Memory Items

Question 1

Aborted Engine Start

Answer 1

1 Engine start lever (affected engine) . . . . CUTOFF

Question 2

Airspeed Unreliable

Answer 2

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

Question 3

APU FIRE

Answer 3

1 APU fire switch…Confirm….Pull,rotate to the stop, and hold for 1 second

2 APU switch . . . . . . . . . . . . . . . . . . . . . . . . OFF

Question 4

CABIN ALTITUDE WARNING
or
Rapid Depressurization

Answer 4

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
PASSOXYGENswitch …………….ON
►►Go to the Emergency Descent checklist on page 0.4

Question 5

Emergency Descent

Answer 5

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 Passengersigns………………….ON
3 Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
4 ENGINE START switches (both) . . . . . . . . . CONT
5 Thrustlevers(both) ……… Reducethrustto minimum or as needed for anti-ice
6 Speedbrake . . . . . . . . . . . . . . . .FLIGHT DETENT

If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads.

7 Set target speed to Mmo/Vmo.

Question 6

ENGINE FIRE
or
Engine Severe Damage or Separation

Answer 6

1 Autothrottle(ifengaged)………..Disengage
2 Thrustlever
(affected engine) . . . . . . Confirm . . . . . . . Close
3 Enginestartlever
(affectedengine) ……Confirm….. CUTOFF
4 Enginefireswitch
(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

Question 7

Engine Limit or Surge or Stall

Answer 7

1 Autothrottle(ifengaged)………..Disengage
2 Thrustlever
(affected engine) . . . . Confirm. . . . .Retard until engine indications stay within limits or the thrust lever is closed

Question 8

ENGINE OVERHEAT

Answer 8

1 Autothrottle(ifengaged)………..Disengage
2 Thrustlever
(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

Question 9

LANDING CONFIGURATION

Answer 9

1 Assure correct airplane landing configuration.

Question 10

TAKEOFF CONFIGURATION

Answer 10

1 1 Assure correct airplane takeoff configuration..

Question 11

Loss Of Thrust On Both Engines

Answer 11

1 ENGINESTARTswitches(both) ………..FLT
2 Enginestartlevers(both)……….. CUTOFF
3 When EGT decreases:
Engine start levers (both) . . . . . . .IDLE detent

4 If EGT reaches 950°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 950°C or there is no increase in EGT within 30 seconds, repeat as needed.

Question 12

Runaway Stabilizer

Answer 12

1 Control column. . . . . . . . . . . . . . . . . Hold firmly
2 Autopilot(ifengaged)………….Disengage
Do not re-engage the autopilot.
Control airplane pitch attitude manually with control column and main electric trim as needed.
3 Autothrottle(ifengaged)………..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
trimwheel .......... Grasp and hold

Question 13

Nose high recovery

Answer 13

• Disconnect autopilot and autothrottle
• Apply as much as full nose-down elevator • * Apply appropriate nose down stabilizer trim
• Reduce thrust
• • Roll (adjust bank angle) to obtain a nose down pitch rate
• Complete the recovery: - When approaching the horizon, roll to wings level - Check airspeed and adjust thrust - Establish pitch attitude.

Question 14

Nose low recovery

Answer 14

• Disconnect autopilot and autothrottle
• Recover from stall, if required
• • Roll in shortest direction to wings level (unload and roll if bank angle is more than 90 degrees)
• Recover to level flight: - Apply nose up elevator - *Apply nose up trim, if required - Adjust thrust and drag as required.

Question 15

Windshear escape

Answer 15

• Disconnect autopilot.
• Press either TO/GA switch.
• Aggressively apply maximum thrust*
• Disconnect autothrottle.
• Simultaneously roll wings level and rotate toward an initial pitch attitude of 15°.
• Retract speedbrakes.
• Follow flight director TO/GA guidance (if available) **
• Do not change flap or gear configuration until windshear is no longer a factor.
• Monitor vertical speed and altitude.
• Do not attempt to regain lost airspeed until windshear is no longer a factor.

Question 16

Terrain escape

Answer 16

Disconnect autopilot.

Disconnect autothrottle.

Aggressively apply maximum* thrust.

Simultaneously roll wings level and rotate to an initial pitch attitude of 20°.

Retract speedbrakes.

If terrain remains a threat, continue rotation up to the pitch limit indicator (if available) or stick shaker or initial buffet.

Assure maximum* thrust.

Verify all required actions have been completed and call out any omissions.