Memory Items Flashcards

1
Q

Max tailwind

A

10 knots

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2
Q

Max operating altitude

A

41,000

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3
Q

Max takeoff and landing altitude

A

8,400’

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4
Q

Crosswind limit

A

33 knots

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5
Q

Speed for turbulent air penetration

A

280 or 0.76

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6
Q

Do not engage the autopilot of takeoff until

A

400’

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7
Q

On a single channel approach, autopilot cannot be used below

A

50’

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8
Q

Max wind for auto land

A

Headwind 25
Crosswind 20
Tailwind 10

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9
Q

Max altitude for APU

A

Bleed air and electrical load- 10,000’

Bleed air only- 17,000’

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10
Q

Max altitude for flap extension

A

20,000’

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11
Q

Maximum allowable wind speeds for HUD AIII operations:

A

Headwind- 25
Crosswind- 15
Tailwind- 10

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12
Q

Aborted Engine Start

A
  1. Engine start lever (affected engine) . . . . CUTOFF
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13
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 the aircraft, 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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14
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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15
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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16
Q

Engine Fire or Engine Severe Damage or Separation

A
  1. Autothrottle (if engaged)………..Disengage

2. Thrust lever (affected engine)………Confirm……Close

17
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
18
Q

Landing Configuration

A

Assure correct airplane landing configuration

19
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
20
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 runaway trim stops………do not re-engage the autopilot or auto throttle
  7. If the runaway continues:
    Stab trim Cutout switches(both) ……………. CUTOUT
    If the runaway continues:
    Stabilizer trim wheel ………. Grasp and hold
21
Q

Evacuation Philosophy

A

STOP
CONFIGURE
SHUTDOWN
EVACUATE

22
Q

Autopilot aileron trim limitation

A

Use of aileron trim with the autopilot engaged is prohibited.

23
Q

Max takeoff and landing tailwind component

A

10 knots, or as permitted by the Company Pages

24
Q

HUD AIII mode 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

  • Landing flaps 30 or 40 with both engines operative
  • Landing flaps 15 with one engine operative