Limitations (# items only) Flashcards

1
Q

Max t/o & ldg tailwind

A

15 knots. 10kts in BBJ SI OPS

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2
Q

HF radios

A

Do not operate during refuelling

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3
Q

Aileron trim with autopilot engaged

A

Prohibited

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4
Q

Minimum AP engagement height

A

400ft AGL

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5
Q

Minimum single channel AP operation during approach

A

50ft AGL

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6
Q

Max/min GS angles for autoland

A

3.25/2.5

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7
Q

Autoland capabilty flap/engine requirement?

A

Flap 30 or 40, and both engines operative

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8
Q

Runway slope

A

+/- 2%

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9
Q

Max altitude, max t/o & ldg

A

41 000ft & 10 000ft

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10
Q

Max demo crosswind

A

33 knots

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11
Q

Max taxi, takeoff, landing, and ZFW

A

Max taxi 77 791
Max takeoff 77 564
Max landing 60 781
Max ZFW 57 152

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12
Q

Max cabin diff

A

9.1psi

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13
Q

Pack limitation with air engine bleed air switches ON

A

Do not operate packs in HIGH for takeoff, approach, or landing

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14
Q

Which VHF radio for primary ATC on ground?

A

The one connected to the top of fuselage antenna

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15
Q

Engine ignition must be on when?

A

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

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16
Q

Reverse thrust

A

Prohibited in flight

17
Q

APU Bleed max alt, APU electrical load max alt

A

Bleeds 17 000ft , electrical 41 000ft

18
Q

APU bleed valve must be closed when:

A

Ground air connected and isolation valve open
Engine no.1 bleed valve open
Isolation and engine no 2 bleed valves open
APU bleed valve may be open during start, but avoid engine power above idle

19
Q

Cooling required after three consecutive start attempts:

A

15 minutes

20
Q

Limitation if cargo fire protection not available

A

No cargo may be carried in forward or aft compartment

21
Q

Max flap extenstion altitude

A

20 000ft

22
Q

Holding with flaps extended in icing conditions

A

Prohibited

23
Q

Speed brake extension in flight

A

Do not extend past FLIGHT DETENT

24
Q

Large/rapid control inputs

A

Avoid, especially with combinations in pitch/roll/yaw (sideslip), as they may result in structural failure at any speed

25
Q

Use of VNAV or LNAV with altimeters referenced to QFE

A

Prohibited

26
Q

GPWS

A

Not for navigation. Do not use within 15nm of a runway not in the database.

27
Q

Weather radar operation

A

Not in a hangar or within 50ft of personnell or a fuel spill

28
Q

Fuel system max/min temp

A

Max 49°
Minimum prior to takeoff and inflight is -43°C, or 3°C above fuel freezing point, whichever is higher
Use of icing inhibitor does not change this limit.

29
Q

Dry running of centre tank fuel pump (low pressure light illuminated)

A

Prohibited

30
Q

Center tank fuel usage

A

Use until all aux fuel has been transferred

31
Q

Lateral fuel imbalance

A

Imbalance between tanks 1 and 2 must be scheduled to be zero. Random fuel imbalance must not exceed 453kg for taxi, takeoff, flight, or landing

32
Q

Fuel loading

A

Main tanks 1 and 2 must be full if centre tank contains more than 453kg. The centre and main fuel tanks must be scheduled to be full if the aux fuel system is to be loaded or contains fuel

33
Q

Brake application

A

Not until after touchdown

34
Q

Anti skid inoperative and assumed temp reduced takeoff thrust

A

Not permitted

35
Q

Max crosswind from FCTM

A
Dry 34
Wet 25
Standing water/slush 15
Snow-no melting 25
Ice-no melting 15