
C
16.1
1%M
AC
18%
MA
C
15.3
3%M
AC
18.4
%M
AC
15%
MA
C
18.7
%M
AC
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
A33
0−30
0
WV
012
WV
013
WV
014
WV
020
WV
022
WV
024
WV
025
WV
050
WV
052
WV
051
WV
053
WV
054
38.6
%
39.6
%
39.1
2%
38.7
%
39.2
9%
218
900
kg(4
82 6
00 lb
)36
900
kg
(81
350
lb)
104
650
kg(2
30 7
25 lb
)34
020
kg
(75
000
lb)
83 7
20 k
g(1
84 5
75 lb
)M
AC
25 0
10 k
g(5
5 15
0 lb
)
215
900
kg(4
75 9
75 lb
)36
410
kg
(80
275
lb)
103
250
kg(2
27 6
25 lb
)33
550
kg
(73
975
lb)
82 6
00 k
g(1
82 1
00 lb
)M
AC
24 6
70 k
g(5
4 40
0 lb
)
205
900
kg(4
53 9
25 lb
)34
790
kg
(76
700
lb)
98 5
70 k
g(2
17 3
00 lb
)32
000
kg
(70
550
lb)
78 8
60 k
g(1
73 8
50 lb
)M
AC
23 5
50 k
g(5
1 92
5 lb
)
230
900
kg(5
09 0
50 lb
)36
940
kg
(81
450
lb)
110
270
kg(2
43 1
00 lb
)35
880
kg
(79
100
lb)
88 2
20 k
g(1
94 5
00 lb
)M
AC
24 3
40 k
g(5
3 65
0 lb
)
233
900
kg(5
15 6
50 lb
)37
130
kg
(81
850
lb)
111
670
kg(2
46 2
00 lb
)36
350
kg
(80
150
lb)
89 3
40 k
g(1
96 9
50 lb
)M
AC
24 3
80 k
g(5
3 75
0 lb
)
205
900
kg(4
53 9
25 lb
)34
790
kg
(76
700
lb)
98 5
70 k
g(2
17 3
00 lb
)32
000
kg
(70
550
lb)
78 8
60 k
g(1
73 8
50 lb
)M
AC
23 5
50 k
g(5
1 92
5 lb
)
217
900
kg(4
80 3
75 lb
)36
030
kg
(79
425
lb)
104
180
kg(2
29 6
75 lb
)33
860
kg
(74
650
lb)
83 3
40 k
g(1
83 7
25 lb
)M
AC
24 1
90 k
g(5
3 32
5 lb
)
212
900
kg(4
69 3
75 lb
)35
720
kg
(78
750l
b)10
1 83
0 kg
(224
500
lb)
33 0
90 k
g(7
2 95
0 lb
)81
470
kg
(179
600
lb)
MA
C
24 1
30 k
g(5
3 20
0 lb
)M
AC
233
900
kg(5
15 6
50 lb
)37
030
kg
(81
625
lb)
111
670
kg(2
46 2
00 lb
)36
350
kg
(80
150
lb)
89 3
40 k
g(1
96 9
50 lb
)M
AC
24 3
80 k
g(5
3 75
0 lb
)
205
900
kg(4
53 9
25 lb
)34
790
kg
(76
700
lb)
98 5
70 k
g(2
17 3
00 lb
)32
000
kg
(70
550
lb)
78 8
60 k
g(1
73 8
50 lb
)M
AC
23 5
50 k
g(5
1 92
5 lb
)
235
900
kg(5
20 0
75 lb
)37
130
kg
(81
850
lb)
111
670
kg(2
46 2
00 lb
)36
660
kg
(80
825
lb)
89 3
40 k
g(1
96 9
50 lb
)M
AC
24 3
80 k
g(5
3 75
0 lb
)
38.6
%
39.6
%
35.7
%
39.1
%
39.2
%
39.6
%
38.7
%
230
900
kg(5
09 0
50 lb
)36
840
kg
(81
225
lb)
110
270
kg(2
43 1
00 lb
)35
880
kg
(79
100
lb)
88 2
20 k
g(1
94 5
00 lb
)24
340
kg
(53
650
lb)
(a)
NO
TE
:
(a)
LOA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
A33
0−30
0
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
(a)
15%
MA
CA
330−
300
WV
011
212
900
kg(4
69 3
75 lb
)35
930
kg
(79
200
lb)
101
840
kg(2
24 5
25 lb
)33
090
kg
(72
950
lb)
81 4
70 k
g(1
79 6
00 lb
)M
AC
24 3
40 k
g(5
3 65
0 lb
)
39.3
%
(a)
(a)
F_AC_070300_1_0030102_01_01
Maximum Pavement Loads(Sheet 2 of 2)
FIGURE-7-3-0-991-003-A01
7-3-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A330-200 A330-200F A330-300
Landing Gear Loading on Pavement
1. This section gives data about the landing gear loading on pavement.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand max aft CG) the lowest MLG load and the highest MLG load of each A/C type.
Example, see FIGURE 7---0-99--001-A, calculation of the total weight on the MLG for:- An aircraft with a MRW of 192 900 kg (425 275 lb),- The aircraft gross weight is 160 000 kg (352 740 lb),- A percentage of weight on MLG of 95,0% (percentage of weight on MLG at MRW and CG max
aft).The total weight on the MLG group is 152 060 kg (335 250 lb).
7-4-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE OF WEIGHT ON MAIN GEAR
(x 1
000
kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
CG FOR ACNCALCULATION
38.8% MAC
TAKE OFF
MTOW − 192 000 Kg
MLW
LANDING
18% MAC
MZFW
500
450
400
350
300
250
(x 1
000
lb)
11010098969492908886
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
F_AC_070400_1_0010101_01_01
Landing Gear Loading on PavementWV026, MRW 192 900 kg (Sheet 1 of 2)
FIGURE-7-4-0-991-001-A01
7-4-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE OF WEIGHT ON MAIN GEAR
(x 1
000
kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
500
450
400
350
300
250
(x 1
000
lb)
11010098969492908886
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CG FOR ACNCALCULATION
31.3% MACMTOW − 238 000 Kg
22.06% MAC
MLW
MZFW
TAKE OFF
LANDING
F_AC_070400_1_0020101_01_01F_AC_070400_1_0010103_01_00
Landing Gear Loading on PavementWV058, MRW 238 900 kg (Sheet 2 of 2)
FIGURE-7-4-0-991-001-A01
7-4-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE OF WEIGHT ON MAIN GEAR
(x 1
000
kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
500
450
400
350
300
250
(x 1
000
lb)
11010098969492908886
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CG FOR ACNCALCULATION
37.6% MACMTOW − 227 000 kg
20.6% MAC
MLW
MZFW
TAKE OFF
LANDING
F_AC_070400_1_0030101_01_01
Landing Gear Loading on PavementWV001, MRW 227 900 kg (Sheet 1 of 2)
FIGURE-7-4-0-991-003-A01
7-4-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE OF WEIGHT ON MAIN GEAR
(x 1
000
kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
500
450
400
350
300
250
(x 1
000
lb)
11010098969492908886
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
MTOW − 233 000 kg
21.4% MAC
MLW
MZFW
TAKE OFF
CG FOR ACNCALCULATION
37.4% MAC
LANDING
F_AC_070400_1_0030201_01_01F_AC_070400_1_0030102_01_00
Landing Gear Loading on PavementWV000, MRW 233 900 kg (Sheet 2 of 2)
FIGURE-7-4-0-991-003-A01
7-4-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE OF WEIGHT ON MAIN GEAR
(x 1
000
kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
500
450
400
350
300
250
(x 1
000
lb)
11010098969492908886
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
15% MAC
MLW
MZFW
TAKE OFF
CG FOR ACNCALCULATION
40.1% MAC
MTOW − 184 000 kg
LANDING
F_AC_070400_1_0040101_01_01
Landing Gear Loading on PavementWV001, MRW 184 900 kg (Sheet 1 of 2)
FIGURE-7-4-0-991-004-A01
7-4-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE OF WEIGHT ON MAIN GEAR
(x 1
000
kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
500
450
400
350
300
250
(x 1
000
lb)
11010098969492908886
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
18.7% MAC
TAKE OFF
CG FOR ACNCALCULATION
35.7% MACMTOW − 235 000 kg
MLW
MZFW
LANDING
F_AC_070400_1_0040201_01_01F_AC_070400_1_0040102_01_00
Landing Gear Loading on PavementWV054, MRW 235 900 kg (Sheet 2 of 2)
FIGURE-7-4-0-991-004-A01
7-4-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A330-200 A330-200F A330-300
Flexible Pavement Requirements - US Army Corps of Engineers Design Method S-77-1
1. This section gives data about the flexible pavement requirements.The flexible pavement requirements graphs are given at standard tire pressure for the weight variantsthat produce (at the MRW and max aft CG) the lowest main MLG and the highest MLG load ofeach A/C type.They are calculated with the US Army Corps of Engineers Design Method.To find a flexible pavement thickness, you must know the Subgrade Strength (CBR), the annualdeparture level and the weight on one MLG.The line that shows 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).The procedure that follows is used to develop flexible pavement design curves:- With the scale for pavement thickness at the bottom and the scale for CBR at the top, a random
line is made to show 10 000 coverages,- A plot is then made of the incremental values of the weight on the MLG,- Annual departure lines are made based on the load lines of the weight on the MLG that is shown
on the graph.
