ATR -600 Series The Latest
GenerationTurboprop
VERSATILITY
COMFORT
TECHNOLOGY
InnovationATR Never Ending
Reinforcingleadershipin the turboprop marketOne of the key success factors of the ATR Program has been the continuous attention to the market evolution, to meet the rigo-rous requirements of the regional airlines.
Leader in the 50-70 seat turboprop market, ATR’s fundamental strategy is to maintain the main strengths of its products, unbea-table operational costs, high reliability, pas-senger comfort and family concept, while continuing to innovate and develop product and services to satisfy the demands of ATR operators worldwide.
2 •ATR -600 SERIES
ATR -600 SERIES•3
In addition to the continuous design changes policy to comply with latest regulatory requirement evolutions, ATR is offering to regional airlines
original and advanced solutions, keeping in mind essential drivers:
Further enhance ATR competitiveness
Reinforce and optimise operational flexibility
Contribute to cost reduction initiatives
Maintain the general ATR design philosophy,
in terms of:
Efficiency
Easy retrofit
High maintainability and reliability
Strong commonality
Low operating cost.
ATR Series -600Product Strategy
Three main development axis have been identified and will be integral part of a significant model evolution:
Performance enhan-cement and expan-ded operational ver-satility
Passengers' comfort and appeal
Technology upgrade
Temperature or altitude extremes from the Equator to the Arctic Circle are the daily environment for ATR aircraft. Operated today in all types of climates and conditions, ATR operational flexibi-
lity and versatility are recognized worldwide by regional operators.
Low weights, together with an advanced aerodynamic design and state-of-the-art Pratt & Whitney Canada PW100 Series engines, keep fuel burn to a minimum.
Expanding further operational versatility is the objective of ATR, to provide airlines with tailored performance to suit regional operations and increase revenues.
Providing exactly what the customer needs in a fast evolving market.
Tailored toRegional Operation
4 •ATR -600 SERIES
EXPANDING OPERATIONAL VERSATILITY
Enhanced Performance
and ExpandedOperational Versatility
Increased ATR 72-600 operational weights
Improved « hot & high » airport perfor-mance with PW127M engine
PW127M multi-rated engine
Short runways’ take-off performance
ATR -600 SERIES•5
EXPANDING OPERATIONAL VERSATILITY
Max Take-Off Weight From 22,500 kg (49,604 lb) up to 23,000 kg (50,706 lb)
Max Zero Fuel Weight From 20,500 kg (45,195 lb) up to 21,000 kg(46,297 lb)
Following a strong market requirement, ATR 72-600 is
offered with increased payload, making the aircraft even more attractive, also in terms of operational range.
Up to 500 kg (1,100 lb) higher payload for the same range, with addi-tional 5-pax revenue
or 190 Nm (350 km) extended range perfor-mance at same payload are now available with MTOW and MZFW increase of 500 kg(1,100 lb).
ADVANTAGES
Higher weights meet new regulations cal-ling for heavier pas-senger and baggage weight
Meets airline require-ments for high density cabin layouts
Increased ATR 72-600 Operational Weights
ISA - No wind - JAR Reserves - Typical European Airline OEW
641 nm828 nm
0
1,000
2,000
3,000
4,000
5,000
6,000
7,000
8,000
9,000
0 500 1,000 1,500 2,000Range (Nm)
ATR72-60070 pax @ 95 kg
640 Nm
830 Nm
Payload (kg)
Basic WeightsATR 72-500MTOW 22,500 kgMZFW 20,500 kg
Optional WeightsATR 72-600MTOW 23,000 kgMZFW 21,000 kg
RangPW1
TLS
BUD
EDI
FRA
FCO
LCY
CDG
MAD
LIS
TUNALG
AMS
BRU
HAM
PRG
BTS
MXP
NAP
VIE
CPH
BEG
DUB
SVQ
WAW
BMAFBU
830 Nm
70 pax @ 95 kg (225 lb)Up to 830 Nm
6 •ATR -600 SERIES
ATR 72-500 ATR 72-600
Basic OptionalMTOW 22,500 kg
49,604 lb22,800 kg50,265 lb
23,000 kg50,706 lb
MLW 22,350 kg49,272 lb
22,350 kg49,272 lb
22,350 kg49,272 lb
MZFW 20,500 kg45,195 lb
20,800 kg45,855 lb
21,000 kg46,297 lb
OEW (Basic) 12,950 kg28,549 lb
13,010 kg28,682 lb
13,010 kg28,682 lb
Max Payload 7,550 kg16,645 lb
7,790 kg17,173 lb
7,990 kg17,614 lb
EXPANDING OPERATIONAL VERSATILITY
Additional revenues in severe environments: PW127M
TAKE-OFF FROM DENVER
Altitude: 5,333 ftOAT: 77°F (25°C)64 pax @ 220 lb (100 kg)OEW : 29,650 lb (13,450 kg)
+ 225 Nm with same payload or+ 5 passengers for the same distance
With the scope to provide even better performance and additional payload for the most demanding networks (hot & high
airports, mountainous environment), ATR is offering a more powerful engine: the PW127M.The PW127M delivers 5% higher thermodynamic power at Take-Off and Max Continuous ratings.
