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
Airspeed Unreliable
Condition: Airspeed or Mach indications are suspected to be unreliable. (Items which might indicate unreliable airspeed are listed in the Additional Information section.)
Objective: To identify a reliable airspeed indication, if possible, or to continue the flight using the Flight With Unreliable Airspeed table in the Performance Inflight chapter for the reminder of the flight.
1 Autopilot (if engaged) . . . . . . . . . . . . . Disengage
2 Autothrottle (if engaged) . . . . . . . . . . . Disengage
3 F/D switches (both) . . . . . . . . . . . . . . . . . . OFF
4 Set the following gear up pitch attitude and thrust: Flaps extended . . . . . . . . . . 10° and 80% N1
Flaps up . . . . . . . . . . . . . . . . 4° and 75% N1
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 a CABIN ALTITUDE light (if installed and operative) illuminates.
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 is uncontrollable:
Passenger signs . . . . . . . . . . . . . . . . . . . . ON
PASS OXYGEN switch . . . . . . . . . . . . . . . . ON
►►Go to the Emergency Descent checklist on page 0.1
Emergency Descent
Condition: One or more of these occur:
•Cabin altitude cannot be controlled
•A rapid descent is needed.
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
7 Set target speed to Mmo/Vmo.
If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads.
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 (affected engine). . . . . Rotate to the stop and hold for 1 second
Loss Of Thrust On Both Engines
Condition: Both of these occur:
•Both engines have a loss of thrust
•Both ENG FAIL alerts show.
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 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.
Runaway Stabilizer
Condition: Uncommanded stabilizer trim movement occurs continuously or in a manner not appropriate for flight conditions.
1 Control column…………….. Holdfirmly
2 Autopilot(if engaged)………….Disengage
3 Autothrottle(if engaged)………..Disengage
4 Control column and
thrust levers . . . . . . . . . . .Control airplane pitch
attitude and airspeed
5 Main Electric
Stabiliser trim ……………Reduce control
column forces
6 If the runaway stops after the autopilot is disengaged:
Do not re-engage the autopilot or autothrottle.
■■■■
7 If the runaway continues after the autopilot is disengaged:
STAB TRIM cutout
switches(both) ……………. CUTOUT
If the runaway continues: Stabilizer
trimwheel ……….Grasp and hold
WARNING HORN (INTERMITTENT)
or WARNING LIGHT - CABIN ALTITUDE
OR TAKEOFF CONFIGURATION
Condition: One of these occurs:
•In flight, at an airplane flight altitude above 10,000 feet MSL, the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates •On the ground, the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates when advancing the thrust levers to takeoff thrust.
1 If the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates in flight at an airplane flight altitude above 10,000 feet MSL: Don the oxygen masks and set the regulators to 100%.
Establish crew communications.
►►Go to the CABIN ALTITUDE WARNING or Rapid Depressurization checklist on page 2.1
■ ■ ■ ■
2 If the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates on the ground when advancing the thrust levers to takeoff thrust: Assure correct airplane takeoff configuration.
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