Example, see FIGURE 7---0-99--002-A, calculation of the thickness of the flexible pavement for:- An aircraft with a MRW of 192 900 kg (425 275 lb),- A ”CBR” value of 10,- An annual departure level of 3 000,- The load on one MLG of 80 000 kg (176 375 lb).The required flexible pavement thickness is 48.7 cm (19 in).
NOTE : The CG in the figure title is the CG used for ACN / LCN calculation
7-5-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 60 80
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
(cm)
(in)
MAXIMUM POSSIBLE MAINGEAR LOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
10 000 COVERAGESUSED FOR ACNCALCULATIONS
6
3 10 15 20 30 40 60 806
10 15 20 30 40 60 80 100 120 150180
50 000 kg (110 225 lb)60 000 kg (132 275 lb)70 000 kg (154 325 lb)80 000 kg (176 375 lb)91 670 kg (202 100 lb)WEIGHT ON ONE MAIN LANDING GEAR
ALPHA FACTOR = 0.8*20 YEAR PAVEMENT LIFE25.00015.0006.0003.0001.200ANNUAL DEPARTURES*
F_AC_070500_1_0020101_01_00
Flexible Pavement RequirementsWV026, MRW 192 900 kg, CG 38.8 % (Sheet 1 of 2)
FIGURE-7-5-0-991-002-A01
7-5-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 60 80
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
(cm)
(in)
6
3 10 15 20 30 40 60 806
10 15 20 30 40 60 80 100 120 150180
70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)100 000 kg (220 450 lb)110 670 kg (243 975 lb)WEIGHT ON ONE MAIN LANDING GEAR
10 000 COVERAGESUSED FOR ACNCALCULATIONS
MAXIMUM POSSIBLE MAINGEAR LOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
ALPHA FACTOR = 0.8*20 YEAR PAVEMENT LIFE25.00015.0006.0003.0001.200ANNUAL DEPARTURES*
F_AC_070500_1_0020201_01_00F_AC_070500_1_0020102_01_00
Flexible Pavement RequirementsWV058, MRW 238 900 kg, CG 31.3 % (Sheet 2 of 2)
FIGURE-7-5-0-991-002-A01
7-5-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 60 80
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
(cm)
(in)
6
3 10 15 20 30 40 60 806
10 15 20 30 40 60 80 100 120 150180
MAXIMUM POSSIBLE MAINGEAR LOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
10 000 COVERAGESUSED FOR ACNCALCULATIONS
ALPHA FACTOR = 0.8*20 YEAR PAVEMENT LIFE25.00015.0006.0003.0001.200ANNUAL DEPARTURES*
60 000 kg (132 275 lb)70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)107 900 kg (237 875 lb)WEIGHT ON ONE MAIN LANDING GEAR
F_AC_070500_1_0030101_01_00
Flexible Pavement RequirementsWV001, MRW 227 900 kg, CG 37.6 % (Sheet 1 of 2)
FIGURE-7-5-0-991-003-A01
7-5-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 60 80
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
(cm)
(in)
6
3 10 15 20 30 40 60 806
10 15 20 30 40 60 80 100 120 150180
70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)100 000 kg (220 450 lb)110 670 kg (243 975 lb)WEIGHT ON ONE MAIN LANDING GEAR
10 000 COVERAGESUSED FOR ACNCALCULATIONS
MAXIMUM POSSIBLE MAINGEAR LOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
ALPHA FACTOR = 0.8*20 YEAR PAVEMENT LIFE25.00015.0006.0003.0001.200ANNUAL DEPARTURES*
F_AC_070500_1_0030201_01_00F_AC_070500_1_0030102_01_00
Flexible Pavement RequirementsWV000, MRW 233 900 kg, CG 37.4 % (Sheet 2 of 2)
FIGURE-7-5-0-991-003-A01
7-5-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 60 80
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 13.1 bar (190 psi)
(cm)
(in)
MAXIMUM POSSIBLE MAINGEAR LOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
10 000 COVERAGESUSED FOR ACNCALCULATIONS
6
3 10 15 20 30 40 60 806
10 15 20 30 40 60 80 100 120 150180
40 000 kg (88 175 lb)50 000 kg (110 225 lb)60 000 kg (132 275 lb)70 000 kg (154 325 lb)88 620 kg (195 375 lb)WEIGHT ON ONE MAIN LANDING GEAR
ALPHA FACTOR = 0.8*20 YEAR PAVEMENT LIFE25.00015.0006.0003.0001.200ANNUAL DEPARTURES*
F_AC_070500_1_0040101_01_00
Flexible Pavement RequirementsWV001, MRW 184 900 kg, CG 40.1 % (Sheet 1 of 2)
FIGURE-7-5-0-991-004-A01
7-5-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 60 80
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.5 bar (210 psi)
(cm)
(in)
6
3 10 15 20 30 40 60 806
10 15 20 30 40 60 80 100 120 150180
70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)100 000 kg (220 450 lb)111 670 kg (246 200 lb)WEIGHT ON ONE MAIN LANDING GEAR
10 000 COVERAGESUSED FOR ACNCALCULATIONS
MAXIMUM POSSIBLE MAINGEAR LOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
ALPHA FACTOR = 0.8*20 YEAR PAVEMENT LIFE25.00015.0006.0003.0001.200ANNUAL DEPARTURES*
F_AC_070500_1_0040201_01_00F_AC_070500_1_0040102_01_00
Flexible Pavement RequirementsWV054, MRW 235 900 kg, CG 35.7 % (Sheet 2 of 2)
FIGURE-7-5-0-991-004-A01
7-5-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A330-200 A330-200F A330-300
Flexible Pavement Requirements - LCN Conversion
1. This section gives data about the flexible pavement requirements for Load Classification Number(LCN) conversion.The flexible pavement requirements graphs are given at standard tire pressure for the weight variantsproducing (at the MRW and max aft CG) the lowest MLG load and the highest MLG load of eachA/C type.To find the aircraft weight that a flexible pavement can support, you must know the LCN of thepavement and the thickness.
Example, see FIGURE 7---0-99--010-A, calculation of the thickness of the flexible pavement for:- An aircraft with a MRW of 192 900 kg (425 275 lb),- The flexible pavement thickness is 1143 mm (45 in) with a related LCN of 108.The weight on one MLG is 80 000 kg (176 375 lb).