Thanks to the new ratings, performance will improve in terms of :
Take-off weight between 500 kg and 600 kg (1,100 lb to 1,320 lb) when limitations exist
Single-Engine Net ceiling increased by about 1,000 ft.
+ 1,000 ft Single-Engine Net Ceiling
IMPROVED MAX CONTI-NUOUS RATING WITH PW127M
Range with PW127M
Range with PW127F
130 Nm (240 km) range (PW127F)355 Nm (658 km) range (PW 127M)
ATR -600 SERIES•7
EXPANDING OPERATIONAL VERSATILITY
Multi-Rated Engine Power
A unique engine hardware PW 127 for three power settings: PW127E, PW127F, PW127M
Engine rating selected through airframe identification system (EEC multi-configura-tion)*Two levels of power will be available for the ATR 72, allowing PW127F ratings for standard operations or PW127M ratings for ‘hot & high’ operations, through the ‘Flex Operation’ concept.
The benefits of this concept for an airline come essentially from the optimisation of a mixed ATR fleet. The management of the engines fleet durability (Life Limited Parts impact) will be facilitated and maintenance costs controlled and optimised.
This engine is made available by early 2008 and it is designed to be retrofitable on ATR -500 Series.
Electronic Engine Control Rating
PW127M «Flex» Operation ConceptP/B: Push/ButtonCAP: Crew Alerting PanelERIU: Engine Rating Interface UnitFDAU: Flight Data Acquisition Unit
8 •ATR -600 SERIES
EXPANDING OPERATIONAL VERSATILITY
Thanks to full RTO take-off procedure, ATR 72-600 can carry up to 70 passengers on a 300 Nm(550 km) sector distance (RW10, no wind, dry runway, 10°C).
ATR 72 aircraft have 6° steep slope approach capability, allowing operations into difficult access airports.
London City Airport Operation
ATR 72-600 can operate profitably on London City airport
In order to respond to even more stringent requirements coming from emerging markets and to assure air transport connexions to remote
regions, ATR has developed a tailored solution, with the objective to further improve take-off capabilities on very short runways. Thanks to this option, ATR 72-600 will be able to operate profitably from very short runways everywhere in the world, improving dramatically MTOW and payload.
Short RunwaysTake-Off Performance (RTO 100%)
IMPROVING ATR 72-600 TAKE-OFF FROM 900 m (2,953 ft) RUNWAYThrough Take-Off with full RTO procedure
RTO: Reserve Take-Off
MTOW: +1,000 kg (2,200 lb)
ATR -600 SERIES•9
EXPANDING OPERATIONAL VERSATILITY
The ATR cabin is simply the best in providing pas-sengers and Operators with what they expect.
New technological inno-vations are being incor-porated to further enhan-ce the feeling of space, comfort and the pleasure of flying with ATR.
Pleasing People
10 •ATR -600 SERIES
ATR -600 SERIES•11
EnhancingComfort & Appeal
MatchingPassengerExpectations
ATR benefits from the widest cabin in the turboprop market, providing maximum passenger space and setting high standards of
comfort.New style interiors offer more baggage room and fee-ling of space.
The new smooth, soft lines of the ceiling and cabin side panels, re-shaped and re-designed to offer passengers more space and light, create an harmonious and balan-ced environment where traveling is a pleasure.
