B777 Memory Items Flashcards
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
Maximum takeoff and landing altitude?
8’400 ft
Max ZFW?
237’600 kg
Max Ramp weight?
352’400 kg
Max TOW?
351’500 kg
Max LW?
251’200 kg
What is the severe turbulence penetration speed?
- 270 kts below 25’000 ft
- 280 kts or M0,82 whichever is lower above 25’000 ft
Maintain minimum 15 kts above MMS at all altitudes when airspeed is below M0,82
Max wind speed for operating cargo doors?
40 kts
Over what wind speed should doors not be kept open ?
When wind gusts are above 65 kts
Maximum differential cabin pressure?
9,1 psi
Maximum cabin differential pressure for takeoff and landing?
0,11 psi
Maximum glideslope angle for autoland?
3,25 degrees
Minimum glideslope angle for autoland?
2,5 degrees
Max altitude with flaps extended?
20’000 ft