2. Flexible Pavement Requirements - LCN tableThe following table provides LCN data in tabular format similar to the one used by ICAO in the”Aerodrome Design Manual Part 3, Pavements - Edition 1977”. In order to use the system accuratelyyou should know the total pavement thickness for flexible pavement.However, the pavement thickness for a particular runway are not frequently published in the standardairport information sources (Jeppesen, AERAD, DOD, etc.).Therefore it is common practice to use a standard thickness (20 in) when determining the LCN andthe ESWL of the aircraft.
If the LCN for an intermediate weight between MRW and the empty weight of the aircraft is requiredor if the real thickness is known, refer to figures that follow.
NOTE : The CG in the figure title is the CG used for ACN / LCN calculation
7-6-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
AIRCRAFT TYPE
A330−200WV020
ALL UPMASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
FLEXIBLE PAVEMENTESWL
x 1000 kg h = 510 mm (20 in)
x 1000 lbLCN
230 900120 000
47.347.2
1.42 2814
6131
9654
A330−200WV021
230 900 47.347.2
A330−200WV022
233 900 47.347.2
A330−200WV023
233 900 47.347.2
A330−200WV024
202 900 47.547.3
24
A330−200WV025
220 900 47.447.2
27
A330−200WV026
192 900 47.547.4
23
A330−200WV027
220 900 47.447.2
27
A330−200WV050
230 900 47.347.2
28
A330−200WV051
192 900 47.547.4
23
A330−200WV052
233 900 47.347.2
28
A330−200WV053
210 900 47.447.3
25
A330−200WV054
230 900 47.347.2
28
A330−200WV055
192 900 47.547.4
23
A330−200WV056
233 900 47.347.2
28
A330−200WV057
236 900 46.746.6
28
A330−200WV058
238 900 46.346.2
28
A330−200WV059
202 900 47.547.3
24
A330−200WV060
220 900 47.447.2
27
A330−200WV061
230 900 47.347.2
28
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
281428142814
14
14
14
14
14
14
14
14
14
14
14
14
14
14
14
14 31 54
31 54
31 54
31 53
31 53
31 54
31 54
31 54
31 54
31 54
31 54
31 54
31 54
31 54
31 54
31 54
31 54
31 54
31 54
62
62
53
59
51
59
61
51
62
56
61
51
62
62
62
53
59
61
96
97
97
86
92
82
92
96
82
97
89
96
82
97
97
97
86
92
96
61120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
F_AC_070600_1_0100101_01_00
Flexible Pavement RequirementsLCN table
FIGURE-7-6-0-991-010-A01
7-6-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
50 0
00 k
g
(110
225
lb)
60 0
00 k
g
(132
275
lb)
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
91 6
70 k
g
(202
100
lb)
LAN
DIN
G G
EA
RW
EIG
HT
ON
ON
E M
AIN
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
1020
3040
5060
8010
010203040506070809010
0
110
120
130
140
150
160
500
750
1000
1500
2000
2500
203040506070
2030
4050
6080
7010
0 120
150 18
023
0
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
S
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070600_1_0010101_01_00
Flexible Pavement Requirements - LCNWV026, MRW 192 900 kg, CG 38.8 % (Sheet 1 of 2)
FIGURE-7-6-0-991-001-A01
7-6-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
1020
3040
5060
8010
0102030405060708090100
110
120
130
140
150
160
500
750
1000
1500
2000
2500
203040506070
2030
4050
6080
7010
0 120
150 18
023
0
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
S
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
100
000
kg
(22
0 45
0 lb
)11
0 67
0 kg
(
243
975
lb)
LAN
DIN
G G
EA
RW
EIG
HT
ON
ON
E M
AIN
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070600_1_0010201_01_00F_AC_070600_1_0010103_01_00
Flexible Pavement Requirements - LCNWV058, MRW 238 900 kg, CG 31.3 % (Sheet 2 of 2)
FIGURE-7-6-0-991-001-A01
7-6-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
AIRCRAFT TYPE
A330−200FWV000
ALL UPMASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
FLEXIBLE PAVEMENTESWL
x 1000 kg h = 510 mm (20 in)
x 1000 lbLCN
233 900120 000
47.347.2
1.42 2814
6231
9754
A330−200FWV001
227 900120 000
47.347.2
A330−200FWV002
1.42
1.42 2714 31 54
9561
2814
6231
9754
233 900120 000
47.347.2
F_AC_070600_1_0110101_01_00
Flexible Pavement RequirementsLCN table
FIGURE-7-6-0-991-011-A01
7-6-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
1020
3040
5060
8010
0102030405060708090100
110
120
130
140
150
160
500
750
1000
1500
2000
2500
203040506070
2030
4050
6080
7010
0 120
150 18
023
0
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
S
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
107
900
kg
(23
7 87
5 lb
)LA
ND
ING
GE
AR
WE
IGH
T O
N O
NE
MA
IN
60 0
00 k
g
(132
275
lb)
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070600_1_0020101_01_00
Flexible Pavement Requirements - LCNWV001, MRW 227 900 kg, CG 37.6 % (Sheet 1 of 2)
FIGURE-7-6-0-991-002-A01
7-6-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
1020
3040
5060
8010
0102030405060708090100
110
120
130
140
150
160
500
750
1000
1500
2000
2500
203040506070
2030
4050
6080
7010
0 120
150 18
023
0
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
S
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
100
000
kg
(22
0 45
0 lb
)11
0 67
0 kg
(
243
975
lb)
LAN
DIN
G G
EA
RW
EIG
HT
ON
ON
E M
AIN
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070600_1_0020201_01_00F_AC_070600_1_0020102_01_00
Flexible Pavement Requirements - LCNWV000, MRW 233 900 kg, CG 37.4 % (Sheet 2 of 2)
FIGURE-7-6-0-991-002-A01
7-6-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
AIRCRAFT TYPE
A330−300
WV001
WV003
WV002
WV004 (209)
WV010
WV004 (215)
WV010b
WV012
WV011
WV013
WV020
WV014
WV022
WV025
WV024
WV050
WV052
WV051
WV053
WV054
WV055
ALL UPMASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
FLEXIBLE PAVEMENTESWL
x 1000 kg h = 510 mm (20 in)
x 1000 lbLCN
212 900 47.447.3
1.31 2615
A330−300 212 900 47.447.3
1.31 26
A330−300 184 900 47.947.9
1.31 2215
A330−300 215 900 47.247.1
1.33 26
A330−300 215 900 47.847.7
1.33 26
A330−300 209 900 47.847.8
1.33 26
A330−300 217 900 47.046.9
1.33 26
A330−300 212 900 47.847.7
1.33 26
A330−300 217 900 47.847.7
1.33 27
A330−300 218 900 47.847.7
1.33 27
A330−300 205 900 47.947.8
1.33 25
A330−300 215 900 47.847.7
1.33 26
A330−300 230 900 47.847.7
1.42 28
A330−300 205 900 47.947.8
1.42 25
A330−300 233 900 47.747.6
1.45 28
A330−300 217 900 47.847.7
1.42 26
A330−300 212 900 47.847.7
1.45 26
A330−300 230 900 47.847.7
1.45 28
A330−300 233 900 47.747.6
1.45 28
A330−300 205 900 47.947.8
1.45 25
A330−300 235 900 47.347.2
1.45 28
A330−300 235 900 42.142.0
1.45 2513
15
15
15
15
15
15
15
15
15
15
15
15
15
15
15
15
15
15
15
WV0005733
8554
5733
8554
4933
7654
5732
8754
5833
8855
5633
8655
5832
8754
5733
8755
5933
8855
5933
8955
5533
8455
5833
8855
6233
9656
5533
8757
6333
9957
5833
9256
5733
9157
6233
9857
6333
9957
5533
8857
6333
9956
5529
8951
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
F_AC_070600_1_0120101_01_00
Flexible Pavement RequirementsLCN table
FIGURE-7-6-0-991-012-A01
7-6-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
1020
3040
5060
8010
0102030405060708090100
110
120
130
140
150
160
500
750
1000
1500
2000
2500
203040506070
2030
4050
6080
7010
0 120
150 18
023
0
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
1 ba
r (1
90 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
S
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
50 0
00 k
g
(110
225
lb)
60 0
00 k
g
(132
275
lb)
70 0
00 k
g
(154
325
lb)
40 0
00 k
g
(88
175
lb)
88 6
20 k
g
(195
375
lb)
LAN
DIN
G G
EA
RW
EIG
HT
ON
ON
E M
AIN
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070600_1_0030101_01_00
Flexible Pavement Requirements - LCNWV001, MRW 184 900 kg, CG 40.1 % (Sheet 1 of 2)
FIGURE-7-6-0-991-003-A01
7-6-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
1020
3040
5060
8010
0102030405060708090100
110
120
130
140
150
160
500
750
1000
1500
2000
2500
203040506070
2030
4050
6080
7010
0 120
150 18
023
0
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
5 ba
r (2
10 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
S
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
100
000
kg
(22
0 45
0 lb
)
LAN
DIN
G G
EA
RW
EIG
HT
ON
ON
E M
AIN
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
111
670
kg
(24
6 20
0 lb
)
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070600_1_0030201_01_00F_AC_070600_1_0030102_01_00
Flexible Pavement Requirements - LCNWV054, MRW 235 900 kg, CG 35.7 % (Sheet 2 of 2)
FIGURE-7-6-0-991-003-A01
7-6-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A330-200 A330-200F A330-300
Rigid Pavement Requirements - Portland Cement Association Design Method
1. This section gives data about the rigid pavement requirements for the PCA (Portland CementAssociation) design method.The rigid pavement requirements graphs are given at standard tire pressure for the weight variantsproducing (at the MRW and max aft CG) the lowest MLG load and the highest MLG load of eachA/C type.To find a rigid pavement thickness, you must know the Subgrade Modulus (K), the permittedworking stress and the weight on one MLG.The procedure that follows is used to develop rigid pavement design curves:- With the scale for pavement thickness on the left and the scale for permitted working stress on
the right, a random load line is made.This represents the MLG maximum weight to be shown.
