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9 Cards in this Set

  • Front
  • Back
SYSTEM A
AILERONS RUDDER ELEVATOR AND ELEVATOR FEEL
FLIGHT SPOILERS
GROUND SPOILERS
ALTERNATE BRAKES
NO 1 THRUST REVERSER
AUTOPILOT A
NOSE WHEEL STEERING
LANDING GEAR
POWER TRANSFER UNIT
SYSTEM B
AILERONS RUDDER ELEVATOR AND ELEVATOR FEEL
FLIGHT SPOILERS
LEADING EDGE FLAPS AND SLATS
BRAKES
NO 2 THRUST REVERSER
AUTOPILOT B
LANDING GEAR TRANSFER UNIT
ALTERNATE NOSE WHEEL STEERING
AUTOSLATS
YAW DAMPER
TRAILING EDGE FLAPS
MINIMUM FUEL FOR GROUND OPERATION OF ELECTRIC MOTOR DRIVEN PUMPS IS
760 KGS IN THE RELATED MAIN TANK
STANDBY SYSTEM USES A SINGLE ELECTRIC MOTOR DRIVEN PUMP TO POWER
THRUST REVERSERS
RUDDER
LEADING EDGE FLAPS AND SLATS (EXTEND ONLY)
STANDBY YAW DAMPER
AUTOMATIC OPERATION OF STANDBY SYSTEM
LOSS OF SYSTEM A AND B AND
FLAPS EXTENDED AND
AIRBORNE OR WHEEL SPEED > 60 KNOTS AND
FLIGHT CONTROL SWITCHES A OR B ON
POWER TRANSFER UNIT
AUTOSLATS AND LEADING EDGE FLAPS AND SLATS

SYSTEM B EDP BELOW LIMITS
AIRBORNE FLAPS ARE LESS THAN 15 BUT NOT UP
LEADING EDGE TRANSFER UNIT
TO RAISE THE LG WHEN SYSTEM A EDP LOST

AIRBORNE
NO 1 ENGINE RPM DROPS BELOW LIMITS
LANDING GEAR LEVER IS POSITIONED UP
EITHER MAIN LANDING GEAR IS NOT UP AND LOCK
RF ILLUMINATED WHITE
HYDRAULIC QUANTITY BELOW 76 %

VALID ONLY WHEN AIRPLANE IS ON GROUND NO ENGINE POWER
AFTER LANDING WITH FLAPS UP DURING TAXI IN
IF THE NOSE GEAR STEERING LOCKOUT PIN IS NOT INSTALLED
SYSTEM A HYDRAULIC PUMPS MUST BE TURNED OFF