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30 Cards in this Set
- Front
- Back
Aborted Engine Start
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7.1
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Aborted Engine Start
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1 Engine start lever (affected engine) . . . . CUTOFF
- - - - - - - - - - - - - - - - - - - - - - - |
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Airspeed Unreliable
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10.1
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Airspeed Unreliable
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1 Adjust the airplane attitude and thrust. Maintain
airplane control. 2 PITOT STATIC HEAT switches . . . . . . . . Check ON 3 Cross check the MACH/AIRSPEED indicators. - - - - - - - - - - - - - - - - - - - - - - - |
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APU FIRE
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8.1
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APU FIRE
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1 APU fire switch. . . Confirm . . . .Pull, rotate to the
stop, and hold for 1 second 2 APU switch . . . . . . . . . . . . . . . . . . . . . . . . OFF |
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CABIN ALTITUDE WARNING or
Rapid Depressurization |
2.1
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CABIN ALTITUDE WARNING or
Rapid Depressurization |
1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications. 3 Pressurization mode selector . . . . . .MAN AC/MAN 4 Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until outflow VALVE indicates fully closed 5 If cabin altitude is not controllable: Passenger signs . . . . . . . . . . . . . . . . . . . .ON If the cabin altitude exceeds or is expected to exceed 14,000 feet: PASS OXYGEN switch . . . . . . . . . . . .ON |
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Emergency Descent
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0.1
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Emergency Descent
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1 Announce the emergency descent. The pilot flying
will advise the cabin crew, on the PA system, of impending rapid descent. The pilot monitoring will advise ATC and obtain the area altimeter setting. 2 Passenger signs . . . . . . . . . . . . . . . . . . . . . .ON 3 Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher. 4 ENGINE START switches (both) . . . . . . . . . CONT 5 Thrust levers (both) . . . . . . . . . Reduce thrust to minimum or as needed for anti-ice 6 Speedbrake . . . . . . . . . . . . . . . .FLIGHT DETENT - - - - - - - - - - - - - - - - - - - - - - - |
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ENGINE FIRE
or Engine Severe Damage or Separation |
8.2
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ENGINE FIRE
or Engine Severe Damage or Separation |
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
2 Thrust lever (affected engine) . . . . . . . .Confirm . . . . . Close 3 Engine start lever (affected engine) . . . . . . . .Confirm . . . CUTOFF 4 Engine fire switch (affected engine) . . . . . . . .Confirm . . . . . . Pull To manually unlock the engine fire switch, press the override and pull. 5 If the engine fire switch or ENG OVERHEAT light stays illuminated: Engine fire switch . . . . . Rotate to the stop and hold for 1 second If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated: Engine fire switch. . . . . . . .Rotate to the other stop and hold for 1 second - - - - - - - - - - - - - - - - - - - - - - - |
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Engine Limit or Surge or Stall
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7.2
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Engine Limit or Surge or Stall
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1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
2 Thrust lever (affected engine) . . . . Confirm. . . . .Retard until indications stay within limits or the thrust lever is closed - - - - - - - - - - - - - - - - - - - - - - - |
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ENGINE OVERHEAT
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8.4
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ENGINE OVERHEAT
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1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
2 Thrust lever (affected engine) . . . . . . . .Confirm . . . . . Close 3 If the ENG OVERHEAT light stays illuminated: |
|
ENGINE FIRE
or Engine Severe Damage or Separation |
8.2
|
|
ENGINE FIRE
or Engine Severe Damage or Separation |
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
2 Thrust lever (affected engine) . . . . . . . .Confirm . . . . . Close 3 Engine start lever (affected engine) . . . . . . . .Confirm . . . CUTOFF 4 Engine fire switch (affected engine) . . . . . . . .Confirm . . . . . . Pull To manually unlock the engine fire switch, press the override and pull. 5 If the engine fire switch or ENG OVERHEAT light stays illuminated: Engine fire switch . . . . . Rotate to the stop and hold for 1 second If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated: Engine fire switch. . . . . . . .Rotate to the other stop and hold for 1 second - - - - - - - - - - - - - - - - - - - - - - - |
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Engine Tailpipe Fire
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8.6
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Engine Tailpipe Fire
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1 Engine start lever
(affected engine) . . . . . . . . . . . . . . . . . CUTOFF 2 Advise the cabin. 3 Choose one: 4 PACK switches (both) . . . . . . . . . . . . . . . . . OFF 5 ISOLATION VALVE switch. . . . . . . . . . . . . . AUTO 6 Engine BLEED air switches (both) . . . . . . . . . .ON 7 Choose one: |
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Evacuation
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Back Cover.2
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Evacuation
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1 PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . Set
2 Speedbrake lever . . . . . . . . . . . . . . . . . . DOWN 3 FLAP lever . . . . . . . . . . . . . . . . . . . . . . . . . . 40 4 STANDBY POWER switch . . . . . . . . . . . . . . . BAT 5 Pressurization mode selector . . . . . . . . . MAN DC 6 Outflow VALVE switch . . . . Hold in OPEN until the outflow VALVE position indicates fully open 7 If time allows: Verify that the flaps are 40 before the engine start levers are moved to CUTOFF. 8 Engine start levers (both) . . . . . . . . . . . CUTOFF 9 Advise the cabin to evacuate. 10 Advise the tower. 11 Engine and APU fire switches (all) . . . . . . . . . . .Override and pull 12 If an engine or APU fire warning occurs: Illuminated fire switch. . . . . Rotate to the stop and hold for 1 second |
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Loss Of Thrust On Both Engines
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7.6
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Loss Of Thrust On Both Engines
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1 ENGINE START switches (both) . . . . . . . . . . FLT
2 Engine start levers (both) . . . . . . . . . . . CUTOFF 3 When EGT decreases: Engine start levers (both) . . . . . . IDLE detent 4 If EGT reaches 930°C or there is no increase in EGT within 30 seconds: Engine start lever (affected engine) . . . . Confirm . . . . . CUTOFF, then IDLE detent If EGT again reaches 930°C or there is no increase in EGT within 30 seconds, repeat as needed. - - - - - - - - - - - - - - - - - - - - - - - |
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Overspeed
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15.1
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Overspeed
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1 Reduce thrust and, if needed, adjust attitude to
reduce airspeed to less than Vmo/Mmo. - - - - - - - - - - - - - - - - - - - - - - - |
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Rapid Depressurization
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2.1
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Rapid Depressurization
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1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications. 3 Pressurization mode selector . . . . . .MAN AC/MAN 4 Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until outflow VALVE indicates fully closed 5 If cabin altitude is not controllable: Passenger signs . . . . . . . . . . . . . . . . . . . .ON If the cabin altitude exceeds or is expected to exceed 14,000 feet: PASS OXYGEN switch . . . . . . . . . . . .ON |
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Runaway Stabilizer
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9.1
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Runaway Stabilizer
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1 Control column. . . . . . . . . . . . . . . . . Hold firmly
2 Autopilot (if engaged) . . . . . . . . . . . . .Disengage Do not re-engage the autopilot. Control airplane pitch attitude manually with control column and main electric trim as needed. 3 If the runaway stops: |