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

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

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- 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 Vmo/MMO

Question 6

Engine fire

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
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

Question 7

Engine Limit or Surge or Stall

Answer 7

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 8

Engine overheat

Answer 8

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 9

Engine Severe Damage or Separation

Answer 9

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

Question 10

Landing configuration

Answer 10

1- Assure correct airplane landing configuration.

Question 11

Loss Of Thrust On Both Engines

Answer 11

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 12

Runaway Stabilizer

Answer 12

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 Electri c 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