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* B77F Caro MEMORY ITEMS > B777 Red Box & Memory Items > Flashcards

B777 Red Box & Memory Items Flashcards

1
Q

ABORTED ENGINE START L, R

Condition: On the ground, an aborted engine start is needed

A
  1. FUEL CONTROL SWITCH (AFFECTED SIDE) - CUTOFF
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2
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 RPM with the autostart switch to OFF

A
  1. FUEL CONTROL SWITCH (AFFECTED SIDE)

- CUTOFF

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3
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 LIMITS OR THE THRUST LEVER IS AT IDLE
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4
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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5
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:
    Engine fire switch…….. Rotate to the other stop and hold for 1 second
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6
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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7
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:
    - ANNOUNCE „Emergency descent“
    - PASS OXYGEN SWITCH………….PUSH TO ON AND HOLD FOR 1 SECOND
    - WITHOUT DELAY: descent to the lowest safe altitude or 10.000ft, whichever is higher
To descend:
           Move thrust lever to idle
           Extend speedbrakes
           If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads
           Descend at Vmo / Mmo
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8
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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9
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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10
Q

WINDSHEAR ESCAPE MANEUVER

Manual Flight

A
  1. call „WINDSHEAR TOGA“
  2. Disconnect the A/P
  3. Push either TO/GA switch
  4. Aggressively apply maximum thrust
  5. Disconnect Autothrottle
  6. Simultaneously roll wings level and rotate toward an initial pitch attitude of 15 deg
  7. Retract speedbrakes
  8. 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

WINDSHEAR ESCAPE MANEUVER

Auto Flight

A
  1. Call „WINDSHEAR TOGA“
  2. Press either TO/GO switch
  3. Verify TO/GA mode annunciation
  4. Verify GA thrust
  5. Retract speedbrakes
  6. Monitor system performance
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12
Q

GPWS CAUTION

A

Correct the flight path or the airplane configuration

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13
Q

GPWS ALERTS
„Pull-Up”
„Terrain, Terrain, Pull-Up”
„Obstacle, Obstacle, Pull-Up”

A
  • Call „TERRAIN TOGA“
  • Disengage Autopilot
  • Disconnect Auto Throttles
  • Aggressively apply maximum thrust
  • Roll Wings Level and Rotate to an initial pitch attitude of 20 deg.
  • Retract Speedbrakes
  • If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet.
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14
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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15
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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15
Q

REJECTED TAKEOFF Captain

A

Call “STOP” and
Without delay:
- Close the thrustlevers
- Disconnect the autothrottles
- Apply maximum reverse thrust consistent with conditions
- Verify the speedbrakes are up
- Apply maximum manual wheel brakes or
verify proper operation of RTO autobrakes

  • Continue max braking until certain the airplane will stop on the runway
  • set the parking brake
  • call „REMAIN SEATED, REMAIN SEATED“
17
Q

SMOKE/FIRE OR FUMES

A
  1. If needed:

Don oxygen masks and smoke goggles

18
Q

Predictive Windshear warning during approach

A

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

19
Q

HIGH NOSE RECOVERY

A
  • Disconnect A/P
  • Disconnect A/T
  • Apply nose down elevator. Apply as much elevator as needed to obtain a nose down pitch rate
  • 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
20
Q

NOSE DOWN RECOVERY

A
  • Disconnect A/P
  • Disconnect A/T
  • Recover from stall, if needed
  • Roll in the shortest direction to wings level. If bank angle is more than 90 deg, unload and roll
  • Complete the recovery
      • apply nose up elevator
      • apply nose up trim, if required
      • adjust thrust and drag as required
21
Q 
Airspeed unreliable 
cruise flight (AL recommendation)
A

Pitch 2.5 degree

Thrust 82.5 %

22
Q 
Dual engine failure with airspeed unreliable 
cruise flight (AL recommendation)
A

Pitch 0 degree

23
Q

Unreliable airspeed table - one engine shut down

A

Multiply N1 values by 1.3

24
Q

TCAS

A

Call „TCAS MY CONTROLS“

* B77F Caro MEMORY ITEMS (1 decks)

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