ENHANCING COMFORT AND APPEAL
The ‘Elegance’ Cabin
Restyled Environment and Modern InteriorsThese changes are included in a new cabin harmony definition, called “Elegance”, already selected by many ATR Operators.
To satisfy the most demanding airline and passenger expectations, new type seats are offered, modern styled and light weight concept, combined with outstanding low maintenance features, meeting the latest requirements of cost conscious airlines.
THE RIGHT COMBINA-TION OF:
Low heat
Low failure rate
Low maintenance
Low weight & volume
Low power
No radio emissions
WITH:
High efficiency
High reliability
Much longer life
Anew cabin styling with totally renewed
commercial furnishing specification is available on ATR models in order to provide Customers with enhanced comfort, space and appeal.
LED LightingCabin lighting based on LED technology for warmer and more agreeable atmosphere with soft and diffused lighting.
LED: Light-Emitting Diodes
12 •ATR -600 SERIES
ENHANCING COMFORT AND APPEAL
ATR -600 SERIES•13
In-Flight Entertainment (IFE)System
MAIN FEATURES
Integrated in PSU
5’’ screen
Up to 18 screens in basic configuration
Motorised
Low weights
Low maintenance
To respond to market needs and evolving requirements coming from passengers and operators, ATR is now offering an IFE system for a
more attractive passenger cabin.
ATR -600 SERIES•13
ENHANCING COMFORT AND APPEAL
14 •ATR -600 SERIES
Never-Ending Innovation
The aviation industry is at the forefront of advanced and innovative technology.Continuous evolution and improvement of pro-
ducts and services have always been decisive to main-tain airlines competitiveness. Today, increasingly demanding technical and safety legislation and Air Traffic Control requirements make adaptability and flexibility more important than ever.
14 •ATR -600 SERIES
ATR -600 SERIES•15
With the future in mind, airlines prefer to avoid the necessity to incur high cost of investing in upgrades and modifications in order to
meet evolving standards. Regional aircraft today must exceed current technical, safety and maintenance requirements.Flight safety and aircraft maintenance optimisation are two of the major requirements coming from Operators and Airworthiness Authorities.
In the wake of this evolution, ATR is now offering signifi-cant product upgrades and innovative solutions.
Leadership is not only market share, but mainly tech-nology at the service of low operating cost and high reliability.
Technology Development
NEW PRODUCTS UPGRADES
Multi-Purpose Computer (MPC)
ACARS
Paperless cockpit (EFB)
Integrated Aircraft Centralized Maintenance System (ACMS)
New Avionics Suite with Glass Cockpit
TECHNOLOGY DEVELOPMENT
16 •ATR -600 SERIES
MPC FEATURES
1 single computer for :
APM (Aircraft Performance Monitoring) providingcrew awareness of in-flight aircraft behaviour
EHS (Enhanced Surveillance) required by March 2007, for aircraft parameters acquisition and transfer to transponders
ADS-B (Auto Dependent Surveillance - Broadcast) foraircraft parameters acquisition and transfer to trans-ponders
Aircraft Centralised Maintenance System
QAR (Quick Access Recorder) allows to record FDR parameters on a PCMCIA card
G-Meter records flight and landing vertical accelera-tions without FDR reading
Maintenance/BITE monitoring availability of BITE messages in the cockpit; provides recommendations in plain text
ACMS (Aircraft Conditions Monitoring System) for aircraft parameters analysis for troubleshooting purpose
FDEP (Flight Data Entry and Printout) simulation (FDAU interface) plain text FDEP page in Computer Display
Engine Parameters Processing and Downloading[under development]
Performancemonitoring
Maintenance
MPC: 1 single computer for all functionalities
Multi-Purpose Computer(MPC)
The innovative concept for system equipment monitoring
Upgradeable solution for flight safety and aircraft maintenance optimization
Compliant with both current and foreseable future airworthiness regulations
16 •ATR -600 SERIES
TECHNOLOGY DEVELOPMENT
Multi-Purpose Computer - APM
APM - Aircraft Performance Monitoring This system is unique in the aviation industry, with the
benefits of enhancing aircraft safety and protection, acting on crew awareness:
Real time acquisition of flight data and aircraft para-meters
Computation of theoretical performance according to flight conditions
Comparison between actual and theoretical perfor-mance (weight, speeds, …)
If discrepancy, alert and warning are delivered to crew
Gives evidence to the crew of « severe ice »effect on the aircraft performance
Alerts the crew about compliance with the minimum required IAS (Indicating Air Speed)
Shows evidence of external conditions encountered as proof of compliance of timely procedure application
Draws pilot’s attention Indicates minimum speed Helps pilot to justify
Record all alerts in FDR
Refer to existing proce-dures after a ‘Degraded performance’
Increasing pilot situa-tion awareness, safety
enhancement through real time acquisition and trend monitoring of aircraft parameters and computation of Minimum Speed according to air-craft configuration.
