B737 NG Memorization Items Flashcards

1
Q

ENGINE FIRE or Engine Severe Damage or Separation

Condition: One or more of these occur:

  • Engine fire warning
  • Airframe vibrations with unusual engine indications
  • Engine separation
A
  1. Autothrottle (if engaged) … Disengage
  2. Thrust Lever (AE) … Confirm … Close
  3. Engine Start Lever (AE) … Confirm … CUTOFF
  4. Engine Fire Switch (AE) … Confirm … Pull
  5. IF the engine fire switch or ENG OVERHEAT light stays illuminated:
    - Engine fire switch … Rotate to the stop and hold 1 sec
    - IF after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated:
    ++ Engine Fire Switch … Rotate to the other stop and hold for 1 sec
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2
Q

Engine Overheat

Condition: an overheat is detected in the engine

A
  1. Autothrottle (if engaged) … Disengage
  2. Thrust Lever (AE) … Confirm … Close
  3. IF the ENG OVERHEAT light stays illuminated:
    » Go to QRC ENGINE FIRE or Engine Severe Damage or Separation checklist
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3
Q

Loss of Thrust on Both Engines

Condition: Both of these occur:

  • Both engines have a loss of thrust
  • Both ENG FAIL alerts occur

Objective: To restart at least one engine

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 950C or there is no increase in EGT within 30 sec:
    - Engine start lever (AE) … Confirm … CUTOFF, then IDLE detent
    - IF EGT again reaches 950C or there is no increase in EGT within 30 sec, repeat as needed.
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4
Q

Engine Limit or Surge or Stall

Condition: One or more of these occur

  • Engine indications are unusual
  • Engine indications are rapidly approaching or exceeding limits
  • Unusual engine noises are heard
  • There is no response to thrust lever movement

Objective: To attempt to recover normal engine operation or shut down the engine if recovery is not possible

A
  1. Autothrottle (if engaged) … Disengage

2. Thrust Lever (AE) … Confirm … Retard until indications stay within limits or the thrust lever is closed

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5
Q

APU Fire

Condition: Fire detected in the APU

A
  1. APU Fire Switch … Confirm … Pull, rotate to the stop and hold for 1 sec
  2. APU Switch … OFF
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6
Q

Aborted Engine Start

Condition: During ground start, an abort engine start condition occurs

Objective: to shut down the engine and motor it

A
  1. Engine Start Lever (AE) … CUTOFF
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7
Q

Takeoff Configuration

Condition: On the ground, the intermittent cabin altitude/configuration warning horn sounds and the TAKEOFF CONFIG lights (if installed and operative) illuminate when advancing the thrust levers to takeoff thrust.

A
  1. Assure correct airplane takeoff configuration

Check:

  • Flaps 1, 5, or 15
  • Slats not up
  • Parking Brake released
  • Trim in green band
  • Speedbrake down
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8
Q

Overspeed

Condition: Airspeed is more than Vmo/Mmo

A
  1. Reduce thrust and, if needed, adjust attitude to reduce airspeed to less than Vmo/Mmo
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9
Q

Warning Horn - Cabin Altitude or Configuration

Condition: One of these occurs:

  • In flight, and intermittent horn sounds and the CABIN ALTITUDE lights (if installed and operative) illuminate, when the cabin altitude is at or above 10,000’
  • On the ground, an intermittent horn sounds and the TAKEOFF CONFIG lights (if installed and operative) illuminate, the the takeoff configuration is not correct during takeoff
  • In flight, a steady horn sounds when the landing configuration is not correct
A
  1. IF the intermittent warning horn sounds and the CABIN ALTITUDE lights illuminate IN FLIGHT:
    - Don the oxygen masks and set the regulators to 100%
    - Establish crew communications
    - Go to the CABIN ALTITUDE WARNING or Rapid Depressurization checklist on page 2.1
    ####
  2. IF the intermittent warning horn sounds and the TAKEOFF CONFIG lights illuminate ON THE GROUND:
    - Assure correct airplane takeoff configuration
    ####
  3. IF the steady warning horn sounds IN FLIGHT:
    - Assure correct airplane landing configuration
    ####
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10
Q

Cabin Altitude Warning or Rapid Depressurization

Condition: One or more of these occur:

  • A cabin altitude exceedance
  • In flight, the intermittent cabin altitude/configuration warning horn sounds and the CABIN ALTITUDE lights (if instaleld and operatuve) illuminate
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 outflow VALVE indicates fully closed
  5. IF cabin altitude is NOT controllable:
    - passenger signs … ON
    - If the cabin altitude exceeds or is expected to exceed 14,000’:
    ++ PASS OXYGEN switch … ON
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11
Q

Airspeed unreliable

Condition: The pitch attitude is not consistent with the phase of flight, altitude, thrust and weight, or noise or low frequency buffeting is experienced

Objective: to establish the normal pitch attitude and thrust setting for the phase of flight

A
  1. Autopilot (if engaged) . . . Disengage
  2. Autothrottle (if engaged) . . . Disengage
  3. F/D Switches (both) . . . OFF
  4. Set the following gear up pitch and thrust:
    - - Flaps extended . . . 10 degrees and 80% n1
    - - Flaps up . . . 4 degrees and 75% N1
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12
Q

. Emergency descent

Condition: One or more of these occur

  • Cabin altitude cannot be controlled when the airplane is above 14,000’
  • A rapid descent is needed
A
  1. Advise flight attendant and ATC of the emergency descent
  2. Passenger signs … ON
  3. Without delay, descend to the lowest safe altitude or 10,000’, 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 Vmo/Mmo
    (If structural integrity is in doubt, limit speed as much as possible and avoid high maneuver loads)
  8. When approaching the level off altitude: smoothly lower the speedbrake lever to the down detent and level off. Add thrust and stabilize on altitude and airspeed
  9. Crew oxygen regulators . . . Normal
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13
Q

Runaway Stabilizer

Condition: Uncommanded stabilizer trim movement occurs continuously

A
  1. Control column … Hold firmly
  2. Autopilot (if engaged) … disengage
    - Do NOT re-engage the autopilot
    - Control airplane pitch attitude manually with control column and main electric trim as needed
  3. Autothrottle (if engaged) . . . Disengage
    - Do NOT reengage autothrottle
  4. IF the runaway stops
    ####
  5. IF the runaway continues:
    - Stab trim cutout switches … CUTOUT
  6. IF the runaway continues:
    - Stabilizer trim wheel … grasp and hold
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