-
Rejected Take-off Before Achieving V1
- Simultaneously:
- (1) Thrust levers ......................................IDLE
- (2) Wheel brakes ......... MAXIMUM until a safe stop.
- (3) Thrust reverser(s) (operating engine[s]) ..................MAXIMUM, consistent with directional control.
-
L ENG FIRE or R ENG FIRE or Severe Engine Damage (In Flight)
- At a safe altitude, affected engine:
- (1) Thrust lever ........................CONFIRM and IDLE
- (2) Thrust lever ..............................CONFIRM and SHUT OFF
- (3) ENG FIRE PUSH ..........................CONFIRM and SELECT
- (4) FUEL, BOOST PUMP ..................CONFIRM and SELECT OFF
- After 10 seconds, L ENG FIRE or R ENG FIRE warning message persists:
- (5) Affected engine BOTTLE ..............................................SELECT
- After another 30 seconds, L ENG FIRE or R ENG FIRE warning message still persists:
- (6) Other engine BOTTLE ...................................................SELECT
-
L ENG FIRE or R ENG FIRE or Severe Engine Damage (On Ground)
- NOTE
- Attempt to face the airplane into the wind.
- (1) PARKING BRAKE ................................................................. ON
- Affected engine:
- (2) Thrust lever ...............................................................SHUT OFF
- (3) ENG FIRE PUSH .....................................SELECT
- (4) FUEL, L and R BOOST PUMP ............................. SELECT OFF
- After 10 seconds, L ENG FIRE or R ENG FIRE warning
- message persists:
- (5) Both engine BOTTLE ........................SELECT
-
Double Engine Failure
- (1) IGNITION, CONT ...................................... ON
- (2) Airspeed ............. Not less than 240 KIAS
-
L REV DEPLOYED or R REV DEPLOYED
(1) Affected thrust lever ...................CONFIRM and IDLE
-
Uncommanded Acceleration / ENGINE OVERSPD
(1) Affected thrust lever ............CONFIRM and IDLE
-
CABIN ALT (Warning Message) or Emergency Descent Procedure
- (1) Oxygen masks ........ DON, SET to 100%
- (2) Crew communication ......................ESTABLISH
- (3) PASS SIGNS (both) .......................................... ON
- (4) Descent ..................... INITIATE to 10000 feet MSL
- or lowest safe altitude, whichever is higher.
- (5) Thrust levers .............................................IDLE
- (6) Flight spoilers .....................................DEPLOY
-
Uncommanded Yaw Motion
- (1) Controls .................. Assume manual control and counter aircraft motion using hand wheel inputs.
- (2) YAW DAMPER, DISC ......... SELECT to disconnect both yaw dampers.
-
APU FIRE
- (1) APU FIRE PUSH ................................SELECT
- After 5 seconds, APU FIRE warning message persists:
- (2) APU BOTTLE .............................SELECT
-
Ditching or Forced Landing Imminent
- (1) L and R PACKs ............................................ OFF
- (2) EMER DEPRESS ........................................ ON
- Just before contact:
- (3) EMER DEPRESS ................ SELECT OFF
-
Passenger Evacuation
- Pilot:
- (1) PARKING BRAKE ...................................... ON
- (2) Evacuation .................................COMMAND
- (3) GND LIFT DUMPING .............................MAN DISARM
- (4) Thrust levers ......................................SHUT OFF
- (5) Evacuation .............. INITIATE using PA system
- (6) APU, LH ENG and RH ENG FIRE
- PUSH ..................................SELECT
- (7) BATTERY MASTER .................................. OFF
- --------------------------------------------------
- Copilot: On evacuation command
- (8) Air Traffic Control (ATC) ..................NOTIFY of emergency
- conditions and intent to evacuate.
- NOTE:
- If ditching, disregard step (9).
- (9) EMER DEPRESS .................................... ON
- (10) EMER LTS (coincident with PA) ............................................ ON
-
Loss of all AC Power
(1) ADG manual deploy ...............................PULL
-
Aileron System Jammed
- (1) Autopilot ......................... DISENGAGE
- (2) Aileron controls (both) ................................. RELEASE pressure
- (3) ROLL DISC ........ PULL and TURN to lock
- (4) Airplane control .................. TRANSFER to pilot with operative aileron.
-
Elevator System Jammed
- (1) Autopilot ................................................................ DISENGAGE
- (2) Elevator controls (both) ............................ RELEASE differential
- pressure
- (3) PITCH DISC ......................................... PULL and TURN to lock
- (4) Airplane control .................................... TRANSFER to pilot with operative elevator.
-
Stabilizer Trim Runaway
- (1) Control wheel ...............................ASSUME manual control and OVERRIDE runaway.
- (2) STAB TRIM DISC ................................SELECT
-
Stall Recovery
- (1) Autopilot .......... DISENGAGE, if required
- (2) Pitch attitude ....... Lower nose to reduce angle
- of attack.
- (3) Thrust levers ........ Advance to MAX POWER
- (4) Roll attitude ...................... Wings level
- (5) FLIGHT SPOILER lever ..................RETRACT
-
MLG BAY OVHT
- (1) Airspeed .........Not more than 220 KIAS
- (2) LDG GEAR lever ....................................... DN
-
BRAKE OVHT
- (1) Airspeed .........Not more than 220 KIAS
- (2) LDG GEAR lever .......................... DN
-
During Landing – Excessive Asymmetry or Loss of Braking
- (1) Wheel brakes ........ RELEASE momentarily
- (2) ANTI-SKID .......................................... OFF
- (3) Wheel brakes ...........RE-APPLY, as required
-
Configuration Warning
(1) Take-off ...........DISCONTINUE IMMEDIATELY
-
Unreliable Airspeed In-flight
- If above minimum safe altitude:
- (1) Autopilot ......................... DISENGAGE
- (2) FDs .......................................DESELECT
- (3) Use ISI.
- CAUTION
- Respect stall warning/stick shaker.
- (4) Proceed to step (7).
- If below minimum safe altitude:
- (1) Autopilot ......................... DISENGAGE
- (2) FDs ......................................DESELECT
- (3) Use ISI.
- (4) Pitch/N1 .......................10 degrees/TO
- (5) Airplane ...............Go-around, clean up and
- climb above minimum safe altitude
- Above 15000 feet:
- (6) Pitch/N1 .......................5 degrees/CLB
- CAUTION
- Respect stall warning/stick shaker.
|
|
