2021 QRH Memory Items and Safety PAs Flashcards
Aborted Engine Start.
Condition: On the ground an aborted engine start is needed.
Objective: To shutdown the engine and motor it.
Engine start lever affected engine- cutoff.
Choose 1- Engine start switch is GRD?
Motor the engine for 60secs,
Engine start switch affected engine AUTO.
- Engine start switch is in AUTO? After N2 decreases to below 20%: Engine start switch (affected engine) GRD Motor the engine for 60secs Engine start switch Auto
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 use the Flight With Unreliable Airspeed table in the Performance Inflight chapter for the remainder 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% N1Flaps up . . . . . . . . . . . . . . . . 4° and 75% N1
Emergency Descent
Condition: cabin altitude can not 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 10,000ft, 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 Detention.
7 Set Target speed to MMO/VMO. (Caution if structural integrity is in doubt limit speed as much as possible and avoid high manoeuvring loads).
APU Fire
Condition; a 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
AUTOMATIC UNLOCK
Condition:The correct emergency access code is entered.
Objective:To deny unauthorized access to the flight deck before the door automatically unlocks
FLT DK DOOR lock selector . . . . . Rotate to DENYand hold for 1 second
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 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 CLOSEuntil the outflow VALVEindication shows fully closed
5 If cabin altitude is uncontrollable:Passenger signs . . . . . . . . . . . . . . . . . . . . ONPASS OXYGEN switch . . . . . . . . . . . . . . . . ON
Go to the emergency descent checklist on pg 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
3Engine start lever(affected engine) . . . . . . Confirm . . . . . CUTOFF
4 Engine fire switch(affected engine) . . . . . . Confirm . . . . . . . . PullTo 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 andhold 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.
LANDING CONFIGURATION
Condition: Inflight a steady warning horn sounds.
Assure correct airplane landing configuration
TAKE OFF CONFIGURATION
Condition:On the ground, the intermittent cabin altitude/configuration warning horn sounds or a TAKEOFF CONFIG light illuminates when advancing the thrust levers to takeoff thrust.
Assure correct airplane take off configuration
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 detentIf 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. . . . . . . . . . . . . . . . . Hold firmly
2 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
3 Autothrottle (if engaged). . . . . . . . . . .Disengage
4 Control column and thrust levers . . . . . . . . . . . Control airplane pitch attitude and airspeed
5 Main ElectricStabilizer 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 trim wheel . . . . . . . . . . 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 10,000ft MSL, the intermittent warning horn sounds or a CABIN ALTITUDE light illuminates
•On the ground, the intermittent warning horn sounds or a TAKEOFF CONFIG light illuminates when advancing the thrust levers to takeoff thrust
If the intermittent warning horn sounds or a CABIN ALTITUDE light illuminates in flight at an airplane flight altitude above 10,000ft MSL:Don the oxygen masks and set the regulators to 100%.
Establish crew communications
Go to the CABIN Altitude checklist on pg 2.1
ALERT ORDER
Condition:Used following an abnormality.
Objective:This PA notifies Cabin Crew of the existence of an emergency situation and pre-empts the possibility of an evacuation being carried out unnecessarily or prematurely. Should only be given on the ground when the aircraft has stopped or about to stop
1“Attention! All passengers remain seated and await further instructions”.