APM
The Man/Machine Inter-face Concept
Three significant indicators placed in front of the pilot and the co-pilot display this information in the following way:
ATR -600 SERIES•17
Cruise Speed Low
The indicator illumina-tes when cruise IAS1 is lower than the expec-ted value
Degraded performance
During climb, cruise and descent, it alerts the crew that:
• Performance is being degraded
• QRH2 procedures must be applied
Increase Speed
The indicator flashes as soon as minimum icing speed is reached and the aircraft speed has to be increased.
1 - IAS: Indicated Air Speed2 - QRH: Quick Reference Handbook
TECHNOLOGY DEVELOPMENT
Multi-Purpose ComputerOther Features
EHS - Enhanced SurveillanceWHY?
European regulation for down-linking aircraft para-meters:• Roll angle • Selected attitude • Vertical rate • True air speed • Indicated airspeed • True track angle • Ground speed • Magnetic heading, for Air Traffic Control purposes
Required by March 31th 2007 (TGL 18 NPA 20-12a)
HOW?
The MPC acquires, formats and sends parameters required by the ATC to the transponders.
Note: Transponder -007 required (standard fit in production)
Air DataComputers
GNSS
ATC - 007TranspondersAFCS MPC
EHS Architecture
ADS-B- Automatic DependentSurveillance - BroadcastWHY?
To make aircraft data available to other ADS-B capable aircraft and ATC centers
To improve aircraft situational awareness and knowledge
ULTIMATELY …
To enhance ATC sur-veillance currently pro-vided by radars
To replace primary/secondary groundradars
Note: No firm certification basis available today; on-going experimentation.
HOW?
MPC acquires, formats and sends required parameters to trans-ponders
Note: Transponders to be upgraded to -108
FDEPReplacement
WHY?
-ne Interface
HOW?
FDEP is removed
MCDU has a FDEP pagein plain text
INIT TIME & FLIGHT
HOUR:MINUTE09:40
MONTH:DAY12:20
YEAR2005
FLIGHT NUMBER0004
<RETURN PRINT*
GPS
Aircraft ‘see’ each other
Air Traffic ControlGround Station
Principle of ADB-S function
18 •ATR -600 SERIES
TECHNOLOGY DEVELOPMENT
Maintenance/BITEWHY?
To make available BITE data reading and/or analysis tools in the cockpit
To give recommenda-tions in plain text
HOW?
Get access to existing BITE data in the rele-vant computers
Read BITE messages through a MCDU BITE page
MAINTENANCE
<AFCS VERSION>
<RAD COM/NAV
<PEC/EEC
<TCAS
<MFC
<RETURN PRINT*
ACMS - Aircraft Condition Monitoring System
WHY?
Addition of more func-tions specified by ATR or operators mainte-nance staff
Capable of doing com-plementary aircraft parameters analysis
HOW?
Use of acquired para-meters
Use of a ground station (for customization by operator)
QAR - Quick Access RecorderWHY?
Operators request to carry out specific flight analyses
HOW?
Recording of all Flight Data Recorder (FDR) parameters on a PCM-CIA card
MPC delivered with a 256-Mb card
May store up to 1Gb i.e. • more than 2,200 flight hours in 64 words per second (wps) FDR • or more than 500 FH with a 256 wps FDR
G-MeterWHY?
To be able to read aircraft flight and max landing verti-cal accelerations, without Flight Data Recorder reading
To avoid a lengthy immobilization of the aircraft by
making a FDR analysis
HOW?