- A plot is then made of all values of the subgrade modulus (k values).- More load lines for the incremental values of weight on the MLG are made based on the curve for
k= 80MN/m3 already shown on the graph.
Example, see FIGURE 7---0-99--001-A, calculation of the thickness of the rigid pavement for:- An aircraft with a MRW of 192 900 kg (425 275 lb),- A k value of 80 MN/m3 (300 lbf/in3),- A permitted working stress of 38.67 kg/cm2 (550 lb/in2),- The load on one MLG is 80 000 kg (176 375 lb).The required rigid pavement thickness is 230 mm (9 in).
NOTE : The CG in the figure title is the CG used for ACN / LCN calculation
7-7-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
60
50
40
30
20
10
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
60 000 kg (132 275 lb)70 000 kg (154 325 lb)80 000 kg (176 375 lb)91 670 kg (202 100 lb)LANDING GEARWEIGHT ON ONE MAIN
50 000 kg (110 225 lb)
F_AC_070700_1_0010101_01_00
Rigid Pavement RequirementsWV026, MRW 192 900 kg, CG 38.8 % (Sheet 1 of 2)
FIGURE-7-7-0-991-001-A01
7-7-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
60
50
40
30
20
10
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
80 000 kg (176 375 lb)90 000 kg (198 425 lb)100 000 kg (220 450 lb)110 670 kg (243 975 lb)LANDING GEARWEIGHT ON ONE MAIN
70 000 kg (154 325 lb)
F_AC_070700_1_0010201_01_00F_AC_070700_1_0010102_01_00
Rigid Pavement RequirementsWV058, MRW 238 900 kg, CG 31.3 % (Sheet 2 of 2)
FIGURE-7-7-0-991-001-A01
7-7-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
60
50
40
30
20
10
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)107 900 kg (237 875 lb)LANDING GEARWEIGHT ON ONE MAIN
60 000 kg (132 275 lb)
F_AC_070700_1_0020101_01_00
Rigid Pavement RequirementsWV001, MRW 227 900 kg, CG 37.6 % (Sheet 1 of 2)
FIGURE-7-7-0-991-002-A01
7-7-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
60
50
40
30
20
10
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
80 000 kg (176 375 lb)90 000 kg (198 425 lb)100 000 kg (220 450 lb)110 670 kg (243 975 lb)LANDING GEARWEIGHT ON ONE MAIN
70 000 kg (154 325 lb)
F_AC_070700_1_0020201_01_00F_AC_070700_1_0020102_01_00
Rigid Pavement RequirementsWV000, MRW 233 900 kg, CG 37.4 % (Sheet 2 of 2)
FIGURE-7-7-0-991-002-A01
7-7-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 13.1 bar (190 psi)
60
50
40
30
20
10
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
50 000 kg (110 225 lb)60 000 kg (132 275 lb)70 000 kg (154 325 lb)88 620 kg (195 375 lb)LANDING GEARWEIGHT ON ONE MAIN
40 000 kg (88 175 lb)
F_AC_070700_1_0030101_01_00
Rigid Pavement RequirementsWV001, MRW 184 900 kg, CG 40.1 % (Sheet 1 of 2)
FIGURE-7-7-0-991-003-A01
7-7-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.5 bar (210 psi)
60
50
40
30
20
10
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
80 000 kg (176 375 lb)90 000 kg (198 425 lb)100 000 kg (220 450 lb)111 670 kg (246 200 lb)LANDING GEARWEIGHT ON ONE MAIN
70 000 kg (154 325 lb)
F_AC_070700_1_0030201_01_00F_AC_070700_1_0030102_01_00
Rigid Pavement RequirementsWV054, MRW 235 900 kg, CG 35.7 % (Sheet 2 of 2)
FIGURE-7-7-0-991-003-A01
7-7-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-0 Rigid Pavement Requirements - LCN Conversion
**ON A/C A330-200 A330-200F A330-300
Rigid Pavement Requirements - LCN Conversion
1. This section gives data about the rigid pavement requirements for the Load Classification Number(LCN) conversion (radius of relative stiffness).The rigid pavement requirements graphs are given at standard tire pressure for the weight variantsproducing (at the MRW and max aft CG) the lowest MLG load and the highest MLG load of eachA/C type.To find the aircraft weight that a rigid pavement can support, you must know the LCN of thepavement and the radius of relative stiffness (L).The calculation of the radius of relative stiffness (L) is done with the formula and the table given in”Radius of Relative Stiffness” (L values based on Young’s Modulus (E) of 4 000 000 psi andPoisson’s Ratio (µ) of 0.15), see FIGURE 7---0-99--001-A.
Example, see FIGURE 7---0-99--004-A, calculation of the aircraft weight through the radius ofrelative stiffness (L) of the rigid pavement for:- An aircraft with a MRW of 192 900 kg (425 275 lb),- The radius of relative stiffness is shown at 1143 mm (45 in) with a related LCN of 83.The weight on one MLG is 80 000 kg (176 375 lb).
The following table provides LCN data in tabular format similar to the one used by ICAO in the”Aerodrome Design Manual Part 3, Pavements - Edition 1977”. In order to use the system accuratelyyou should know the total pavement radius of relative stiffness (L-value) for rigid pavement.However, the pavement radius of relative stiffness for a particular runway are not frequently publishedin the standard airport information sources (Jeppesen, AERAD, DOD, etc.).Therefore it is common practice to use a standard radius of relative stiffness (30 inches) whendetermining the LCN and the ESWL of the aircraft.If the LCN for an intermediate weight between maximum ramp weight and the empty weight of theaircraft is required or if the real thickness is known, refer to figures that follows.
