737 Quick Reference Checklist (Memory Items) Flashcards

1
Q

Aborted Engine Start

A

Engine Start Lever (affected engine) — CUTOFF

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2
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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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

Cabin Altitude Warning or Rapid Depressurization

A

1: Don the oxygen masks and set regulators to 100%
2: Establish Crew communications.

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5
Q

Cargo Fire (Main)

A

1: Don oxygen masks and set regulators to 100%, as needed.
2: Don smoke goggles, as needed.
3: Close the flight deck door. This step prevents smoke or fumes contamination from other compartments.
4: Establish Crew and supernumerary cabin communications

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6
Q

ENGINE FIRE or Engine Severe Damage or Separation

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 — Rotate to the stop and hold for 1 second
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 second

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7
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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8
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 CHECKLIST on page (-400 8.3) (-800 8.8)

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9
Q

LANDING CONFIGURATION

A

1: Assure correct airplane landing configuration

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10
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 = (-800) / (-400 = 930C) 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 = (-800) / (-400 = 930C) or there is no increase in EGT within 30 seconds, repeat as needed.

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11
Q

Runaway Stabilizer

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 re-engage the autothrottle.
4: IF the runaway STOPS after the autopilot is DISENGAGED (checklist complete)
5: IF the runaway CONTINUES after the autopilot is disengaged:
STAB TRIM CUTOUT switches (both) — CUTOUT
IF the runaway CONTINUES:
Stabilizer trim wheel — grasp and hold

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12
Q

TAKEOFF CONFIGURATION

A
  1. Assure correct airplane takeoff configuration
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13
Q

Uncommanded Roll (-400)

A

1: Autopilot (if engaged) — Disengage
2: Maintain Control of the airplane with all available flight controls. If roll is uncontrollable, immediately reduce pitch/angle of attack and increase airspeed.
Do not attempt to maintain altitude until control is recovered.
3: Autothrottle (If engaged) — disengage
4: Verify thrust is symmetrical

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14
Q

WARNING HORN (INTERMITTENT) or WARNING LIGHT - CABIN ALTITUDE or TAKEOFF CONFIGURATION

A

1: IF the intermittent warning sound horn sounds or the CABIN ALTITUDE light illuminates IN FLIGHT at an airplane flight altitude above 10,000 feet MSL:

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 (checklist complete).

2: IF the intermittent warning horn sounds or the TAKEOFF CONFIG light illuminates ON THE GROUND when advancing the thrust levers to takeoff thrust:
Assure correct airplane takeoff configuration (checklist complete)

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15
Q

Flight Controls AFM Limitation

A

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.

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