Limitations 737 Flashcards

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

A

Red

18
Q

Colour of caution limits

A

Amber

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

A

41,000 ft

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
Q

Max flap extension altitude

A

20,000 ft

26
Q

Holding in icing conditions:

A

Is prohibited with flaps extended

27
Q

Minimum radio altitude for speedbrakes

A

1,000 feet radio altitude (or above)

28
Q

Maximum setting in flight for speed brake

A

Do not put lever beyond flight detent

29
Q

Flaps 15 landing

A

Is prohibited when operating a normal landing

30
Q

Lateral imbalance of fuel tanks

A

Must be scheduled to zero

31
Q

Random fuel imbalance for taxi, takeoff, flight or landing

A

Maximum 453 kg