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30 Cards in this Set

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  • Back
Aborted Engine Start
7.1
Aborted Engine Start
1 Engine start lever (affected engine) . . . . CUTOFF
- - - - - - - - - - - - - - - - - - - - - - -
Airspeed Unreliable
10.1
Airspeed Unreliable
1 Adjust the airplane attitude and thrust. Maintain
airplane control.
2 PITOT STATIC HEAT switches . . . . . . . . Check ON
3 Cross check the MACH/AIRSPEED indicators.
- - - - - - - - - - - - - - - - - - - - - - -
APU FIRE
8.1
APU FIRE
1 APU fire switch. . . Confirm . . . .Pull, rotate to the
stop, and hold
for 1 second
2 APU switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
CABIN ALTITUDE WARNING or
Rapid Depressurization
2.1
CABIN ALTITUDE WARNING or
Rapid Depressurization
1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications.
3 Pressurization mode selector . . . . . .MAN AC/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
Emergency Descent
0.1
Emergency Descent
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
- - - - - - - - - - - - - - - - - - - - - - -
ENGINE FIRE
or
Engine Severe Damage or
Separation
8.2
ENGINE FIRE
or
Engine Severe Damage or
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
- - - - - - - - - - - - - - - - - - - - - - -
Engine Limit or Surge or Stall
7.2
Engine Limit or Surge or Stall
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
2 Thrust lever
(affected engine) . . . . Confirm. . . . .Retard until
indications stay
within limits or
the thrust lever is closed
- - - - - - - - - - - - - - - - - - - - - - -
ENGINE OVERHEAT
8.4
ENGINE OVERHEAT
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
2 Thrust lever
(affected engine) . . . . . . . .Confirm . . . . . Close
3 If the ENG OVERHEAT light stays illuminated:
ENGINE FIRE
or
Engine Severe Damage or
Separation
8.2
ENGINE FIRE
or
Engine Severe Damage or
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
- - - - - - - - - - - - - - - - - - - - - - -
Engine Tailpipe Fire
8.6
Engine Tailpipe Fire
1 Engine start lever
(affected engine) . . . . . . . . . . . . . . . . . CUTOFF
2 Advise the cabin.
3 Choose one:
4 PACK switches (both) . . . . . . . . . . . . . . . . . OFF
5 ISOLATION VALVE switch. . . . . . . . . . . . . . AUTO
6 Engine BLEED air switches (both) . . . . . . . . . .ON
7 Choose one:
Evacuation
Back Cover.2
Evacuation
1 PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . Set
2 Speedbrake lever . . . . . . . . . . . . . . . . . . DOWN
3 FLAP lever . . . . . . . . . . . . . . . . . . . . . . . . . . 40
4 STANDBY POWER switch . . . . . . . . . . . . . . . BAT
5 Pressurization mode selector . . . . . . . . . MAN DC
6 Outflow VALVE switch . . . . Hold in OPEN until the
outflow VALVE position
indicates fully open
7 If time allows:
Verify that the flaps are 40 before the engine
start levers are moved to CUTOFF.
8 Engine start levers (both) . . . . . . . . . . . CUTOFF
9 Advise the cabin to evacuate.
10 Advise the tower.
11 Engine and APU
fire switches (all) . . . . . . . . . . .Override and pull
12 If an engine or APU fire warning occurs:
Illuminated fire switch. . . . . Rotate to the stop
and hold for 1 second
Loss Of Thrust On Both Engines
7.6
Loss Of Thrust On Both Engines
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.
- - - - - - - - - - - - - - - - - - - - - - -
Overspeed
15.1
Overspeed
1 Reduce thrust and, if needed, adjust attitude to
reduce airspeed to less than Vmo/Mmo.
- - - - - - - - - - - - - - - - - - - - - - -
Rapid Depressurization
2.1
Rapid Depressurization
1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications.
3 Pressurization mode selector . . . . . .MAN AC/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
Runaway Stabilizer
9.1
Runaway Stabilizer
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: