P2P1 P3

P2

S2S1

P1P1

S1S2

P2

SFCC 2

[DC ESSLAND REC]

SFCC 2[DC2]

SFCC 1

[DC2]

SFCC 1[DC ESS SHED

LAND REC]

ELECPUMP[AC1,DC1]

ENG 1ENG2

REV REV

NORM BRK

Gear & doorsselector valves

NOSEWHEEL

STEERINGALTN & PARK BRK

ELEVATOR ACTUATOR MODES- active, electrically controlled- damping, follows surface- centering, hydraulically maintained in neutralonly if 4 jacks are unpowered (both sides)

AILERONS ACTUATOR MODES- active, electrically controlled- damping, follows surfaceROLL DEFLECTION LIMITS- 25° for ailerons- 35° for spoilers

MOT MOT

MOT1[DC ESSSHED]

MOT3[DC2]

MOT2[DC2]

TRIM WHEEL

BSCUCH1 [DC ESS SHEDLAND REC]

CH2 [DC2]BSCU

LGCIU 1[LAND REC]

LGCIU 2[DC2]

NORMAL

=

NORMAL SERVOVALVE

LANDINGSAFETYVALVE

BOGIEPITCH

TRIMMER

ALTERNATESERVOVALVE

DUALVALVE

PARKINGBRAKEVALVE

DUALSHUTTLE

VALVE

LP DISTRIBUTION LINE

NORMALSELECTOR

VALVE

AUTOMATICSELECTOR

SERVOVALVE

G HYD fromnose gear doorsclosing circuit

GRAVITYEXTENSION

CUT OUTVALVE

ACCUELECTRIC PUMPSFlow is ~18% of eng pump, used to retractsurfaces but not to replace the eng pumps.

ELEVATORS

AILERONS / SPOILERS

SLATSFLAPS

LANDING GEAR / NWS

FLIGHT CONTROLS LAWS

HYDRAULICS

BRAKES

STABILIZERTRIM

FLIGHT CONTROL COMPUTERS MAIN STBYPRIM 1 DC ESS HOTPRIM 2 DC2PRIM 3 DC2SEC 1 DC ESS HOTSEC 2 DC2 DC ESSFCDC 1 DC ESS SHEDFCDC 2 DC2BUS in red are available in ELEC EMERconfig with EMER GEN on ENG PUMP

NWS LIMITSSteering hanwheels:max 72° at 14kts, 0° at 100ktsRudder pedals:TO: max 6° at 100kts, 0° at 150ktsLDG: max 6° at 40kts, 0° at 100ktsTowing max 65°Oversteer at 93°

LIMITATIONSNormal pressure 3000 ± 200 psiRAT pressure ~2500 psiFluid SKYDROL LD4RESERVOIR PRESSURIZATIONis achived by HP bleed air fromengine 1 or x-duct bleed

RAT comes automatic out if dual eng fail or G+B lo lvl or G+Y lo lvl

GEAR LIMITSretraction 250kts/.55extension 250kts/.55extended 250/M.55gravity ext 200ktsmax alt ext 21'000ft gear dn flt 255/M.60tire speed 204kts

ACCUdesigned for 7 full brakes application or at least 12 hrs prk brk

AUTOBRAKEmode delay decelLO 1s 1.8m/s2MED 0s 3m/s2MAX max pressureDECEL light illuminates if 80% of rate in LO or MED and if 2.65m/s2 decel in MAX mode

!!! NOT FOR OPERATIONAL USE !!! A330 ©Pierre-Michel Gasser , 26.3.2009

ELEVATOR DEFLECTION LIMITS- 30° nose up- 15° nose down

STABILIZER LIMITS14° nose up2° nose down

P3

S1P1

P2S2

P3

P3

S1 S1

P1

GND SPLR and SPD BRK

S2

P2 WTB P1 P2

S2S1 S2 P3

65

43

21

Maneuver Load AllevationRoll Control

WTB

SF

CC

1

SF

CC

2

WTB

SF

CC

2

SF

CC

1

SF

CC

1

SF

CC

2

WTB

SF

CC

1

SF

CC

2

FLAPSECAM Slats Flaps (ailerons) VFE1 16° 0° (0°) 240kts1+F 16° 8° (5°) 215kts2 RELIEF 20° 8° (10°) 205kts2 20° 14° (10°) 196kts3 RELIEF 23° 14° (10°) 186kts3 (FULL RELIEF) 23° 22° (10°) 186ktsFULL 23° 32° (10°) 180ktsMax altitude with Flaps/Slats extended is 20’000ftSlats ALPHA LOCK if α > 8.5° or IAS < 148ktsT/O with conf 1+F, auto flaps retract at 200kts

