Limitations 737 Flashcards

(31 cards)

1
Q

Maximum takeoff and landing tailwind component

A

15 kts

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2
Q

Maximum speeds

A

Observe gear and flap placards

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3
Q

Maximum operating altitude

A

41,000 ft

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4
Q

Maximum takeoff and landing altitude

A

8,400 feet

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5
Q

Maximum demonstrated takeoff and landing crosswind

A

33 kts

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6
Q

Max runway slope

A

+/- 2%

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7
Q

Maximum taxi weight

A

79,242 kg

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8
Q

Maximum takeoff weight

A

79,015 kg

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9
Q

Maximum landing weight

A

66,360 kg

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10
Q

Maximum zero fuel weight

A

62,731 kg

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11
Q

Maximum cabin differential pressure (relief valves)

A

9,1 psi

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12
Q

Engine TAI (thermal anti ice) must be on in icing conditions, except

A

Below -40 SAT

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13
Q

Autopilot and trim

A

Aileron trim is not allowed when autopilot is on

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14
Q

Minimum altitude for autopilot when takeoff

A

400 ft AGL

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15
Q

Minimum use height (MUH) for single channel autopilot operation

A

158 feet AGL

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16
Q

Level Change limitation in altitude

A

Do not use on final approach below 1,000 feet AFE (above field elevation)

17
Q

Colour of maximum and minimum limits

18
Q

Colour of caution limits

19
Q

Maximum time limit for takeoff thrust

A

2-ENG: 5 min

N-1: 10 min

20
Q

Engine ignition must be on for

A

Takeoff, landing, operation in heavy rain and anti-ice operation

21
Q

Max altitude APU + electrical load

A

Max 10,000 ft

22
Q

Max altitude APU bleed

A

Max 17,000 ft

23
Q

Max altitude APU electrical load

24
Q

APU bleed valve must be closed when:

A
  • ground air connected and isolation valve is open
  • engine no 1 bleed valve is open
  • isolation and engine no 2 bleed valves open
25
Max flap extension altitude
20,000 ft
26
Holding in icing conditions:
Is prohibited with flaps extended
27
Minimum radio altitude for speedbrakes
1,000 feet radio altitude (or above)
28
Maximum setting in flight for speed brake
Do not put lever beyond flight detent
29
Flaps 15 landing
Is prohibited when operating a normal landing
30
Lateral imbalance of fuel tanks
Must be scheduled to zero
31
Random fuel imbalance for taxi, takeoff, flight or landing
Maximum 453 kg