Memory Items Flashcards

(26 cards)

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)

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
Runaway Stabilizer
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
Emergency Evacuation Flow
- STOP - CONFIGURE - SHUTDOWN - EVACUATE