2. Radius of Relative Stiffness (Other values of E and µ)This section gives data about the rigid pavement requirements for the Load Classification Number(LCN) conversion (radius of relative stiffness with other values of E (Young’s modulus) and µ(Poisson’s ratio).The other values of E and µ have an effect on the radius of relative stiffness value L.The effect of E and µ on the radius of relative stiffness value L is shown in the diagrams of FIGURE7---0-99--014-A.The table in FIGURE 7---0-99--001-ARadius of Relative Stiffness, shows values L based on a Young’smodulus (E) of 4 000 000 psi and a Poisson’s ratio (µ) of 0.15.To find values L, you must know the values of E and µ.
7-8-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Example, see FIGURE 7---0-99--014-A, calculation of values L of the rigid pavement for an E of 3000 000 psi.The ”E” factor is 0.931.The radius of relative stiffness value L is the value found in the table FIGURE 7---0-99--001-Amultiplied by 0.931.
NOTE : The CG in the figure title is the CG used for ACN / LCN calculation
7-8-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
AIRCRAFT TYPE
A330−200WV020
ALL UPMASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
RGID PAVEMENTESWL
x 1000 kg L = 760 mm (30 in)
x 1000 lbLCN
47.347.2
1.42
A330−200WV021
47.347.2
A330−200WV022
47.347.2
A330−200WV023
47.347.2
A330−200WV024
47.547.3
A330−200WV025
47.447.2
A330−200WV026
47.547.4
A330−200WV027
47.447.2
A330−200WV050
47.347.2
A330−200WV051
47.547.4
A330−200WV052
47.347.2
A330−200WV053
47.447.3
A330−200WV054
47.347.2
A330−200WV055
47.547.4
A330−200WV056
47.347.2
A330−200WV057
46.746.6
A330−200WV058
46.346.2
A330−200WV059
47.547.3
A330−200WV060
47.447.2
A330−200WV061
47.347.2
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
2613
5729
9049
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
13 29
26 57 9049
26 58 9149
26 58 9149
23 50 8250
25 55 8749
22 48 7850
25 55 8749
26 57 9049
22 48 7850
26 58 9149
24 52 8449
26 57 9049
22 48 7850
26 58 9149
26 58 9149
26 58 9148
23 50 8250
25 55 8749
26 57 9049
230 900120 000230 900120 000233 900
233 900
202 900
220 900
192 900
220 900
230 900
192 900
233 900
210 900
230 900
192 900
233 900
236 900
238 900
202 900
220 900
230 900
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
F_AC_070800_1_0170101_01_00
Rigid Pavement RequirementsLCN table
FIGURE-7-8-0-991-017-A01
7-8-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
AIRCRAFT TYPE
A330−300
ALL UPMASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
RIGID PAVEMENTESWL
x 1000 kg L = 760 mm (30 in)
x 1000 lbLCN
212 900125 000
47.447.3
1.31 2414WV000
5331
8150
WV001
WV002
WV003
WV004 (209)
WV004 (215)
WV010
WV010b
WV011
WV012
WV013
WV014
WV020
WV022
WV024
WV025
WV050
WV051
WV052
WV053
WV054
125 00047.947.9
1.31 2114
4631
7351
184 900
125 00047.447.3
1.31 2414
5331
8150
212 900
125 00047.247.1
1.33 2414
5331
8250
215 900
125 00047.847.8
1.33 2414
5231
8151
209 900
125 00047.847.7
1.33 2414
5431
8351
215 900
125 00047.046.9
1.33 2414
5330
8250
217 900
125 00047.847.7
1.33 2514
5431
8351
217 900
125 00047.847.7
1.33 2414
5331
8251
212 900
125 00047.847.7
1.33 2514
5531
8451
218 900
125 00047.847.7
1.33 2414
5431
8351
215 900
125 00047.947.8
1.33 2314
5131
8051
205 900
125 00047.847.7
1.42 2614
5831
9152
230 900
125 00047.747.6
1.45 2614
5831
9353
233 900
125 00047.947.8
1.42 2314
5131
8352
205 900
125 00047.847.7
1.42 2514
5431
8752
217 900
125 00047.847.7
1.45 2614
5831
9253
230 900
125 00047.847.7
1.45 2414
5331
8653
212 900
125 00047.747.6
1.45 2614
5831
9353
233 900
125 00047.947.8
1.45 2314
5131
8453
205 900
125 00047.347.2
1.45 2614
5831
9352
235 900
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
F_AC_070800_1_0170201_01_00
Rigid Pavement RequirementsLCN table
FIGURE-7-8-0-991-017-B01
7-8-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
AIRCRAFT TYPE
A330−200FWV000
ALL UPMASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
RIGID PAVEMENTESWL
x 1000 kg L = 760 mm (30 in)
x 1000 lbLCN
233 900120 000
47.347.2
1.42 2613
5829
9149
A330−200FWV001
227 900120 000
47.347.2
A330−200FWV002
1.42
1.42 2613 29 49
8956
2613
5829
9149
233 900120 000
47.347.2
F_AC_070800_1_0170302_01_00
Rigid Pavement RequirementsLCN table
FIGURE-7-8-0-991-017-C01
7-8-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
WHERE
=
E
k
d
Ed4
=
=
=
dk
= 24.1652 4
RIGID PAVEMENT THICKNESS, (in)
YOUNG’S MODULUS = 4 x 10 psi
RADIUS OF RELATIVE STIFFNESS VALUES IN INCHES
L
SUBGRADE MODULUS, lb/in
= POISSON’S RATIO = 0.15
6.06.57.07.5
31.4833.4335.3437.22
29.3031.1132.8934.63
26.4728.1129.7231.29
24.6326.1627.6529.12
23.3024.7426.1527.54
22.2623.6424.9926.32
21.4222.7424.0425.32
20.7222.0023.2524.49
19.1320.3121.4722.61
8.08.59.09.5
39.0640.8842.6744.43
36.3538.0439.7141.35
32.8534.3735.8837.36
30.5731.9933.3934.77
28.9130.2531.5832.89
27.6228.9130.1731.42
26.5827.8129.0330.23
25.7026.9028.0829.24
23.7424.8425.9327.00
10.010.511.011.5
46.1847.9049.6051.28
38.8340.2841.7143.12
36.1437.4838.8140.13
34.1735.4536.7137.95
32.6533.8735.0736.26
31.4232.5933.7534.89
30.3931.5232.6433.74
28.0629.1130.1431.16
12.012.513.013.5
52.9454.5956.2257.83
49.2750.8052.3253.82
44.5245.9047.2748.63
41.4342.7243.9945.26
39.1840.4041.6142.80
37.4438.6039.7540.89
36.0237.1438.2539.35
34.8435.9236.9938.06
32.1733.1734.1635.14
14.014.515.015.5
16.016.517.017.5
55.3156.7858.2559.70
65.6967.2368.7570.26
61.1362.5663.9865.38
49.9851.3152.6353.94
46.5147.7548.9850.20
43.9845.1646.3247.47
55.2456.5357.8159.08
51.4152.6153.8054.98
48.6249.7550.8852.00
42.0243.1544.2645.36
40.4441.5142.5843.64
39.1140.1541.1942.21
36.1237.0838.0338.98
46.4547.5448.6149.68
44.7045.7446.7747.80
43.2344.2445.2446.23
39.9240.8541.7842.70
18.019.020.021.0
22.023.024.025.0
71.7674.7377.6680.55
83.4186.2489.0491.81
66.7869.5472.2774.96
77.6380.2682.8685.44
60.3462.8465.3067.74
70.1472.5274.8777.20
56.1558.4860.7763.04
65.2867.4969.6871.84
53.1155.3157.4759.62
61.7363.8365.9067.95
50.7452.8454.9156.96
58.9860.9862.9664.92
48.8250.8452.8454.81
56.7558.6860.5862.46
54.8956.7558.5960.41
47.2249.1751.1053.01
43.6145.4147.1948.95
50.6952.4154.1155.79
d k=75 k=100 k=150 k=200 k=250 k=300 k=350 k=400 k=550
59.4361.0262.5964.15
42.9744.5746.1647.72