Access and reading through an MCDU1 G-Meter page
Storage of max vertical acceleration in the PCMCIA card
G-METER REPORT
DATE GMT FLTFEB20 1603 ATR001
GMT ACC1505 01.55 FLT1455 01.20 FLT1515 01.71 GNDVERT ACC : VALIDLONG ACC : VALIDLAT ACC : VALID
<RETURN PRINT*
Aircraft Flight Manual
Weight
Acceleration
2.4
2.6
2.8
3.0
3.2
12000 14000 16000 18000 20000
Hardlanding Zone
Normallanding Zone
Aircraft Flight Manual
Weight
Acceleration
2.4
2.6
2.8
3.0
3.2
12000 14000 16000 18000 20000
Hardlanding zone
Normallanding zone
1 - MCDU: Multi-functional Control Display Unit
MPC - Multi-Purpose ComputerMain Operators Benefits
One single computer able to manage various functionalitiesAll available for retrofit
Improve Crew Situa-tional Awareness and Knowledge
Improve knowledge of both internal and exter-nal environmentsAlert crew about aircraft performance degradationEnhance traffic mana-gement and improve safety
Optimized SolutionCombination of diffe-rent functions into one evolving unitAllows to add new functions without a complete new equip-ment
Effective MaintenanceMaintenance informa-tion centralized and directly available on a single displayMore accurate diagno-ses and recommenda-tionsAnticipate maintenan-ce tasks
Detection of maximum ITT at take-off
Divergence Detection
ACMS
Customised detection& recording
Limits exceedence detection
Cycle Counting
Trend Monitoring
ACMS Capabilities
ATR -600 SERIES•19
TECHNOLOGY DEVELOPMENT
20 •ATR -600 SERIES
CMS main page
Flight report
Ground report
This system can offer additional functionalities, for example:
On-line Troubleshooting Aid, through:
• Interrogating on line the ATR TS data bank
• Selecting the most probable scenario
• Identifying suspect LRU1
• Validating customer experience.
1: LRU: Line Replaceable Unit
It is based on the Air-craft Condition Moni-toring System (ACMS) function of MPC, and on the current functions of the Multi Function Com-puter (MFC), allowing failure source identifica-tion. It does not require additional equipment, but only a software evo-lution.
Engine parameters exceedance available without Flight Data Recorder (FDR) reading
Data access and rea-ding through dedicated MPC function
PCMCIA card storage report
Report files availa-ble for download via VHF network through ACARS
OPERATORS BENEFITS
Will replace or integrate DMT tool for creating data directly usable for ECTM reports
No aircraft hardware utilisation
Engine files erected on PCMCIA card and/or will be downloadable with ACARS.
Engine Parameters Processing & Downloading
ACARS Link
EngineControl Trend Monitoring(ECTM)
Access and reading through an MCDU(MaintenanceControl Display Unit) dedicated page
Storage of exceedancereport in the PCMCIA card
FDAU
Multi-Purpose ComputerOther Features
Flight Data Acquisi-tion Unit (FDAU) data accessed through MPC to create :
Engine reports for trend monitoring
Reading engine para-meters exceedance report, avoiding a lengthly immobiliza-tion of the aircraft, by making a FDR analysis.
Integrated ACMS (Aircraft Centralized Maintenance System)
OPERATORS BENEFITSAutomatic Pilot Flight Report• In flight/on ground data link when combi-ned with ACARSImproved Maintenance• Reliable system moni-toring
• Effective troubleshoo-tingImproved Dispatcha-bility• Faulty LRU1 identifica-tion• Minimum Equipment List (MEL) management
20 •ATR -600 SERIES
TECHNOLOGY DEVELOPMENT
MESSAGE TYPES Position reportingATIS reportPre-departure clea-rancePassenger serviceTake-off dataEmergency reportDelay reportFuel statusEngines report
ACARS - Aircraft Communications Addressing & Reporting System
Up/down-loading digital data via VHF network
Customisable with dedicated tools
Improved communication between aircraft, Opera-tor’s base and ATC (Air Traffic Control)
EFB FEATURES
Checklists
Aircraft manuals
Electronic charts
Performance calcula-tions
Customer dedicated application
EFB - Electronic Flight BagProvides flight crew with a paperless cockpit, replacing the current paper-based documentation
Integration in the cockpit
Pilots will have at their fingertips moving maps, graphical weather fore-casts, terrain mapping and a variety of aviation data and functions.
