CABIN ALTITUDE
- DON THE OXYGEN MASKS
- ESTABLISH CREW COMMUNICATIONS
- CHECK THE CABIN ALTITUDE AND RATE
- IF THE CABIN ALTITUDE IS UNCONTROLLABLE:
- PASS OXYGEN SWITCH………….PUSH TO ON AND HOLD FOR 1 SECOND
– WITHOUT DELAY: EMERGENCY DESCENT-ACCOMPLISH
DUAL ENG FAIL / STALL
- FUEL CONTROL SWITCHES (BOTH)
- CUTOFF, then RUN - RAM AIR TURBINE SWITCH
- PUSH AND HOLD FOR 1 SECOND
STABILIZER
(Condition: One of these occurs:
- Stabilizer movement without a signal to trim
- The stabilizer is failed)
- STAB cutout switches (both)
- CUTOUT - Do not exceed the current airspeed
AIRSPEED UNRELIABLE
- AUTOPILOT DISENGAGE SWITCH
- PUSH - A/T ARM SWITCHES (BOTH)
- OFF - F/D SWITCHES (BOTH)
- OFF - SET THE FOLLOWING GEAR UP PITCH ATTITUDE AND THRUST:
- FLAPS EXTENDED: 10 DEGREES AND 85% N1
- FLAPS UP: 4 DEGREES AND 70% N1
ENG LIM / SURGE / STALL L, R
- A/T ARM SWITCH (AFFECTED SIDE)………CONFIRM
- OFF - THRUST LEVER (AFFECTED SIDE)…………CONFIRM
- RETARD UNTIL ENGINE INDICATIONS STAY WITHIN APPROPRIATELIMITS OR THE THRUST LEVER IS AT IDLE
ENG SVR DAMAGE / SEP L, R
(Condition: One or more of these occur:
- Airframe vibration with abnormal engine indications
- Engine separation)
- A/T ARM switch (affected side)………confirm
- OFF - Thrust lever (affected side)…………confirm
- Idle - FUEL CONTROL switch (affected side)….confim
- CUTOFF - Engine fire switch (affected side)……………confirm
- PULL
FIRE ENG L, R
(Condition: Fire is detected in the engine)
- A/T ARM switch (affected side)…………….confirm
- OFF - Thrust lever (affected side)………………….confrim
- Idle - FUEL CONTROL switch (affected side)……………confirm
- CUTOFF - Engine fire switch (affected side)………….confrim
- Pull - IF the FIRE ENG message stays shown:
Engine fire switch……..Rotate to the stop and hold for
1 second
IF after 30 seconds the ENGINE FIRE message
stays shown:
- Rotate to the other stop and hold
for 1 second
ABORTED ENGINE START L, R
(Condition: During a ground start, an abort start condition occurs)
- FUEL CONTROL SWITCH (AFFECTED SIDE)
– CUTOFF
ENG AUTOSTART L, R
(Condition: During a ground start, one of these occurs:
- Autostart did not start the engine
- Fuel control switch is in RUN at low engine
- FUEL CONTROL SWITCH (AFFECTED SIDE)
- CUTOFF
WINDSHEAR ESCAPE MANEUVER
(Manual Flight)
- Push either TO/GA switch
- Aggressively apply maximum thrust
- Verify TO/GA mode annunciation
- Disconnect Autothrottle
- Simultaneously roll wings level and rotate toward an
initial pitch attitude of 15 deg - Retract speedbrakes
- Follow flight director TO/GA guidance
– Do not change gear of flap configuration until windshear is no longer a factor
– Monitor vertical speed and altitude
– Do not attempt to regain lost airspeed until windshear is no longer a factor
“MICROBURST ALERT”
If ATC issues a microburst alert for the runway of intended landing, a Go-Around MUST be executed, and if necessary, windshear escape procedures accomplished.
GPWS ALERTS
“Pull-Up” / “Terrain, Terrain, Pull-Up” / “Obstacle, Obstacle, Pull-Up” /
- Autopilot / Auto Throttles - Disconnect
- Throttles – Aggressively apply maximum thrust
- Attitude – Roll Wings Level and Rotate to an initial pitch attitude of 20 deg.
- Speed Brakes – Retract
- If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet.
GPWS ALERTS Pilot Monitoring
– Assure maximum thrust.
– Verify all required actions have been completed and call out any omissions.
– Monitor vertical speed and altitude (radio alt. for terrain clearance and baro altitude for a min safe alt.), call out any trend toward terrain contact.
REJECTED TAKEOFF Captain
Call “STOP” and
Captain: Without delay, simultaneously:
- Throttles – Close
- Autothrottles – Disengage
- Brakes – Apply maximum manual wheel brakes or
verify proper operation of RTO autobrakes
- Apply maximum reverse thrust consistent with conditions
- Verify the speedbrakes are extended
- Continue max braking until certain the airplane will
stop on the runway
SMOKE/FIRE OR FUMES
- If needed:
Don oxygen masks and smoke goggles
WINDSHEAR ESCAPE MANEUVER
(Auto Flight)
- Press either TO/GO switch
- Follow FD commands if AP not engaged
- Verify TO/GA mode annunciation
- Retract speedbrakes
- Engage A/P (if not already engaged)
- Monitor system performance
Predictive Windshear warning during approach
Call “Go-around” and perform a normal go-around
GPWS CAUTION
Correct the flight path or the airplane configuration
GPWS WARNING
- Disconnect A/P
- Disconnect A/T
- Aggressively apply maximum thrust
- Simultaneoulsy roll wings level and rotate to an initial
pitch attitude of 20 deg - Retract speedbrakes
IF terrain remains a threat:
- Continue rotation up to pitch limit indicator or stick
shaker or initial buffet
HIGH NOSE RECOVERY
- Disconnect A/P and A/T
- Apply as much as full nose down elevator
- Apply appropriate nose down stabilizer trim
- Reduce thrust
- Roll to adjust to obtain nose down pitch rate
- Complete recovery
– When approaching the horizon, roll to wings level
– Check airspeed and adjust thrust
– Establish pitch attitude
NOSE DOWN RECOVERY
- Disconnect A/P and A/T
- Recover from stall, if required
- Roll in the shortest direction to wings level
- Recover to level flight
– apply nose up elevator
– apply nose up trim, if required
– adjust thrust and drag as required
Maximum runway slope allowed?
+- 2%
Maximum tailwind component for takeoff and landing?
15 knots
Max operating altitude?
43’100 ft
