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B-777 MEMORY ITEMS > B777 Memory Items > Flashcards

B777 Memory Items Flashcards

1
Q

CABIN ALTITUDE

A
  1. DON THE OXYGEN MASKS
  2. ESTABLISH CREW COMMUNICATIONS
  3. CHECK THE CABIN ALTITUDE AND RATE
  4. IF THE CABIN ALTITUDE IS UNCONTROLLABLE:
    - PASS OXYGEN SWITCH………….PUSH TO ON AND HOLD FOR 1 SECOND

– WITHOUT DELAY: EMERGENCY DESCENT-ACCOMPLISH

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2
Q

DUAL ENG FAIL / STALL

A
  1. FUEL CONTROL SWITCHES (BOTH)
    - CUTOFF, then RUN
  2. RAM AIR TURBINE SWITCH
    - PUSH AND HOLD FOR 1 SECOND
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3
Q

STABILIZER
(Condition: One of these occurs:
- Stabilizer movement without a signal to trim
- The stabilizer is failed)

A
  1. STAB cutout switches (both)
    - CUTOUT
  2. Do not exceed the current airspeed
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4
Q

AIRSPEED UNRELIABLE

A
  1. AUTOPILOT DISENGAGE SWITCH
    - PUSH
  2. A/T ARM SWITCHES (BOTH)
    - OFF
  3. F/D SWITCHES (BOTH)
    - OFF
  4. SET THE FOLLOWING GEAR UP PITCH ATTITUDE AND THRUST:
    - FLAPS EXTENDED: 10 DEGREES AND 85% N1
    - FLAPS UP: 4 DEGREES AND 70% N1
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5
Q

ENG LIM / SURGE / STALL L, R

A
  1. A/T ARM SWITCH (AFFECTED SIDE)………CONFIRM
    - OFF
  2. THRUST LEVER (AFFECTED SIDE)…………CONFIRM
    - RETARD UNTIL ENGINE INDICATIONS STAY WITHIN APPROPRIATELIMITS OR THE THRUST LEVER IS AT IDLE
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6
Q

ENG SVR DAMAGE / SEP L, R
(Condition: One or more of these occur:
- Airframe vibration with abnormal engine indications
- Engine separation)

A
  1. A/T ARM switch (affected side)………confirm
    - OFF
  2. Thrust lever (affected side)…………confirm
    - Idle
  3. FUEL CONTROL switch (affected side)….confim
    - CUTOFF
  4. Engine fire switch (affected side)……………confirm
    - PULL
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7
Q

FIRE ENG L, R
(Condition: Fire is detected in the engine)

A
  1. A/T ARM switch (affected side)…………….confirm
    - OFF
  2. Thrust lever (affected side)………………….confrim
    - Idle
  3. FUEL CONTROL switch (affected side)……………confirm
    - CUTOFF
  4. Engine fire switch (affected side)………….confrim
    - Pull
  5. 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
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8
Q

ABORTED ENGINE START L, R
(Condition: During a ground start, an abort start condition occurs)

A
  1. FUEL CONTROL SWITCH (AFFECTED SIDE)
    – CUTOFF
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9
Q

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

A
  1. FUEL CONTROL SWITCH (AFFECTED SIDE)
    - CUTOFF
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10
Q

WINDSHEAR ESCAPE MANEUVER
(Manual Flight)

A
  1. Push either TO/GA switch
  2. Aggressively apply maximum thrust
  3. Verify TO/GA mode annunciation
  4. Disconnect Autothrottle
  5. Simultaneously roll wings level and rotate toward an
    initial pitch attitude of 15 deg
  6. Retract speedbrakes
  7. 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

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11
Q

“MICROBURST ALERT”

A

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.

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12
Q

GPWS ALERTS
“Pull-Up” / “Terrain, Terrain, Pull-Up” / “Obstacle, Obstacle, Pull-Up” /

A
  • 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.
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13
Q

GPWS ALERTS Pilot Monitoring

A

– 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.

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14
Q

REJECTED TAKEOFF Captain

A

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

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15
Q

SMOKE/FIRE OR FUMES

A
  1. If needed:
    Don oxygen masks and smoke goggles
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16
Q

WINDSHEAR ESCAPE MANEUVER
(Auto Flight)

A
  1. Press either TO/GO switch
  2. Follow FD commands if AP not engaged
  3. Verify TO/GA mode annunciation
  4. Retract speedbrakes
  5. Engage A/P (if not already engaged)
  6. Monitor system performance
17
Q

Predictive Windshear warning during approach

A

Call “Go-around” and perform a normal go-around

18
Q

GPWS CAUTION

A

Correct the flight path or the airplane configuration

19
Q

GPWS WARNING

A
  • 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

20
Q

HIGH NOSE RECOVERY

A
  • 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
21
Q

NOSE DOWN RECOVERY

A
  • 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
22
Q

Maximum runway slope allowed?

A

+- 2%

23
Q

Maximum tailwind component for takeoff and landing?

A

15 knots

24
Q

Max operating altitude?

A

43’100 ft

25
Q

Maximum takeoff and landing altitude?

A

8’400 ft

26
Q

Max ZFW?

A

237’600 kg

27
Q

Max Ramp weight?

A

352’400 kg

28
Q

Max TOW?

A

351’500 kg

29
Q

Max LW?

A

251’200 kg

30
Q

What is the severe turbulence penetration speed?

A
  • 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
31
Q

Max wind speed for operating cargo doors?

A

40 kts

32
Q

Over what wind speed should doors not be kept open ?

A

When wind gusts are above 65 kts

33
Q

Maximum differential cabin pressure?

A

9,1 psi

34
Q

Maximum cabin differential pressure for takeoff and landing?

A

0,11 psi

35
Q

Maximum glideslope angle for autoland?

A

3,25 degrees

36
Q

Minimum glideslope angle for autoland?

A

2,5 degrees

37
Q

Max altitude with flaps extended?

A

20’000 ft

B-777 MEMORY ITEMS (1 decks)

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