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Flashcards in Quick Action Memory Items Deck (16)
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0

Aborted Engine Start
7.1

Aborted Engine Start

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

Objective: To shut down the engine and motor it.

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

Airspeed Unreliable
10.1

Airspeed Unreliable

Condition: 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.

1 Adjust the airplane attitude and thrust. Maintain airplane control.
2 PITOT STATIC HEAT switches . . . . . . . . Check ON
3 Cross check the MACH/AIRSPEED indicators.
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2

APU FIRE
8.1

APU FIRE

Condition: 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
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3

CABIN ALTITUDE WARNING or Rapid Depressurization
2.1

CABIN ALTITUDE (as installed)

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 the CABIN ALTITUDE light (as installed) illuminates.

1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications.
3 Pressurization mode selector . . . . . . . . . MAN AC
4 Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until the outflow VALVE indication shows fully closed

5 If cabin altitude is uncontrollable:
Passenger signs . . . . . . . . . . . . . . . . . . . .ON
If the cabin altitude exceeds or is expected to exceed 14,000 feet:
PASS OXYGEN switch . . . . . . . . . . . .ON

►►Go to the Emergency Descent checklist on page 0.1 5

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4

Emergency Descent
0.1

Emergency Descent

Condition:
One or more of these occur:
•Cabin pressure cannot be controlled when the airplane is above 14,000 feet
•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 10,000 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
If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads.
7 Set target speed to Mmo/Vmo.
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5

ENGINE FIRE or Engine Severe Damage or Separation
8.2

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
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
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6

Engine Limit or Surge or Stall
7.2

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
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7

ENGINE OVERHEAT
8.5

ENG 1 OVERHEAT or ENG 2 OVERHEAT

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 on page 8.2

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8

Engine Tailpipe Fire
8.6

Engine Tailpipe Fire

Condition:
An engine tailpipe fire occurs on the ground with no engine fire warning.

1 Engine start lever (affected engine) . . . . . . . . . . . . . . . . . CUTOFF
2 Advise the cabin.

3 Choose one:
Bleed air is available:
►►Go to step 4

Bleed air is not available:
Advise the tower.
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4 PACK switches (both) . . . . . . . . . . . . . . . . . OFF
5 ISOLATION VALVE switch. . . . . . . . . . . . . . AUTO
6 Engine BLEED air switches (both). . . . . . . . . .ON

7 Choose one:
APU is running:
APU BLEED air switch . . . . . . . . . . . . .ON
►►Go to step 8

APU is not running:
►►Go to step 8

8 Choose one:
Affected ENGINE START switch is in GRD:
►►Go to step 9

Affected ENGINE START switch is not in GRD:
Allow the affected N2 to decrease below 20%.
ENGINE START switch (affected engine). . . . . . . . . . . . . . .GRD
►►Go to step 9

9 Advise the tower.

10 When the tailpipe fire is extinguished:
ENGINE START switch (affected engine) . . . . . . . . . . . . . . . . . . OFF
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9

Evacuation
Back Cover.2

Evacuation

Condition:
Evacuation is needed.

1 PARKING BRAKE. . . . . . . . . . . . . . . Set (Capt)
2 Speedbrake lever . . . . . . . . . . . . DOWN (Capt)
3 FLAP lever . . . . . . . . . . . . . . . . . . . .40 (FO)
4 STANDBY POWER switch . . . . . . . . . BAT (FO)
5 Pressurization mode selector . . . MAN DC (FO)
6 Outflow VALVE switch . . . . . . . . . . . . . . . Hold in OPEN until the outflow VALVE indication shows fully open to depressurize the airplane (FO)

7 If time allows:
Verify that the flaps are 40 before the engine start levers are moved to CUTOFF. (Capt)

8 Engine start levers (both) . . . . . CUTOFF (Capt)
9 Advise the cabin to evacuate. (Capt)
10 Advise the tower. (FO)
11 Engine and APU fire switches (all) . . . . Override and pull (FO)

12 If an engine or APU fire warning occurs:
Illuminated fire switch . . . . . . . . . Rotate to the stop and hold for 1 second (FO)
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10

LANDING CONFIGURATION
15.1

Landing Config Warning Horn

LANDING CONFIGURATION

Condition: In flight, the steady warning horn sounds.

1 Assure correct airplane landing configuration.
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11

Loss Of Thrust On Both Engines
7.5

Loss Of Thrust On Both Engines

Condition:
Both of these occur:
•Both engines have a loss of thrust
•Loss of thrust lever response from both engines.

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 930°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 930°C or there is no increase in EGT within 30 seconds, repeat as needed.
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12

Runaway Stabilizer
9.1

Runaway Stabilizer

Condition:
Uncommanded stabilizer trim movement occurs continuously.

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

Autopilot (if engaged). . . . . . . . . . . . .Disengage
Do not re-engage the autopilot.
Control airplane pitch attitude manually with control column and main electric trim as needed.

Autothrottle (if engaged). . . . . . . . . . .Disengage
Do not re-engage the autothrottle.

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 trim wheel . . . . . . . . . . Grasp and hold
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13

TAKEOFF CONFIGURATION
15.1

TAKEOFF CONFIG (As installed) On the ground

TAKEOFF CONFIGURATION

Condition: On the ground, the intermittent cabin altitude/configuration warning horn sounds or the TAKEOFF CONFIG light (as installed) illuminates when advancing the thrust levers to takeoff thrust.

1 Assure correct airplane takeoff configuration.
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14

Uncommanded Roll
9.4

Uncommanded Roll

Condition:
Uncommanded roll occurs when flaps are extended with no flap asymmetry. May be accompanied by a loud bang.

1 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
2 Maintain control of the airplane with all available flight controls. If roll is uncontrollable, immediately reduce pitch/angle of attack and increase airspeed. Do not attempt to maintain altitude until control is recovered.

3 Autothrottle (if engaged). . . . . . . . . . .Disengage
4 Verify thrust is symmetrical.
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15

WARNING HORN (INTERMITTENT) or WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION
15.2

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

Condition:
One of these occurs:
•In flight, at an airplane flight altitude above 10,000 feet MSL, the intermittent warning horn sounds or the CABIN ALTITUDE light (as installed) illuminates
•On the ground, the intermittent warning horn sounds or the TAKEOFF CONFIG light (as installed) illuminates when advancing the thrust levers to takeoff thrust.

1 If the intermittent warning horn sounds or the CABIN ALTITUDE light (as installed) 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 on page 2.1
■■■■

2 If the intermittent warning horn sounds or the TAKEOFF CONFIG light (as installed) illuminates on the ground when advancing the thrust levers to takeoff thrust:
Assure correct airplane takeoff configuration.
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