Memory Actions Flashcards

(13 cards)

1
Q

Takeoff Configuration

A
  1. Assure correct airplane takeoff configuration
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2
Q

Landing Configuration

A
  1. Assure correct airplane landing configuration
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3
Q

APU Fire

A
  1. APU Fire Switch
    ……CONFIRM…………………………..PULL,
    rotate to the stop,
    and hold for 1 second
  2. APU switch
    …………………………………………………..OFF
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4
Q

Aborted Engine Start

A
  1. Engine Start Lever (affected engine)
    …………………………………………….CUTOFF
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5
Q

Airspeed Unreliable

A
  1. Autopilot (if engaged)
    ……………………………………….DISENGAGE
  2. Autothrottle (if engaged)
    ……………………………………….DISENGAGE
  3. F/D switches (both)
    …………………………………………………..OFF
  4. Set the following gear up pitch attitude and thrust:
  • Flaps extended……….10° and 80% N1
  • Flaps up…………………..4° and 75% N1
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6
Q

Engine Fire OR Engine Severe Damage or Seperation

A
  1. Autothrottle (if engaged)
    ……………………………………….DISENGAGE
  2. Thrust Lever (affected engine)
    ……………………….CONFIRM………CLOSE
  3. Engine Start Lever (affected engine)
    ………………………CONFIRM………CUTOFF
  4. Engine Fire switch (affected engine)
    …………………….CONFIRM…………….PULL
    To manually unlock the engine fire switch, press the override and pull.
  5. IF the engine fire switch or ENG OVERHEAT light is illuminated:
    - Engine Fire switch (affected engine)
    …………………………………………….ROTATE
    to the stop and hold
    for 1 seconds
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7
Q

Engine Overheat

A
  1. Autothrottle (if engaged)
    ……………………………………….DISENGAGE
  2. Thrust Lever (affected engine)
    ……………………CONFIRM…………..CLOSE
  3. IF the ENG OVERHEAT light stays illuminated:
    - Go to the ENGINE FIRE or ENGINE SEVERE DAMAGE or SEPERATION Checklist
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8
Q

Engine Limit or Surge or Stall

A
  1. Autothrottle (if engaged)
    ……………………………………….DISENGAGE
  2. Thrust Lever (affected engine)
    …CONFIRM……………………………RETARD
    until engine indications
    stay within limits or the
    thrust lever is closed
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9
Q

Loss of Thrust on both Engines

A
  1. Engine Start switches (both)
    ……………………………………………………FLT
  2. Engine Start levers (both)
    …………………………………………….CUTOFF
  3. When EGT decreases:
    - Engine Start Levers (both)
    …………………………… ……….IDLE DETENT
  4. IF EGT reaches a redline or there is no increase in EGT within 30 seconds:
    - Engine Start Lever (affected engine)
    ………CONFIRM……………………..CUTOFF,
    then IDLE DETENT

If EGT again reaches a redline or there is no increase in EGT within 30 seconds, repeat as needed

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10
Q

Runaway Stabilizer

A
  1. Control Column
    ……………………………………HOLD FIRMLY
  2. Autopilot (if engaged)
    ……………………………………….DISENGAGE
  3. Autothrottle (if engaged)
    ……………………………………….DISENGAGE
  4. Control Column and thrust levers
    ………………………….CONTROL AIRPLANE
    PITCH ATTITUDE
    AND AIRSPEED
  5. Main Electric Stabilizer Trim
    …………………………….REDUCE CONTROL
    COLUMN FORCES
  6. IF the runaway stops after the autopilot is disengaged:
    - Do not reengage the autopilot or autothrottle
  7. IF the runaway continues after the autopilot is disengaged:
    - STAB TRIM cutout switches (both)
    ……………………………………………CUTOUTIF the runaway continues
    - Stabilizer Trim wheel
    ……………………………..GRASP AND HOLD
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11
Q

Warning Horn (intermittent) or Warning Light - Cabin Altitude or Takeoff Configuration

A
  1. If the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates in flight at an airplane flight altitude above 10 000 feet MSL:
    - Don the oygen masks and set the regulators to 100%
    - Establish crew communications
  2. If the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates on the ground when advancing the thrust levers to takeoff thrust:
    - Assure correct airplane takeoff configuration
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12
Q

CABIN ALTITUDE WARNING or Rapid Depressurization

A
  1. Don oxygen masks and set regulators to 100%
  2. Establish crew communications
  3. Pressurization mode selector
    …………………………………………………MAN
  4. Outflow valve switch
    ……………………………………………….HOLD,
    in CLOSE until the outflow valve indication shows fully closed.
  5. If cabin altitude is uncontrollable:
    - Passenger signs………………………….ON
    - PASS OXYGEN switch………………….ON
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13
Q

Emergency Descent

A
  1. Announce the emergency descent. The PF will advise the cabin crew, on the PA system, of impending rapid descent. The pilot monitoring will advise ATC and obtain the area altimeter setting.
  2. Passenger signs
    ……………………………………………………ON
  3. Without delay, descend to the lowest safe altitude or 10 000 feet, whichever is higher.
  4. Engine Start switches (both)
    ………………………………………………..CONT
  5. Thrust Levers (both)
    …………………………………………….REDUCE
    thrust to minimum or
    as needed for anti-ice
  6. Speedbrake
    …………………………………FLIGHT DETENT
  7. Set target speed to MMO/ VMO
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