Memory Items Flashcards
Aborted Engine Start
1) Engine start lever (affected engine) . . . . CUTOFF
Airspeed Unreliable
1) Autopilot (if engaged) . . . .Disengage
2) Autothrottle (if engaged) . . . . . Disengage
3) F/D switches (both) . . . . OFF
4) Set the following pitch and thrust:
Flaps extended . . . . 10 deg and 80% N1
Flaps retracted . . . . 4 deg and 75% N1
APU Fire
1) APU Fire switch . . . Confirm . . . Pull, rotate to the stop, and hold for 1 second
2) APU switch . . . . OFF
Cabin Altitude Warning
or
Rapid Depressurization
1) Don oxygen masks and set regulators to 100%
2) Establish crew communications
3) Pressurization mode selector . . . . MAN
4) Outflow VALVE switch . . . . Hold in CLOSE until the outflow VALVE indication shows fully closed
5) IF cabin altitude remains uncontrollable:
Passenger signs . . . . ON
PASS OXYGEN switch . . . . ON
-> Go to the Emergency Descent checklist on page 0.1
Elevator Tab Limit Cycle Oscillation
1) Airspeed. . . . Reduce to 270 KIAS or until the vibration ceases, whichever is lower
2) Do not use speedbrakes or change aircraft configuration to reduce airspeed
Emergency Descent
1) Announce the emergency descent. The pilot flying will advise the cabin crew of the 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
Note: If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads
7) Set target speed to Mmo/Vmo
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
5) IF the engine fire switch or ENG OVERHEAT light is still 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
ENGINE OVERHEAT
1) Autothrottle (if engaged) . . . . Disengage
2) Thrust lever (affected engine) . . . Confirm. . . Close
3) IF the ENG OVERHEAT light STAYS ILLUMINATED:
Go to Engine Fire checklist on page 8.2
Engine Limit or Surge or Stall
1) Autothrottle (if engaged) . . . . Disengage
2) Thrust lever (affected engine) . . . Confirm. . . Retard until engine indications stay within limits or the thrust lever is closed
LANDING CONFIGURATION
1) Assure correct airplane landing configuration
TAKEOFF CONFIGURATION
1) Assure correct airplane takeoff configuration
Loss Of Thrust On Both Engines
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 a redline or there is no increase in EGT for 30 seconds:
Engine start lever (affected engine) . . . Confirm . . . CUTOFF, then IDLE detent
IF EGT again reaches a redline or there is no increase in EGT within 30 seconds, repeat as needed.
Runaway Stabalizer
1) Control column . . . . Hold firmly
2) Autopilot (if engaged) . . . . Disengage
DO NOT reengage the Autopilot. Control airplane attitude manually with control column and main electric trim as needed.
3) Autothrottle (if engaged) . . . . Disengage
DO NOT reengage the autothrottle
4) IF the runaway STOPS after the autopilot is disengaged:
••••
5) IF the runaway CONTINUES after the autopilot is disengaged:
STAB TRIM CUTOUT switches (both) . . . . CUTOUT
IF the runaway continues:
Stabilizer trim wheel . . . . Grasp and hold