ELECPUMP[AC1,DC2]

HANDPUMP

ENG2PUMP

RESERVOIRRESERVOIR

RAT

ACCU CARGODOORS

ENG1PUMP

RESERVOIR

ACCU

ELECPUMP[AC2,DC1]

ENG2PUMP

ENG1PUMP

EMERGEN

GRAVITYEXTENSIONSYS 1 [HOT 1]

SYS 2 [HOT 2]

( IAS<280kts or MLG on GND )

andGear Lever Down

[DC ESS]

PITCHGND

FLT

FLARE

ROLL PROTECTIONSDirect deflection Direct deflection

Roll rate

Load factor +2.5g / -1g cleanLoad factor +2g / 0g not clean= Pitch 30°up / 15°down= Bank 67° / 33° stick neutralSide slip blue if eng failureHigh α, Vα prot, Vα floor, Vα max= High speed VMO+4, bank 0° with stick neutralLow energy warning Flaps 2,3 or FULL 100ft - 2000ft

Direct deflection50ft pitch down order

Load factor demandAuto pitch Trim if lessthan 33° bank

ALTN 1same as Normal

Same as Normal except:X no Pitch & Low energy protHigh α: LOST if VS1g computation failureLow speed, nose down demand 5-10kts > Stall warningHigh speed, light nose up demand, symbol disappears

same as Normal

ALTN 2Roll directSpoiler 2,3 & 6 u/sYaw alternate

Same as Altn 1 except:X no Bank protno Low speed prot if 2 ADR failedno High speedif 3 ADR failed

same as Normal

DIRECT

MECHANICAL BACK-UP

Roll directYaw alternate

No protection exceptOverspeed & Stall warningDirect control

Manual pitch trim only

USE MAN PITCH TRIM

RUDDER ONLYYaw by BYDU MAN PITCH TRIM ONLY

RA<100ft

RA>50ft

BRAKE TEMPERATURE- T/O max 300°C- A332 only: if BRK FAN ON max 150°C, thenswitch brake fan OFF for T/O

Maintenance action required if:- (TEMP difference on same gear > 150°C) and (1 BRK > 600°C or < 60°C)- average diff TEMP L/R > 200°C- a fuse plug has melt- Brake temp > 800°C, tyre deflates at ~800°C

x

x

P3

P1P1S1

P3

P2

S2

S1

MOT1[DC ESSSHED]

ARTFEEL

MOT2[DC2]

ACTUATOR

BYDU

BACKUP YAWDAMPER UNIT

ACTUATOR

S2

S1

S2

S1

RUDDERTRIM

YAW DAMPER

RUDDERPEDALS

MOT1[DC ESS]

MOT2[DC2] S2

S1RUDDERLIMITER

PTLUPedalTravelLimitUnit

RUDDERA333

RUDDER A332

LIMITS85% of

deflectionlimited to 29°

RUDER LIMITS35° < 150kts4° > 350kts

Max deflection 31.6°

ARTFEEL

MOT1

MOT2

ELECGEN

ELECGEN

ELECGEN

ELECGEN

MOT1[DC ESSSHED]

MOT2[DC2]S2

S1

RUDDER TRIMPFTU(Pedal Feel andTrim Unit)

+

BCMBackupControlModule

ACTUATOR

ACTUATOR

ACTUATOR

F/CTL ALTN LAW (PROT LOST)

F/CTL ALTN LAW (PROT LOST)

F/CTL DIRECT LAW (PROT LOST)

A333 with BCM

F/CTL L + R ELEV FAULT

G ELEC PUMP runs 25’ if ENG 1 (2) FAILand GEAR selected up and speed>100kts

Y ELEC PUMP runs if ENG 2 FAIL and FLAPS not 0° and G elec pmp not running

A333: B ELEC PUMP runs if ENG 1 FAIL and F/CTL PRIM 1 (3) FAULT to ensure sufficient authority on electrical rudder

A332/A333