Aborted Engine Start
1. Engine start lever (affected engine)………CUTOFF
APU FIRE
1.
2.
APU fire switch……Confirm….…Pull, rotate
to the stop, and
hold for 1 second
APU switch……………………………..OFF
Set a lower MCP altitude
PASS OXYGEN switch….ON
Advise ATC and obtain area
altimeter setting.
ENGINE START
switches….CONT
Consider turn
Select LVL CHG
Close thrust levers
Select BELOW on
transponder
Select FIXED LANDING lights
ON
Extend the speedbrake
Set target speed to
MMO/VMO (if structural
integrity is in doubt, limit
airspeed and avoid high
maneuvering loads).
Airspeed Unreliable
1.
2.
3.
4.
Autopilot (if engaged)…………………………..Disengage
Autothrottle (if engaged)……………………..Disengage
F/D switches (both)……………………………….OFF
Set the following gear up pitch attitude and thrust:
Flaps extended…………..…………………...10° and 80% N1
Flaps up……………………………………………..4° and 75% N1
CABIN ALTITUDE WARNING or Rapid
Depressurization
Pilot Flying
Call for CABIN ALTITUDE
memory items
Don oxygen masks and set
regulators to 100%. Establish
crew communication
Pilot Monitoring
Adjust level off altitude to
10000ft or the lowest safe
altitude whichever is higher.
Adjust MCP altitude as
needed
Pressurization mode
selector……..MAN
Outfllow VALVE
switch……..HOLD in CLOSE
until the outflow VALVE
indication shows fully
closed.
If the cabin altitude is
uncontrollable, the
emergency descent is
initiated
Advise cabin crew on public
address
Adjust heading as needed
Passengers signs…………ON
If the cabin altitude exceed
or is expected to exceed
14.000ft
Call for CABIN ALTITUDE
Warning or Rapid
Depressurization and
Emergency Descent
checklists.
Verify lowest safe altitude
and advise pilot flying.
Do the CABIN ALTITUDE
Warning or Rapid
Depressurization and
Emergency Descent
checklists.
Call “2000ft TO LEVEL OFF”
Set speed as needed
Call “1000ft TO LEVEL OFF”
When speed reduced, retract
speedbrakes
Initiate ALERT CALL (at safe
cabin altitude)
LANDING CONFIGURATION
1.
Assure correct airplane landing configuration
Engine Limit or Surge or Stall
1.
2.
Autothrottle………………………………………….Disengage
Thrust lever
(affected engine)…...Confirm……………….Retard until
engine
indications
stay within limits
or the thrust lever is closed
ENGINE OVERHEAT
1.
2.
3.
Autothrottle…………………………………………Disengage
Thrust lever
(affected engine)…...Confirm………………Close
If the ENG OVERHEAT light stays illumi nated
>> Go to the ENGINE FIRE or Engine Severe Damage
or Separation checklist on page 8.2
ENGINE FIRE
1.
2.
3.
4.
5.
6.
or
Engine Severe Damage or Separation
Autothrottle………………………………….Disengange
Thrust lever
(affected engine)……Confirm..………Close
Engine start lever
(affected engine)……Confirm………..CUTOFF
Engine fire switch
(affected engine)……Confirm………..Pull
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
WARNING HORN (INTERMITTENT)
or
WARNING LIGHT – CABIN ALTITUDE OR
TAKEOFF CONFIGURATION
Emergency Descent
1.
2.
3.
4.
5.
6.
7.
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.
Passenger signs…………………………………….ON
Without delay, descent to the lowest safe altitude or
10.000ft, whichever is higher
ENGINE START switches (both)…………….CONT
Thrust levers (both)………………………………Reduce
thrust to
minimum or
as needed for
anti-ice
Speedbrake………………………………………….FLIGHT
DETENT
Set target speed to Mmo/Vmo
If the intermittent warning horn sounds or a CABIN
ALTITUDE light (if installed and operative) illuminates in
flight at an airplane flight altitude above 10.000ft MSL:
1.
2.
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
If the intermittent warning horn sounds or a TAKEOFF
CONFIG light illuminates on the ground:
Assure correct airplane takeoff configuration
TAKEOFF CONFIGURATION
1.
Assure correct airplane take-off configuration
Overspeed
1.
Reduce thrust and, if needed, adjust attitude to
reduce airspeed to less than Vmo/Mmo.
Runaway Stabilizer
Loss Of Thrust On Both Engines
1.
2.
3.
4.
ENGINE START switches (both)…………… FLT
Engine start levers (both)…………………….CUTOFF
When EGT decreases
Engine start levers (both)…………………….IDLE detent
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.
1.
2.
3.
4.
5.
Control column…………………………………….Hold firmly
Autopilot………………………………………………Disengage
Do not re-engage the autopilot
Control airplane pitch attitude manually with control
column and main electric trim as needed.
Autothrottle………………………………………….Disengage
Do not re-engage the autothrottle
If the runaway stops after the autopilot is
disengaged
If runaway continues after the autopilot is
disengaged:
STAB TRIM CUTOUT
switches (both)…………………………………….CUTOUT
If the runaway continues
Stabilizer trim wheel……………………………Grasp and
hold
Evacuation
1.
2.
3.
4.
5.
PARKING BRAKE……………………………………..Set
C
Speedbrake lever…………………………………….DOWN C
Flap lever…………………………………………………40
F/O
Pressurization mode selector………………….MAN F/O
Outflow Valve switch………………………………Hold F/O
In OPEN until the
outflow VALVE indication shows
fully open to depressurize the airplane
6. If time allows, verify that the flaps are 40
C
before the engine start levers are moved
to CUTOFF.
7. Engine start levers (both)…………………………CUTOFF C
8. Advise the cabin to evacuate
C
9. Advise the tower
F/O
10. Engine and APU fire switches (all)……………Override
and pull F/O
11. If an engine or APU fire warning occurs:
Illuminated fire switch……………………….Rotate to
the stop and hold for 1 second
F/O