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9 Cards in this Set
- Front
- Back
SYSTEM A
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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 |
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SYSTEM B
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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 |
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MINIMUM FUEL FOR GROUND OPERATION OF ELECTRIC MOTOR DRIVEN PUMPS IS
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760 KGS IN THE RELATED MAIN TANK
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STANDBY SYSTEM USES A SINGLE ELECTRIC MOTOR DRIVEN PUMP TO POWER
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THRUST REVERSERS
RUDDER LEADING EDGE FLAPS AND SLATS (EXTEND ONLY) STANDBY YAW DAMPER |
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AUTOMATIC OPERATION OF STANDBY SYSTEM
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LOSS OF SYSTEM A AND B AND
FLAPS EXTENDED AND AIRBORNE OR WHEEL SPEED > 60 KNOTS AND FLIGHT CONTROL SWITCHES A OR B ON |
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POWER TRANSFER UNIT
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AUTOSLATS AND LEADING EDGE FLAPS AND SLATS
SYSTEM B EDP BELOW LIMITS AIRBORNE FLAPS ARE LESS THAN 15 BUT NOT UP |
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LEADING EDGE TRANSFER UNIT
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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 |
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RF ILLUMINATED WHITE
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HYDRAULIC QUANTITY BELOW 76 %
VALID ONLY WHEN AIRPLANE IS ON GROUND NO ENGINE POWER AFTER LANDING WITH FLAPS UP DURING TAXI IN |
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IF THE NOSE GEAR STEERING LOCKOUT PIN IS NOT INSTALLED
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SYSTEM A HYDRAULIC PUMPS MUST BE TURNED OFF
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