A multi-function tool for the modern cockpit
ATR -600 SERIES•21
OPERATORS BENEFITS
Faster and more accurate information flowEnhanced flight safetyIncreased operational efficiencyImproved passenger serviceReduced crew workloadReduced maintenance and operating costs
TECHNOLOGY DEVELOPMENT
The ATR avionics have been improved and
developed during recent years essentially to face required regulatory evolutions, in connection with new required functionalities:
FM immunity, 8.33 KHz radio, B-RNAV, ACAS, TAWS
HF, ACARS, …
Regional air transport’s dramatic evolution and continuous require-ments for advanced state-of-the-art tech-nology turboprops, are now the drivers for further ATR avionics upgrading.
The new avionics suite will modify significantly the display of the main information and data required by the pilot to achieve his main tasks: operate, navigate and manage.
This will simplify the cockpit dramatically and allows pilots to focus only on the most perti-nent information.
All these changes will improve situational awa-reness and customise the man-machine inter-face to enhance safety.
ATR -600 Series: New Avionics Suite
Simplified, integrated LCD advanced functions will enhance safety, reliability, handling for pilots, while contributing to mainte-nance cost savings and weight reduction.
The major design objective of new ATR avionics’ suite is to provide the crew with the most realistic picture of the in-flight situation and the most comprehensive displays of the aircraft systems, in addition to ensuring growth for future navigation needs and communication means by the end of the decade.
The cockpit will be designed in order to replace most of the present instruments by five 6” x 8” LCD displays composed of:
2 Primary Flight Displays (PFD),2 Multi-Function Displays (MFD),1 Engine & Warning Display (EWD)
Virtu
al v
iew
-com
pute
r gen
erat
ed
ATR -600 Series will be also capable of Category IIIA approach (landing with a decision height of 50ft), in addition to GPS capability for Non-Precision Approach 0.3Nm.
22 •ATR -600 SERIES
TECHNOLOGY DEVELOPMENT
ATR -600 SERIES•23
General System Architecture
23 •ATR -600 SERIES
The new technology available on ATR -600 Series aircraft
features advanced solutions and superior performance compared to previous generation Glass Cockpit.These may be recogni-zed in all operational domains:
Improved Operation and Situational Awareness
Improved Dispatch Capability
RNP 0.3 ready with path for lower RNP
Enhanced Crew Alert System
Paper-Less cockpit with procedures and system page management
Basic WAAS capability
All weather operation with 50 ft decision height (Cat IIIA Operation)
Improved situational awareness and safety
• Navigation Charts display with A/C position
• Provision for Vertical Situation Display with terrain profile
• Provision for ADS-B with CDTI for full traffic aware-ness
Operations and Situa-tional Awareness
Maintenance
Performance
Technology
ATR -600 SERIES•23
TECHNOLOGY DEVELOPMENT
24 •ATR -600 SERIES
EasierMaintenance
On-Wing SW and Database high-speed upload via standard Data-loader (A429/Ethernet) or Flashcard
Centralized Main-tenance with Plain English fault report
Raw Maintenance data displayed on MFD
Engine Run Up pages
Aircraft Configura-tion management via software pin-prog to manage options
Enhanced BITE ope-ration thanks to latest THALES development on recent programs
Maintenance opera-tion (BITE read out) possible on failed Core Avionics Modules
No reset required to retrieve data allowing improved isolation and identification of failed item thus reducing NFF and allowing product future improvement
Reset of one embedded application without resetting the HW module on CAC
ATR -600 SERIES•24
Better Performance
30% Weight savings compared to current ATR
Reduced volume and heat dissipation
Reduced LRU count compared with current ATR version
30% Lower P/N count
Improved MTBF
Growth Capability
Ultimate Technology Latest Integrated Modular Avionics Technology
• Certified on A380 program
• Offering Flexibility and growth capability
