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Memory Items 737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum runway slope

A

2%

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2
Q

Maximum take off and landing tailwind component

A

15KTS, but omanair 10KTS company limitation

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3
Q

Maximum operating altitude

A

41000’

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4
Q

Maximum altitude for take off and landing

A

8400’

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5
Q

Maximum flight operating latitudes

A

Between 82N and 82S

Except between 80 and 130 WEST longitude:
70N latitude

And between 120 and 160 EAST longitude:
60S latitude

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6
Q

Turbulent air penetration speed

A

0.76M/280 KTS, Whichever is lower

Only applicable for climb and descend

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7
Q

Do not operate HF radios during:

A

Refueling

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8
Q

Maximum allowable RVSM differences between:

  • Captain & FO in flight
  • Captain and FO on ground
  • Captain or FO and field elevation
A
  • captain and FO in flight:
    200’
  • captain and FO on ground:
    Below 5000’ elevation: 50’
    Above 5000’ elevation: 60’
  • captain or FO and field elevation:
    Below and above 5000’ elevation: 75’
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9
Q

Maximum taxi weight B738:

A

79242 KG

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10
Q

Maximum take off weight:

A

79015 KG

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11
Q

Maximum landing weight:

A

66360 KG

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12
Q

Maximum zero fuel weight

A

62731 KG

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13
Q

Maximum differential pressure

A

9.1 PSI

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14
Q

Do not operate pack switched in high for:

A

Takeoff, approach and landing
When bleed air switch is switched ON.

This limitation may be ignored by the NNC of the fire and fumes removal.

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15
Q

Autopilot limitations (3 limitations):

A
  • Do not operate aileron trim with the autopilot switched on.
  • autopilot minimum disengage height is 50’ for manual landing.
  • do not engage the autopilot after take off below 400’.
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16
Q

Autoland wind limitations:

Headwind/crosswind/tailwind

A

Headwind: 25KTS
Crosswind: 20KTS
Tailwind: 10KTS

17
Q

Autoland glide path limitations:

A

Between 2.5 till 3.25 degrees

18
Q

Flap settings for autoland:

A

Autoland only with flaps 30 or 40.

19
Q

Do not use LVL change:

A

Below 1000’ AFE

20
Q

Engine start switches must be on for:

A
  • Takeoff
  • Landing
  • Engine anti ice operation
  • In heavy rain
21
Q

Operation of assumed temperature reduced takeoff thrust not allowed when:

A

Anti skid inoperative

22
Q

Apu limitations:

A

Providing electrical and bleed air: 10000’
Providing only bleed air: 17000’
Providing only electrical load: 41000’

23
Q

APU bleed air valve limitations and start limitation:

A

Must be closed when:

  • auxiliary power connected and isolation valve is open
  • engine no 1 bleed air is open
  • isolation and engine no 2 bleed air is open

APU bleed valve may be open during engine start, but avoid engine power above idle.

After three consecutive aborted start attempts, a fifteen minute cooling period is required.

24
Q

Flaps extension maximum altitude:

A

20000’

25
Q

In flight do not extend speedbrake:

A
  • beyond flight detent

- below 1000’ RA.

26
Q

Alternate flap operation limitations

A
  • when operating the alternate flaps with the alternate flaps position switch, allow 15 seconds between the operation of the alternate flap switch again to avoid damage to the alternate flap motor clutch.
  • after a complete cycle between 0 to flaps 15 and back to 0, allow a 15 minute cooling period before operating again.
27
Q

ADIRU alignment:

A

Do not align with latitudes higher than 78 degree and 15 minutes North or south.

28
Q

Do not look ahead terrain radar (GPWS):

A

within 15 nm of takeoff, approach or landing at an airport not contained in the GPWS terrain database.

Note: Refer to Honeywell Document 060-4267-000 for airports and runways contained in the installed GPWS terrain database.

29
Q

Do not operate weather radar when:

A
  • in a hangar
  • with personnel surrounding the nose area of the aircraft.

This does not apply to the WX radar test modes

30
Q

Fuel system limitations:

Max temp
Min temp
Center tank limitation
Fuel balance 
Fuel loading 
Fuel for ground operation of electric hydraulic pump
A

Max temp: 49 degrees
Min temp: -43 degrees or 3 degrees above the minimum freezing temp of the fuel

Fuel balance: schedule to zero, but no more imbalance for taxi takeoff, cruise and landing than 453KG.

Fuel loading: when more than 453 KG in center tank, then the main tanks should be full

Fuel for ground operation of electric hydraulic pump:
760 KG in related tank

31
Q

Landing gear limitations;

A

Do not apply wheel brakes until after touchdown.

Memory Items 737 (3 decks)

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