Memory Items Flashcards
MEM: Aborted Engine Start
- Engine start lever (affected engine) - CUTOFF
MEM: Airspeed Unreliable
- Autopilot (if engaged) - Disengage
- Autothrottle( if engaged) - Disengage
- F/D switches (both) - OFF
- Set the following gear up pitch attitude and thrust:
Flaps extended - 10º and 80% N1
Flaps up - 4º and 75% N1
MEM: APU FIRE
- APU fire switch - Confirm - Pull, rotate to teh stop and hold for 1 second
- APU switch - OFF
MEM: ENGINE FIRE or Engine Severe Damage or Separation
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Conditions
Condition: One or more of these occur:
- Engine fire warning
- Airframe vibrations with abnormal engine indications
- Engine separation
- Autothrottle (if engaged) - Disengage
- Thrust lever (affected engine) - Confirm - Close
- Engine fire switch (affected engine) - Confirm - CUTOFF
- Engine fire switch (affected engine) - Confirm - Pull
- If the engine fire switch or ENG OVERHEAT light is illuminated:
Engine fire switch - Rotate to the stop and hold for 1 second
If after 30 seconds the hengine fire switch or ENG OVERHEAT light stays illuminated:
Engine fire switch - Rotate to the other stop and hold for 1 second
MEM: ENGINE OVERHEAT
Condition: An overheat is detected in the engine.
- Autothrottle (if engaged) - Disengage
- Thrust lever (affected engine) - Confirm - Close
- If the ENG OVERHEAT light stays illuminated:
>> Go to the ENGINE FIRE or Engine Servere Damage or Seperation checklist on page 8.2
MEM: Engine Limit or Surge or Stall
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Conditions and Objective
Condition: One or more of these occur:
- Engine indications are abnomal
- Engine indications are rapidly approaching or exceeding limits
- Abnormal engine noieses are heard, possibly with airframe vibration
- There is no response to thrust lever movement or the response is abnormal
- Flames in the engine inlet or exhaust are reported
Ojective: To attempt to recover normal engine operation or shut down the engine if recovery is not possible.
- Autothrottle (if engaged) - Disengage
- Thrust lever (affected engine) - Confirm - Retard until engine indications stay within limits or the thrust lever is closed
MEM: LANDING CONFIGURATION
Condition: In flight, the steady warning horn sounds.
- Assure correct airplane landing configuration.
MEM: TAKEOFF CONFIGURATION
Condition: On ground, intermittent warning horn sounds and/or a TAKEOFF CONFIG light illuminates when advancing thrust levers for takeoff.
- Assure correct airplane takeoff configuration
MEM: Loss Of Thrust On Both Engines
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Conditions
Condition: Both of these occur:
- Both engines have a loss of thrust
- Both ENG FAIL alerts show. (these need to illuminate otherwise you may interrupt the auto re-light function)
1. ENGINE START switches (both) - FLT
2. Engine start levers (both) - CUTOFF
3. When EGT decreases:
Engine start levers (both) - CUTOFF
- If EGT reaches a redline or there is no increase in EGT within 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
MEM: RAPID DEPRESSURISATION
- Don oxygen masks and set regulators to 100%
- Establish crew communications
- Pressurization mode selector - MAN
- Outflow VALVE switch - Hold in CLOSE until the outflow VALVE indication shows fully closed
- If cabin altitude is uncontrolable:
Passenger signs - ON
PASS OXYGEN switch - ON
>> Go to the Emergency Descent checklist on page 0.1
MEM: Runaway Stabilizer
- Control column - Hold firmly
- Autopilot (if engaged) - Disengage
- Do not re-engage the autopilot.
- Control airplane pitch attitude manually with control column and main electric trim as needed.
- Autothrottle (if engaged) - Disengage
- Do not re-engage autothrottle.
- If the runaway stops after the autopilot is disengaged:
X X X X
- 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