Latest AMLCD 6" x 8" displays
• Led Array backlighting: Reduced power consump-tion, Improved View angles up to 55° horizontal
• Improved resolution: 1024 x 768
• Embedded Mass memory for Jeppesen, FMS data-base
• Video capable (up to three inputs)
• Processing and Graphic power: FMS, Airport Nav all embedded in DU
Flight Deck Architecture
Two Primary Flight Displays (PFD) for EFIS functions (EADI/EHSI)
Two Multi-Function Displays (MFD) for Navigation and aircraft system synoptic
One Engine & Warning Display (EWD) for Engine Instruments and Crew Alerting System, Check-lists/Proceduresmanagement and permanent data
Control panels for system settings
24 •ATR -600 SERIES
Superior performance compared to previous generation Glass Cockpit
TECHNOLOGY DEVELOPMENT
ATR -600 SERIES•25
2 Primary Flight Displays - PFD
PFD’s integrate multiple conventional instruments:
EADI on top
• Digital ASI• Radio altitude• Lateral & vertical deviation
• FD guidance
EHSI on bottom
• Bearing pointers
• TAWS or WSR data
Rolling Air Speed Indi-cator with speed bugs
• V-speeds• Low and over speeds• Speed trend• Managed/selectedspeeds• Rolling barometric alti-tude display
Vertical speed
Flight mode, icing conditions annuncia-tions
2 Multi-Function Displays - MFD
MFD’s integrate multiple sensors:
Navigation display
• Actual & selected heading• Bearing pointers• FMS data• Navaids• TAWS or WXR image
• TCAS data
System and utilities pages
• Cabin• Electric• Hydraulic• Engine
Video (optional)
Memo panel
Radio management
Engine & Warning Display - EWD
Primary engine para-meters
• Flight controls posi-tion indication• Trim
• Flaps
Crew Alerting Panel
Emergency, Normal and Abnormal proce-dure display
Permanent data (TAT, SAT, Gross Weight, Fuel on board…)
Five 6" x 8" LCD Units
TECHNOLOGY DEVELOPMENT
26 •ATR -600 SERIES
Centralized Audio Management System (example)
26 •ATR -600 SERIES
Growth and options capabilityOptional CAT IIIa autopi-lot is available allowing ILS auto-land with aDecision Height of 50 feet and VR 200m
GPS capability for Non-Precision Approach 0.3Nm.
Provisions included in the basic architecturewill permit to developfurther optional capabili-ties such as:
• ADS-B «in» with Cock-pit Display of TrafficInformation: Allows to display surrounding aircraft information for improved traffic situatio-nal awareness
• Upgrade to provide
with lower RNP minima capability if required.(I.e. RNP AR APPCH < 0.3 Nm)
• Vertical Situation Dis-play: Terrain and Air-craft Vertical Situation display on MFD
• Airport Navigation Function: Aircraft ground navigation aidsand guidance.
• Coupled VNAV : Cruisealtitude and steps mana-gement, Vertical devia-tion computation
O F FFAULT
O F FFAULT
A R MO F F
EEC 1 ATPCS EEC 2HYD
ANTI SKIDOFF
FAULT
0 5 0 0
HIGHDUMP
AUTO PRESS
T OMCT
CRZCLB
PWR MGT O F FFAULT
O F FFAULT
PEC 1 PEC 2
TRIM1 ADC 2
O NFAULTMAN
CAB PRESSDITCH
UNLK UNLKUNLK
10
20
10
20
5
5
I S I S
TEST
PUSHEROFF
FAULT
WATCH
E N G 2 F I R E
B R A K E S H O T
D O O R S-------------
-. . .
ANTI-SKID TESF F
C A B A L T5 2 3 0 F T
3 .3 P S I
D P
4 5 0 F T / M N
V S
P A XD O O R
48 °C
37 °C
22 °C
21 °C
SMOKE
1 1 2 1 0 9
F USED K GF USED K G
120 P S I
O 2
CRZ
6 1 .3 1 0 9 .3T Q %
N P %
I T T °C5 4 3 8 4 3
F I R E 2
LO PITCH
E E C
P E CSGL CHL
UPTRIMATPCS
1 0 1 .38 1 . 9
ANTI-ICINGDE-ICINGFUEL XFRPRK BK ONPROPBKON
NO SMKGSEAT BLT
RMU1
SBY RMI
I C I N GICINGA O A
TEST
RMU2
SBY RMI
O F FFAULT
O F FFAULT
A R MO F F
EEC 1 ATPCS EEC 2O F FFAULT
O F FFAULT
A R MO F F
O F FFAULT
O F FFAULT
A R MO F F
EEC 1 ATPCS EEC 2HYDHYD
ANTI SKIDOFF
FAULT
0 5 0 0
HIGHDUMP
AUTO PRESS0 5 0 0
HIGHDUMP
AUTO PRESS
T OMCT
CRZCLB
PWR MGT O F FFAULT
O F FFAULT
PEC 1 PEC 2O F F
FAULTO F F
FAULTO F F
FAULTO F F
FAULT
PEC 1 PEC 2
TRIMTRIM1 ADC 21 ADC 2
O NFAULTMAN
CAB PRESSDITCH
O NFAULTMANO NFAULTMAN
CAB PRESSDITCH
UNLK UNLKUNLK UNLK UNLKUNLK
10
20
10
20
5
5
I S I S 10
20
10
20
5
5
I S I S 10
20
10
20
5
5
10
20
10
20
5
5
10
20
10
20
5
5
I S I S
TEST
PUSHEROFF
FAULT
PUSHEROFF
FAULT
PUSHEROFF
FAULT
WATCHWATCH
E N G 2 F I R E
B R A K E S H O T
D O O R S-------------
-. . .