( )L
12 (1 − ) k
REFERENCE: PORTLAND CEMENT ASSOCIATION
F_AC_070800_1_0010101_01_00
Radius of Relative Stiffness (L)FIGURE-7-8-0-991-001-A01
7-8-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
102030405060708090100
110
120
750
1000
1500
2000
2500
2030
4050
6070
8090
100
2030
4050
6070
8010
0 12015
0 18023
0
101520253035404550 5
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
50 0
00 k
g
(110
225
lb)
60 0
00 k
g
(132
275
lb)
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
91 6
70 k
g
(202
100
lb)
LAN
DIN
G G
EA
RW
EIG
HT
ON
ON
E M
AIN
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070800_1_0040101_01_00
Rigid Pavement Requirements - LCNWV026, MRW 192 900 kg, CG 38.8 % (Sheet 1 of 2)
FIGURE-7-8-0-991-004-A01
7-8-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
102030405060708090100
110
120
750
1000
1500
2000
2500
2030
4050
6070
8090
100
2030
4050
6070
8010
0 12015
0 18023
0
101520253035404550 5
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
100
000
kg
(22
0 45
0 lb
)11
0 67
0 kg
(
243
975
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070800_1_0050101_01_00F_AC_070800_1_0040102_01_00
Rigid Pavement Requirements - LCNWV058, MRW 238 900 kg, CG 31.3 % (Sheet 2 of 2)
FIGURE-7-8-0-991-004-A01
7-8-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
102030405060708090100
110
120
750
1000
1500
2000
2500
2030
4050
6070
8090
100
2030
4050
6070
8010
0 12015
0 18023
0
101520253035404550 5
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
107
900
kg
(23
7 87
5 lb
)W
EIG
HT
ON
ON
E M
AIN
LA
ND
ING
GE
AR
60 0
00 k
g
(132
275
lb)
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070800_1_0060101_01_00
Rigid Pavement Requirements - LCNWV001, MRW 227 900 kg, CG 37.6 % (Sheet 1 of 2)
FIGURE-7-8-0-991-006-A01
7-8-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
102030405060708090100
110
120
750
1000
1500
2000
2500
2030
4050
6070
8090
100
2030
4050
6070
8010
0 12015
0 18023
0
101520253035404550 5
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
1400
x530
R23
OR
54x
21−
23
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
100
000
kg
(22
0 45
0 lb
)11
0 67
0 kg
(
243
975
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070800_1_0060201_01_00F_AC_070800_1_0060102_01_00
Rigid Pavement Requirements - LCNWV000, MRW 233 900 kg, CG 37.4 % (Sheet 2 of 2)
FIGURE-7-8-0-991-006-A01
7-8-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
102030405060708090100
110
120
750
1000
1500
2000
2500
2030
4050
6070
8090
100
2030
4050
6070
8010
0 12015
0 18023
0
101520253035404550 5
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
1bar
(19
0 ps
i)14
00x5
30R
23 O
R 5
4x21
−23
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
50 0
00 k
g
(110
225
lb)
60 0
00 k
g
(132
275
lb)
70 0
00 k
g
(154
325
lb)
40 0
00 k
g
(88
175
lb)
88 6
20 k
g
(195
375
lb)
LAN
DIN
G G
EA
RW
EIG
HT
ON
ON
E M
AIN
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
F_AC_070800_1_0070101_01_00
Rigid Pavement Requirements - LCNWV001, MRW 184 900 kg, CG 40.1 % (Sheet 1 of 2)
FIGURE-7-8-0-991-007-A01
7-8-0Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
102030405060708090100
110
120
750
1000
1500
2000
2500
2030
4050
6070
8090
100
2030
4050
6070
8010
0 12015
0 18023
0
101520253035404550 5
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
5 ba
r (2
10 p
si)
1400
x530
R23
or
54x2
1−23
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
in)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
SE
CO
ND
ED
ITIO
N 1
965
NO
TE
:
EQUIVALENT SINGLE WHEEL LOAD (1000 lb)
EQUIVALENT SINGLE WHEEL LOAD (1000 kg)
70 0
00 k
g
(154
325
lb)
80 0
00 k
g
(176
375
lb)
90 0
00 k
g
(198
425
lb)
100
000
kg
(22
0 45
0 lb
)11
1 67
0 kg
(
246
200
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
DA
FT
CG
F_AC_070800_1_0070201_01_00F_AC_070800_1_0070102_01_00
Rigid Pavement Requirements - LCNWV054, MRW 235 900 kg, CG 35.7 % (Sheet 2 of 2)
FIGURE-7-8-0-991-007-A01
7-8-0Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-200F A330-300
0 1 2 3 4 50.80
0.85
0.90
0.95
1.00
1.05
1.10EFFECT OF E ON
E F
AC
TO
R
0.00 0.05 0.10 0.15 0.20 0.250.995
1.000
1.005
1.010
1.015EFFECT OF
FA
CT
OR
, POISSON’S RATIO
NOTE: BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE
E, YOUNG’S MODULUS (10 psi)
ON
OF RADIUS OF RELATIVE STIFFNESS ( ) TABLEL
VALUESL
VALUESL
L VALUESF_AC_070800_1_0140101_01_00
Radius of Relative Stiffness (Effect E and µ ON ”L” values)FIGURE-7-8-0-991-014-A01
7-8-0Page 13
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements
**ON A/C A330-200 A330-200F A330-300
Aircraft Classification Number - Flexible and Rigid Pavement
1. This section gives data about the Aircraft Classification Number (ACN) for an aircraft gross weight inrelation with a subgrade strength value for flexible and rigid pavement.The flexible and rigid pavement requirements graphs are given at standard tire pressure for theweight variants producing (at the MRW and max aft CG) the lowest MLG load and the highest MLGload of each A/C type.To find the ACN of an aircraft on flexible and rigid pavement, you must know the aircraft grossweight and the subgrade strength.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref: ICAO Aerodrome Design Manual, Part 3, Chapter 1, Second Edition 1983).
Example, see FIGURE 7---0-99--008-A (sheet 1), calculation of the ACN for flexible pavement for:- An aircraft with a MRW of 192 900 kg (425 275 lb),- An aircraft gross weight of 180 000 kg (396 825 lb),- A medium subgrade strength (code B).The ACN for flexible pavement is 45.
Example, see FIGURE 7---0-99--008-A (sheet 2), calculation of the ACN for rigid pavement for:- An aircraft with a MRW of 192 900 kg (425 275 lb),- An aircraft gross weight of 180 000 kg (396 825 lb),- A medium subgrade strength (code B).The ACN for rigid pavement is 45.
2. Aircraft Classification Number - ACN tableThe table FIGURE 7---0-99--001-A, FIGURE 7---0-99--002-A and FIGURE 7---0-99--003-A provideACN data in tabular format similar to the one used by ICAO in the ”Aerodrome Design Manual Part3, Pavements - Edition 1983”. If the ACN for an intermediate weight between MRW and theminimum weight of the aircraft is required, refer to figures that follows.
