Memory Items Flashcards

1
Q

Maximum Takeoff and Landing Tailwind Component (all planes)

A

10 kts, or as permitted by company pages

General Operation Limits
Limitations - Airplane General

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2
Q

Maximum Operating Altitude

A

41,000 ft pressure altitude

General Operation Limits
Limitations - Airplane General

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3
Q

Maximum Takeoff and Landing Altitude

A

8,400 ft pressure altitude

General Operation Limits
Limitations - Airplane General

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4
Q

Crosswind Limitation

A

33 knots

Note: the crosswind component may be further limited by low visibility takeoffs, low visibility approaches, autolands, contamination, or runway widths.

Note: Refer to 5.16.3 guidelines for Takeoff on Contaminated Runways or Landing with Braking Action less than Good

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5
Q

Severe Turbulence Penetration Speed

A

280 KIAS/ .76M, whichever is lower

Applicable to climb and descent only. During cruise, refer to 5.16.11.1 Severe Turbulence

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6
Q

Use of aileron trim with the autopilot engaged is _____.

A

Prohibited

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7
Q

Do not engage the autopilot for takeoff below ______.

A

400 ft AGL

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8
Q

For single channel operation during approach, the autopilot shall not remain engaged below _____.

A

50 ft AGL

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9
Q

Max allowable wind speeds for autoland operations

A

Headwind: 25 kts
Crosswind: 20 kts
Tailwind: 10 kts

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10
Q

Max Altitude APU Bleed + Electrical Load (in flight)

A

10,000 ft

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11
Q

Max Altitude APU Bleed

A

17,000 ft

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12
Q

Max Flaps Extended Altitude

A

20,000 ft

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13
Q

Max allowable wind speeds for HUD AIII operations

A

Headwind: 25 kts
Crosswind: 15 kts
Tailwind: 10 kts

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14
Q

For HUD AIII approach to a manual landing, AIII mode must be selected and the A/P and A/T must be disengaged prior to _____.

A

500 ft above TDZE

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15
Q

HUD AIII Landing flaps (both engines operating)

A

Flaps 30 or 40

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16
Q

HUD AIII Landing flaps (one engine inop)

A

Flaps 15

17
Q

Aborted Engine Start

A
  1. Engine start lever (affected engine) … CUTOFF

Non-Normal Checklists

18
Q

Airspeed Unreliable

A
  1. Autopilot … Disengage
  2. Autothrottle … Disengage
  3. F/D switches … 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

Non-Normal Checklists

19
Q

APU FIRE

A
  1. APU fire switch … Confirm … Pull, rotate to the stop, and hold for 1 second
  2. APU switch …. OFF

Non-Normal Checklists

20
Q

CABIN ALTITUDE WARNING or Rapid Depressurization

A
  1. Don oxygen masks and set regulators to 100%
  2. Establish crew communication

Non-Normal Checklists

21
Q

ENGINE FIRE or Engine Severe Damage or Separation

A
  1. Autothrottle …. Disengage
  2. Thrust lever (affected engine) … confirm … Close

Non-Normal Checklists

22
Q

Engine Limit or Surge Stall

A
  1. Autothrottle …. Disengage
  2. Thrust lever (affected engine) … confirm …Retard until indications stay within limits or the thrust lever is closed

Non-Normal Checklists

23
Q

LANDING CONFIGURATION

A
  1. Ensure correct airplane landing configuration

Non-Normal Checklists

24
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

Non-Normal Checklists

25
Q

Runaway Stabilizer

A
  1. Control column …. Hold firmly
  2. A/P …. Disengage
  3. A/T …. 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 A/P is disengaged:
    Do not re-engage the A/P or A/T
  7. If the runaway continutes after the A/P is disengaged:
    STAB TRIM CUTOUT switches (both) …. CUTOUT
    - If the runaway continues:
    Stabilizer trim wheel …. Grasp & Hold
26
Q

Emergency Evacuation Flow

A
  • STOP
  • CONFIGURE
  • SHUTDOWN
  • EVACUATE