Emergency Boldface

Question 0

ENGINE OVERHEAT

Answer 0

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

Question 1

ENGINE FIRE
or
Engine Severe Damage or Separation

Answer 1

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 stays 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 2

Loss Of Thrust On Both Engines

Answer 2

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 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 5

Engine Limit or Surge or Stall

Answer 5

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

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

Question 6

TAKEOFF CONFIGURATION

Answer 6

1 Assure correct airplane takeoff configuration.

Question 8

WARNING HORN -

CABIN ALTITUDE OR CONFIGURATION

Answer 8

1 If the intermittent warning horn sounds and the CABIN ALTITUDE lights (if installed and operative) illuminate in flight:

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 and the TAKEOFF CONFIG lights (if installed and operative) illuminate on the ground:

Assure correct airplane takeoff configuration.

3 If the steady warning horn sounds in flight:

Assure correct airplane landing configuration.

Question 9

Overspeed

Answer 9

1 Reduce thrust and, if needed, adjust attitude to reduce airspeed to less than Vmo/Mmo.

Question 11

APU FIRE

Answer 11

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

2 APU Switch . . . . . . . . . . . . . . . . . . . . . .OFF

Question 13

Aborted Engine Start

Answer 13

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

Question 14

Runaway Stabilizer

Answer 14

1 Control column. . . . . . . . . . . . . . . . . Hold firmly

2 Autopilot (if engaged) . . . . . . . . . . . . .Disengage

Do not re-engage the autopilot.

Control airplane pitch attitude manually with control column and main electric trim as needed.

3 If the runaway stops:

4 If the runaway continues:

STAB TRIM CUTOUT switches (both) . . . . . . . . . . . . . . . . CUTOUT

If the runaway continues:

Stabilizer trim wheel. . . . . . . . . . . Grasp and hold

Question 15

Condition: ENGINE FIRE or Engine Severe Damage or Separation

Answer 15

One or more of these occur:
•Engine fire warning
•Airframe vibrations with unusual engine indications •Engine separation.

Question 16

Condition: Loss Of Thrust On Both Engines

Answer 16

Both of these occur:
•Both engines have a loss of thrust
•Both ENG FAIL alerts show.

Objective: To restart at least one engine.

Question 17

Condition: Engine Limit or Surge or Stall

Answer 17

One or more of these occur:
•Engine indications are unusual
•Engine indications are rapidly approaching or exceeding limits
•Unusual engine noises are heard
•There is no response to thrust lever movement.

To attempt to recover normal engine operation or shut down the engine if recovery is not possible.

Question 18

Condition: Aborted Engine Start

Answer 18

During a ground start, an abort engine start condition occurs.

Objective: To shut down the engine and motor it.

Question 19

Condition: TAKEOFF CONFIGURATION

Answer 19

On the ground, the intermittent cabin altitude/configuration warning horn sounds and the TAKEOFF CONFIG lights (if installed and operative) illuminate when advancing the thrust levers to takeoff thrust.

Question 20

Condition: WARNING HORN - CABIN ALTITUDE OR CONFIGURATION

Answer 20

One of these occurs:
•In flight, an intermittent horn sounds and the CABIN ALTITUDE lights (if installed and operative) illuminate, when the cabin altitude is at or above 10,000 feet
•On the ground, an intermittent horn sounds and the TAKEOFF CONFIG lights (if installed and operative) illuminate, when the takeoff configuration is not correct during takeoff
•In flight, a steady horn sounds when the landing configuration is not correct.

Question 21

Condition: CABIN ALTITUDE WARNING or Rapid Depressurization

Answer 21

One or more of these occur:
•A cabin altitude exceedance
•In flight, the intermittent cabin altitude/configuration warning horn sounds and the CABIN ALTITUDE lights (if installed and operative) illuminate.

Question 22

Condition: Airspeed Unreliable

Answer 22

The pitch attitude is not consistent with the phase of flight, altitude, thrust and weight, or noise or low frequency buffeting is experienced.

Objective: To establish the normal pitch attitude and thrust setting for the phase of flight.

Question 23

Condition: Emergency Descent

Answer 23

One or more of these occur:
•Cabin altitude cannot be controlled when the airplane is above 14,000 feet
•A rapid descent is needed.

Question 24

Condition: Runaway Stabilizer

Answer 24

Uncommanded stabilizer trim movement occurs continuously.

Question 27

CABIN ALTITUDE WARNING
or
Rapid Depressurization

Answer 27

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 outflow VALVE indicates fully closed

5 If cabin altitude is not controllable:

Passenger signs . . . . . . . . . . . . . . . . . . . . ON

If the cabin altitude exceeds or is expected to exceed 14,000 feet:

PASS OXYGEN switch . . . . . . . . . . . . ON

Question 29

Evacuation

Answer 29

1 PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . Set

2 Speedbrake lever . . . . . . . . . . . . . . . . . . DOWN

3 FLAP lever . . . . . . . . . . . . . . . . . . . . . . . . . . 40

4 Pressurization mode selector . . . . . . . . . . . .MAN

5 Outflow VALVE switch . . . . Hold in OPEN until the outflow VALVE position indicates fully open

6 If time allows:

Verify that the flaps are 40 before the engine start levers are moved to CUTOFF.

7 Engine start levers (both) . . . . . . . . . . . CUTOFF

8 Advise the cabin to evacuate.

9 Advise the tower.

10 Engine and APU fire switches (all) . . . . . . . . . . .Override and pull

11 If an engine or APU fire warning occurs:

Illuminated fire switch. . . . . Rotate to the stop and hold for 1 second

Question 30

Emergency Descent

Answer 30

1 Announce the emergency descent. The captain will advise the cabin crew, on the PA system, of impending rapid descent. The first officer 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.

Question 32

Airspeed Unreliable

Answer 32

1 Adjust the airplane attitude and thrust. Maintain airplane control.

2 PROBE HEAT switches . . . . . . . . . . . . . Check ON

3 Cross check the MACH/AIRSPEED indicators.

Question 33

Elevator Tab Limit Cycle Oscillation

Answer 33

1 Airspeed . . . . . . . . . Reduce to 270 KIAS or until the vibration ceases, whichever is lower

2 Do not use speedbrakes or change aircraft configuration to reduce airspeed.