NOTE : The CG in the figure title is the CG used for ACN / LCN calculation
7-9-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
AIRCRAFT TYPE
A330−200WV020
ALL UPMASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
230 900120 000
47.347.2
1.42
A330−200WV021
230 900120 000
47.347.2
A330−200WV022
233 900 47.347.2
A330−200WV023
233 900 47.347.2
A330−200WV024
202 900 47.547.3
A330−200WV025
220 900 47.447.2
A330−200WV026
192 900 47.547.4
A330−200WV027
220 900 47.447.2
A330−200WV050
230 900 47.347.2
A330−200WV051
192 900 47.547.4
A330−200WV052
233 900 47.347.2
A330−200WV053
210 900 47.447.3
A330−200WV054
230 900 47.347.2
A330−200WV055
192 900 47.547.4
A330−200WV056
233 900 47.347.2
A330−200WV057
236 900 46.746.6
A330−200WV058
238 900 46.346.2
A330−200WV059
202 900 47.547.3
A330−200WV060
220 900 47.447.2
A330−200WV061
230 900 47.347.2
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
120 000
5328
ACN FOR
High150
RIGID PAVEMENTSUBGRADES − MN/m³
6127
Medium80
7230
Low40
8535
Ultral−low20
5726
ACN FOR
High15
FLEXIBLE PAVEMENTSUBGRADES − CBR
6227
Medium10
7130
Low6
9736
Ultral−low3
53 6127
7230
8535
5726
6227
71 97
28
28
28
28
28
28
28
28
28
28
28
28
28
27
27
27
28
28
28
27
27
27
27
27
27
27
27
27
27
27
27
27
27
26
27
27
27
54
54
45
50
43
50
53
43
54
47
53
43
54
54
54
45
50
53
62 7430
8635
5826
63 73 98
62 7430
8635
5826
63 73 98
52 6131
7135
4926
52 60 8037
58 6831
8035
5426
58 67 9136
49 5731
6735
4626
49 56 7537
58 6831
8035
5426
58 67 9136
61 7230
8535
5726
62 71 9736
49 5731
6735
4626
49 56 7537
62 7430
8635
5826
63 73 9836
54 6431
7535
5126
55 63 8537
61 7230
8535
5726
62 71 9736
49 5731
6735
4626
49 56 7537
62 7430
8635
5826
63 73 9836
62 7430
8634
5826
63 73 9836
62 7430
8634
5825
63 73 9835
52 6131
7135
4926
52 60 8037
58 6831
8035
5426
58 67 9136
61 7230
8535
5726
62 71 973627
27
27
26
27
27
27
27
27
27
27
27
27
27
27
27
27
27
30
30
30
29
29
30
30
30
30
30
30
30
30
30
30
30
30
30
30 36
36
36
F_AC_070900_1_0010101_01_00
Aircraft Classification NumberACN Table
FIGURE-7-9-0-991-001-A01
7-9-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
300
400
500
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0080101_01_00
Aircraft Classification NumberFlexible Pavement - WV026, MRW 192 900 kg, CG 38.8 % (Sheet 1 of 2)
FIGURE-7-9-0-991-008-A01
7-9-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
250
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
300
350
400
450
500
550
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
F_AC_070900_1_0080102_01_00
Aircraft Classification NumberRigid Pavement - WV026, MRW 192 900 kg, CG 38.8 % (Sheet 2 of 2)
FIGURE-7-9-0-991-008-A01
7-9-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
300
400
500
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0110101_01_00
Aircraft Classification NumberFlexible Pavement - WV058, MRW 238 900 kg, CG 31.3 % (Sheet 1 of 2)
FIGURE-7-9-0-991-011-A01
7-9-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
250
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
300
350
400
450
500
550
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
F_AC_070900_1_0110102_01_00
Aircraft Classification NumberRigid Pavement - WV058, MRW 238 900 kg, CG 31.3 % (Sheet 2 of 2)
FIGURE-7-9-0-991-011-A01
7-9-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
AIRCRAFT TYPEALL UP
MASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
5428
ACN FOR
High150
RIGID PAVEMENTSUBGRADES − MN/m³
6227
Medium80
7430
Low40
8635
Ultral−low20
5826
ACN FOR
High15
FLEXIBLE PAVEMENTSUBGRADES − CBR
6327
Medium10
7330
Low6
9836
Ultral−low3
A330−200FWV000
233 900120 000
47.347.2
1.42
A330−200FWV001
227 900120 000
47.347.2
A330−200FWV002
1.42
1.42
233 900120 000
47.347.2
28 27 30 35 26 27 30 36
28 27 30 35 26 27 30 3654 62 74 86 58 63 73 98
52 60 71 83 56 61 70 95
F_AC_070900_1_0020101_01_00
Aircraft Classification NumberACN Table
FIGURE-7-9-0-991-002-A01
7-9-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
300
400
500
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0090101_01_00
Aircraft Classification NumberFlexible Pavement - WV001, MRW 227 900 kg, CG 37.6 % (Sheet 1 of 2)
FIGURE-7-9-0-991-009-A01
7-9-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
250
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
300
350
400
450
500
550
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
F_AC_070900_1_0090102_01_00
Aircraft Classification NumberRigid Pavement - WV001, MRW 227 900 kg, CG 37.6 % (Sheet 2 of 2)
FIGURE-7-9-0-991-009-A01
7-9-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
300
400
500
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0120101_01_00
Aircraft Classification NumberFlexible Pavement - WV000, MRW 233 900 kg, CG 37.4 % (Sheet 1 of 2)
FIGURE-7-9-0-991-012-A01
7-9-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
250
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
300
350
400
450
500
550
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
F_AC_070900_1_0120102_01_00
Aircraft Classification NumberRigid Pavement - WV000, MRW 233 900 kg, CG 37.4 % (Sheet 2 of 2)
FIGURE-7-9-0-991-012-A01
7-9-0Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
AIRCRAFT TYPEALL UP
MASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
4628472846284728472848284728482847284528532955294629502954294829552947295529
ACN FOR
High150
RIGID PAVEMENTSUBGRADES − MN/m³
5327
Medium80
6331
Low40
7536
Ultral−low20
5127
ACN FOR
High15
FLEXIBLE PAVEMENTSUBGRADES − CBR
5528
Medium10
6431
Low6
8639
Ultral−low3
A330−300
WV001
WV003
WV002
WV004 (209)
WV010
WV004 (215)
WV010b
WV012
WV011
WV013
WV020
WV014
WV022
WV025
WV024
WV050
WV052
WV051
WV053
WV054
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
A330−300
WV000212 900 47.4
47.31.31
212 900 47.447.3
1.31
184 900 47.947.9
1.31
215 900 47.247.1
1.33
215 900 47.847.7
1.33
209 900 47.847.8
1.33
217 900 47.046.9
1.33
212 900 47.847.7
1.33
217 900 47.847.7
1.33
218 900 47.847.7
1.33
205 900 47.947.8
1.33
215 900 47.847.7
1.33
230 900 47.847.7
1.42
205 900 47.947.8
1.42
233 900 47.747.6
1.45
217 900 47.847.7
1.42
212 900 47.847.7
1.45
230 900 47.847.7
1.45
233 900 47.747.6
1.45
205 900 47.947.8
1.45
235 900 47.347.2
1.45
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
125 000
4528
5332
6237
4428
4729
5332
7139
5327
6331
7536
5127
5528
6431
8639
5427
6531
7636
5227
5628
6531
8738
5328
6332
7437
5127
5529
6332
8539
5528
6632
7737
5327
5729
6632
8939
5527
6531
7636
5227
5628
6531
8838
5628
6732
7837
5327
5829
6732
9039
5428
6532
7637
5227
5629
6432
8739
5628
6732
7937
5427
5829
6732
9139
5528
6632
7737
5327
5729
6632
8939
5228
6232
7237
5027
5429
6232
8339
6229
7332
8637
5828
6229
7232
9839
6329
7533
8738
5928
6329
7432
10039
5329
6333
7338
5028
5429
6232
8339
5729
6833
7937
5428
5829
6732
9039
6229
7433
8638
5828
6229
7232
9839
5629
6633
7738
5228
5629
6532
8739
6329
7533
8738
5928
6329
7432
10039
5429
6333
7438
5028
5429
6232
8339
6328
7532
8737
5927
6329
7431
10039
46284028
F_AC_070900_1_0030101_01_00
Aircraft Classification NumberACN Table
FIGURE-7-9-0-991-003-A01
7-9-0Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
300
400
500
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(190
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0100101_01_00
Aircraft Classification NumberFlexible Pavement - WV001, MRW 184 900 kg, CG 40.1 % (Sheet 1 of 2)
FIGURE-7-9-0-991-010-A01
7-9-0Page 13
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
250
(x 1
000
lb)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(190
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
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F_AC_070900_1_0100102_01_00
Aircraft Classification NumberRigid Pavement - WV001, MRW 184 900 kg, CG 40.1 % (Sheet 2 of 2)
FIGURE-7-9-0-991-010-A01
7-9-0Page 14
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
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(x 1
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Aircraft Classification NumberFlexible Pavement - WV054, MRW 235 900 kg, CG 35.7 % (Sheet 1 of 2)
FIGURE-7-9-0-991-013-A01
7-9-0Page 15
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
100
120
140
160
110
130
150
170
180
190
200
210
220
230
240
250
0102030405060708090100
110
120
250
(x 1
000
lb)
TIR
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ON
ST
AN
T A
T 1
4.5
bar
(210
psi
)14
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4x21
−23
(bi
as)
TIR
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SE
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EC
TIO
N 7
−4−
0
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
AIR
CR
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T G
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WE
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CO
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N 1
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L P
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AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
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EN
CE
D IN
300
350
400
450
500
550
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
C −
K =
40
MN
/m³
(LO
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B −
K =
80
MN
/m³
(M
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IUM
)A
− K
= 1
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³ (
HIG
H)
F_AC_070900_1_0130102_01_00
Aircraft Classification NumberRigid Pavement - WV054, MRW 235 900 kg, CG 35.7 % (Sheet 2 of 2)
