Memory Items Flashcards
Aborted engine start
Condition: On the ground, an aborted engine start is needed.
Objective: To shut down the engine and motor it.
1 Engine start lever (affected engine) . . . . CUTOFF
Engine Limit or Surge or Stall
Condition: One or more of these occur:
•Engine indications are abnormal
•Engine indications are rapidly approaching or exceeding limits
•Abnormal engine noises 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.
Objective: To attempt to recover normal engine operation or shut down the engine if recovery is not possible.
1 Autothrottle (if engaged). . . . . . . . . . .Disengage
2 Thrust lever (affected engine) . . . . Confirm. . . . .Retard until engine indications stay within limits or the thrust lever is closed
APU FIRE
Condition: Fire is detected in the APU.
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
Condition: One or more of these occur:
•A cabin altitude exceedance
•In flight, the intermittent cabin altitude/configuration warning horn sounds or the CABIN ALTITUDE light (as installed) illuminates.
1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications.
CPCS airplanes 3 Pressurization mode selector . . . . . . . . . MAN AC
DCPCS airplanes 4 Pressurization mode selector . . . . . . . . . . . .MAN
5 Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until the outflow VALVE indication shows fully closed
6 If cabin altitude is uncontrollable:
Passenger signs . . . . . . . . . . . . . . . . . . . .ON
PASS OXYGEN switch . . . . . . . . . . . . . . . .ON
►►Go to the Emergency Descent checklist on page 0.1
ENGINE FIRE or Engine Severe Damage or Separation
Condition: One or more of these occur:
•Engine fire warning
•Airframe vibrations with abnormal engine indications
•Engine 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 is 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 Limit or Surge or Stall
Condition: One or more of these occur:
•Engine indications are abnormal
•Engine indications are rapidly approaching or exceeding limits
•Abnormal engine noises 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.
Objective: To attempt to recover normal engine operation or shut down the engine if recovery is not possible.
1 Autothrottle (if engaged). . . . . . . . . . .Disengage
2 Thrust lever (affected engine) . . . . Confirm. . . . .Retard until engine indications stay within limits or the thrust lever is closed
ENGINE OVERHEAT
Condition: An overheat is detected in the engine.
1 Autothrottle (if engaged). . . . . . . . . . .Disengage
2 Thrust lever (affected engine) . . . . . . . .Confirm . . . . . Close
3 If the ENG OVERHEAT light stays illuminated:
►►Go to the ENGINE FIRE or Engine Severe Damage or Separation checklist on page 8.2
LANDING CONFIGURATION
Condition: In flight, the steady warning horn sounds.
1 Assure correct airplane landing configuration.
TAKEOFF CONFIGURATION
Condition: On the ground, the intermittent cabin altitude/configuration warning horn sounds or the TAKEOFF CONFIG light (as installed) illuminates when advancing the thrust levers to takeoff thrust.
1 Assure correct airplane takeoff configuration.
Loss Of Thrust On Both Engines
Condition: Both of these occur: •Both engines have a loss of thrust •Loss of thrust lever response from both engines.
Objective: To restart at least one engine.
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.
CABIN ALTITUDE WARNING or Rapid Depressurization
Condition: One or more of these occur:
•A cabin altitude exceedance
•In flight, the intermittent cabin altitude/configuration warning horn sounds or the CABIN ALTITUDE light (as installed) illuminates.
1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications.
CPCS airplanes 3 Pressurization mode selector . . . . . . . . . MAN AC
DCPCS airplanes 4 Pressurization mode selector . . . . . . . . . . . .MAN
5 Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until the outflow VALVE indication shows fully closed
6 If cabin altitude is uncontrollable:
Passenger signs . . . . . . . . . . . . . . . . . . . .ON
PASS OXYGEN switch . . . . . . . . . . . . . . . .ON
►►Go to the Emergency Descent checklist on page 0.1
Runaway Stabilizer
Condition: Uncommanded stabilizer trim movement occurs continuously.
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 Autothrottle (if engaged). . . . . . . . . . .Disengage
Do not re-engage 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
Uncommanded Rudder/Yaw Or Roll
Condition: Uncommanded rudder pedal displacement or pedal kicks, or uncommanded yaw or roll occurs.
1 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
2 Maintain control of the airplane with all available flight controls. If roll is uncontrollable, immediately reduce pitch/angle of attack and increase airspeed. Do not attempt to maintain altitude until control is recovered.
3 Autothrottle (if engaged). . . . . . . . . . .Disengage
4 Verify thrust is symmetrical.
