Memory Items Flashcards

1
Q

Airspeed Unreliable

A
  1. Autopilot (if engaged) - Disengage
  2. Autothrottle (if engaged) - Disengage
  3. F/D Switches (both) - Off
  4. If necessary to stabilize aircraft, set the following gear up pitch attitude and thrust:
    Flaps Extended: 10 deg / 80% N1
    Flaps up: 4 deg / 75% N1
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2
Q

Max Crosswind Component

A

33 kts for takeoff and landing (including gusts)

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3
Q

Aborted Engine Start

A
  1. Engine Start Lever (affected engine) - Cutoff
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4
Q

Max Altitude with flaps extended

A

20,000 ft

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5
Q

Max Allowable wind speeds for HUD AIII ops
HW
XW
TW

A

HW - 25 kts,

XW - 15 kts,

TW - 10 kts

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6
Q

Landing Configuration

A
  1. Assure correct airplane landing configuration
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7
Q

APU altitude limits

A

In flight:
APU bleed and electrical load: 10,000 ft
APU bleed load: 17,000 ft

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8
Q

Max operating altitude

A

41,000 feet

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9
Q

Max takeoff and landing tailwind component

A

10 kts, or as permitted by company pages

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10
Q

Maximum Takeoff and Landing Altitude

A

8,400 feet pressure altitude

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11
Q

HUD AIII engine/flap limitations

A

Both engines operative: Flaps 30 or 40
One engine operative: Flaps 15

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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

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13
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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14
Q

For HUD AIII approach to a manual landing:

A

AIII Mode must be selected and the autopilot (A/P) and autothrottle (A/T) must be disengaged prior to 500 feet above TDZE.

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15
Q

Severe turbulent air penetration airspeed

A

280 KIAS / .76 Mach (whichever is lower)
Applicable to CLIMB AND DESCENT ONLY.
For cruise, refer to 5.16.11.1 Severe Turbulence.

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16
Q

Autopilot trim limitation

A

No aileron trim with autopilot engaged

17
Q

Single channel autopilot approach

A

Not below 50 feet AGL

18
Q

Autopilot takeoff limit

A

Do not engage below 400 feet agl

19
Q

Max allowable wind speeds for autoland
HW
XW
TW

A

HW - 25 kts

XW - 20 kts

TW - 10 kts

20
Q

Crosswind limit may be further limited by:

A

Low visibility Takeoffs,
Low visibility approaches,
Autolands,
Contamination,
Runway width

21
Q

Engine Fire
or
Engine Severe Damage or Separation

A
  1. Autothrottles (if engaged) - Disengage
  2. Thrust Lever (affected engine) - Confirm - Close
22
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
23
Q

Engine Limit
or
Surge
or
Stall

A
  1. Autothrottle (if engaged) - Disengage
  2. Thrust Lever (affected engine) - Confirm -
    Retard until indications stay within limits or the thrust Lever is closed
24
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 re-engage the autopilot or autothrottle.
  1. 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
25
Q

For crosswind landings, refer to:

A

5.16.3 Guidelines for Takeoff on Contaminated Runways or Landing with Braking Action Less than Good.

26
Q

EMERGENCY EVACUATION FLOW/PHILOSOPHY

A

STOP
CONFIGURE
SHUTDOWN
EVACUATE

27
Q

Cruise Severe Turbulence Penetration Airspeed

A

Refer to Vol 1 5.16.11.1 Severe Turbulence

28
Q

Crosswind Reference

A

Vol 1 5.16.3 Guidelines for Takeoff on Contaminated Runways or Landing with Braking Action Less than Good.