FIGURE-7-9-0-991-013-A01
7-9-0Page 16
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
**ON A/C A330-200 A330-200F A330-300
Scaled Drawings
1. This section provides the scaled drawings.
NOTE : When printing this drawing, make sure to adjust for proper scaling.
8-0-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200
010
2030
40F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40FEET
0 4 8 12 16 20METERS
NOTE:WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.
5060
50 60
F_AC_080000_1_0020101_01_00
Scaled DrawingFIGURE-8-0-0-991-002-A01
8-0-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-300
010
2030
40F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40FEET
0 4 8 12 16 20METERS
NOTE:WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.
5060
50 60
F_AC_080000_1_0020201_01_00
Scaled DrawingFIGURE-8-0-0-991-002-B01
8-0-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
010
2030
40F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40FEET
0 4 8 12 16 20METERS
NOTE:WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.
5060
50 60
F_AC_080000_1_0020301_01_00
Scaled DrawingFIGURE-8-0-0-991-002-C01
8-0-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A330-200 A330-300
Aircraft Rescue and Fire Fighting
1. Aircraft Rescue and Fire Fighting ChartsThis sections gives data related to aircraft rescue and fire fighting.The figures contained in this section are the figures that are in the Aircraft Rescue and Fire FightingCharts (ARFC) poster available on AIRBUSWorld and the Airbus website.
10-0-0Page 1
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0010101_01_00
Front PageFIGURE-10-0-0-991-001-A01
10-0-0Page 2
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0020101_01_00
Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-002-A01
10-0-0Page 3
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0030101_01_00
Crew Rest Compartments LocationFIGURE-10-0-0-991-003-A01
10-0-0Page 4
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0040101_01_00
Wheel/Brake OverheatWheel Safety Area (Sheet 1 of 2)
FIGURE-10-0-0-991-004-A01
10-0-0Page 5
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0040102_01_00
Wheel/Brake OverheatRecommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-004-A01
10-0-0Page 6
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0050101_01_00
Composite Materials LocationFIGURE-10-0-0-991-005-A01
10-0-0Page 7
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
BA
AB
F_AC_100000_1_0060101_01_00
Ground Lock Safety DevicesFIGURE-10-0-0-991-006-A01
10-0-0Page 8
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0070101_01_00
Emergency Evacuation DevicesFIGURE-10-0-0-991-007-A01
10-0-0Page 9
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0080101_01_00
Pax/Crew Doors and Emergency ExitsFIGURE-10-0-0-991-008-A01
10-0-0Page 10
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
122C
R
FW
D
7155
JE 196B
B
152N
R/
197C
B
F_AC_100000_1_0090101_01_00
FWD and AFT Lower Deck Cargo DoorsFIGURE-10-0-0-991-009-A01
10-0-0Page 11
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
A B CD
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A
R O
UTE
R T
K
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KO
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INC
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IN R
PLN
TO
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LOW
FAS
T
OFF
E
B
D
F_AC_100000_1_0100101_01_00
Control PanelsFIGURE-10-0-0-991-010-A01
10-0-0Page 12
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
A
315A
L
316A
R
A
F_AC_100000_1_0110101_01_00
APU Compartment AccessFIGURE-10-0-0-991-011-A01
10-0-0Page 13
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0120101_01_00
Ground ClearancesFIGURE-10-0-0-991-012-A01
10-0-0Page 14
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200 A330-300
F_AC_100000_1_0130101_01_00
Structural Break-in PointsFIGURE-10-0-0-991-013-A01
10-0-0Page 15
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
Aircraft Rescue and Fire Fighting
1. Aircraft Rescue and Fire Fighting ChartsThis sections gives data related to aircraft rescue and fire fighting.The figures contained in this section are the figures that are in the Aircraft Rescue and Fire FightingCharts (ARFC) poster available on AIRBUSWorld and the Airbus website.
10-0-0Page 16
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0140101_01_00
Front PageFIGURE-10-0-0-991-014-A01
10-0-0Page 17
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0150101_01_00
Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-015-A01
10-0-0Page 18
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0160101_01_00
Wheel/Brake OverheatWheel Safety Area (Sheet 1 of 2)
FIGURE-10-0-0-991-016-A01
10-0-0Page 19
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0160102_01_00
Wheel/Brake OverheatRecommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-016-A01
10-0-0Page 20
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0180101_01_00
Composite Materials LocationFIGURE-10-0-0-991-018-A01
10-0-0Page 21
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
BA
AB
F_AC_100000_1_0190101_01_00
Ground Lock Safety DevicesFIGURE-10-0-0-991-019-A01
10-0-0Page 22
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0200101_01_00
Emergency Evacuation DevicesFIGURE-10-0-0-991-020-A01
10-0-0Page 23
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0210101_01_00
Crew Doors and Emergency ExitsFIGURE-10-0-0-991-021-A01
10-0-0Page 24
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
122C
R
FW
D
7155
JE 196B
B
152N
R/
197C
B
F_AC_100000_1_0220101_01_00
Cargo DoorsFWD and AFT Lower Deck Compartments (Sheet 1 of 2)
FIGURE-10-0-0-991-022-A01
10-0-0Page 25
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
221N
Q
835B
L
803M
J
805M
J
F_AC_100000_1_0220102_01_00
Cargo DoorsUpper Deck Compartment (Sheet 2 of 2)
FIGURE-10-0-0-991-022-A01
10-0-0Page 26
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
CA
B F
AN
SE
XTR
AC
TA
VN
CS
BTL
2
BTL
1
TES
TD
ISC
HA
GE
NT
SMO
KE
SQU
IBSM
OK
ESQ
UIB
OFF
FAU
LT
OFF
FAU
LT
OFF
FAU
LT
CA
RG
O S
MO
KE
/ A
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ON
DC
AB
MD
& L
AV
FA
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OL
VA
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HE
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R
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AR
GO
SM
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LATI
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EN
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AN
STA
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LTO
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FF/R
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FF/R
PR
IM 2
PR
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RA
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LT
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LD F
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TK
C
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B
D
F_AC_100000_1_0230101_01_00
Control PanelsFIGURE-10-0-0-991-023-A01
10-0-0Page 27
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
A
315A
L
316A
R
A
F_AC_100000_1_0240101_01_00
APU Compartment AccessFIGURE-10-0-0-991-024-A01
10-0-0Page 28
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
F_AC_100000_1_0250101_01_00
Ground ClearancesFIGURE-10-0-0-991-025-A01
10-0-0Page 29
Apr 01/13
@A330AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-200F
AA
AA
AA
AF
WD
F_AC_100000_1_0260101_01_00
Structural Break-in PointsFIGURE-10-0-0-991-026-A01
10-0-0Page 30
Apr 01/13