Memory Actions

Question 1

Aborted Engine Start (1)

Answer 1

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

Question 2

Airspeed Unreliable (4)

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 (2)

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 (5)

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
PASS OXYGEN switch . . . . . . . . . . . . . . . .ON
►►Go to the Emergency Descent checklist

Question 5

Emergency Descent (7)

Answer 5

1) Announce the emergency descent. The pilot flying will advise the cabin crew, on the PA system. 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.

Question 6

ENGINE FIRE or Engine Severe Damage or Separation (5)

Answer 6

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

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

Question 7

ENGINE OVERHEAT (3)

Answer 7

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

Question 8

Engine Limit or Surge or Stall (2)

Answer 8

1) Autothrottle (if engaged). . . . . . . . . . .Disengage

2) Thrust lever (affected engine) . . . . Confirm. . . . .Retard until engine indications stay within limits or the thrust lever is closed

Question 9

Engine Tailpipe Fire (1)

Answer 9

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

Question 10

LANDING CONFIGURATION (1)

Answer 10

1) Assure correct airplane landing configuration.

Question 11

TAKEOFF CONFIGURATION (1)

Answer 11

1) Assure correct airplane takeoff configuration.

Question 12

Loss Of Thrust On Both Engines (4)

Answer 12

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.

Question 13

Runaway Stabilizer (7)

Answer 13

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 Electric Stabilizer 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

Question 14

WARNING HORN (INTERMITTENT) or WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION (1)

Answer 14

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.

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.