ANTI-SKID TESF F
C A B A L T5 2 3 0 F T
3 .3 P S I
D P
4 5 0 F T / M N
V S
P A XD O O R
48 °C
37 °C
22 °C
21 °C
SMOKE
1 1 2 1 0 9
F USED K GF USED K G
120 P S I
O 2
CRZ
6 1 .3 1 0 9 .3T Q %
N P %
I T T °C5 4 3 8 4 3
F I R E 2
LO PITCH
E E C
P E CSGL CHL
UPTRIMATPCS
1 0 1 .38 1 . 9
ANTI-ICINGDE-ICINGFUEL XFRPRK BK ONPROPBKON
NO SMKGSEAT BLTE N G 2 F I R E
B R A K E S H O T
D O O R S-------------
-. . .
ANTI-SKID TESF F
C A B A L T5 2 3 0 F T
3 .3 P S I
D P
3 .3 P S I
D P
4 5 0 F T / M N
V S
4 5 0 F T / M N
V S
P A XD O O R
48 °C
37 °C
22 °C
21 °C
SMOKE
P A XD O O R
48 °C
37 °C
22 °C
21 °C
SMOKE
1 1 2 1 0 9
F USED K GF USED K G
1 1 2 1 0 9
F USED K GF USED K G
120 P S I
O 2
120 P S I120 P S I
O 2
CRZ
6 1 .3 1 0 9 .3T Q %
N P %
I T T °C5 4 35 4 3 8 4 38 4 3
F I R E 2
LO PITCH
E E C
P E CSGL CHL
UPTRIMATPCS
1 0 1 .38 1 . 9
ANTI-ICINGDE-ICINGFUEL XFRPRK BK ONPROPBKON
NO SMKGSEAT BLT
RMU1
SBY RMI
RMU1
SBY RMI
I C I N GICINGA O A
I C I N GICINGA O A
TESTTEST
RMU2
SBY RMI
RMU2
SBY RMI
TECHNOLOGY DEVELOPMENT
ATR -600 SERIES•27
Glossary
ACAS: Aircraft Collision Alerting System
ADS-B: Automatic Depen-dent Surveillance - Broa-dcast
ASI: Air Speed Indicator
CDTI: Cockpit Display of Traffic Information
DME: Distance Measuring Equipment
EADI: Electronic Attitude Director Indicator
EGPWS: Enhanced Ground Proximity Warning System (or TAWS, OACI designa-tion)
EHSI: Electronic Horizontal Situation Indicator
MTBF: Meantime Between Failure
NFF: No Fault Found
RMI: Radio Magnetic Indi-cator
RNP: Required Navigation Procedure
TAWS: terrain Awareness and Warning System
TCAS: Traffic Collision Avoidance System (or ACAS, OACI designation)
VSI/TRA: Vertical Speed Indicator/Traffic Resolution Advisory
WAAS: Wide Area Aug-mentation System
WSR: Weather Surveillan-ce Radar
WXR: Weather X-Ray
ATR -600 Series Never Ending Innovations
TECHNOLOGY DEVELOPMENT
28 •ATR -600 SERIES
ATR DC/E Marketing February 2008 - The information contained in this document are presented in good faith and do not in any way constitute an offer or a warranty. Issue 0.9
Avions de Transport Régional - 1, allée Pierre Nadot - 31712 Blagnac Cedex - France Phone +33 (0)5 62 21 62 21http://www.atraircraft.com