Limitations Flashcards

1
Q

Ground Wind limits for all Doors

A

40kt while opening or closing

65kt while open

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2
Q

RVSM altitude difference

A

50ft between Captain and F/O

75ft between field elevation and Capt or F/O

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3
Q

Max Taxi Weight

A

79 242kg VXA-VXU, VYZ, VZF-XZP

75 296kg VYA-VZE

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4
Q

Max Takeoff Weight

A

79 015kg VXA-VXU, VYZ, VZF-XZP

75 069kg VYA-VZE

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5
Q

Max Landing Weight

A

66 360kg

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6
Q

Max Zero Fuel Weight

A

61 688 VXA-VXU, VYA-VZE

62 731 VYZ, VZF-XZP

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7
Q

Max cabin diff pressure (relief valves)

A

9.1psi

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8
Q

Autopilot Limitations

A

Takeoff 400ftAGL

Landing (single channel) 50ftAGL

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9
Q

Autoland Limitations

A

25kt Headwind

20kt Crosswind

15kt Tailwind

2.5-3.25 Glideslope angle

Flap 30 or 40 with both engines running

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10
Q

APU Bleed and/or Electrical Load

A

10 000ft Bleed + Electrical

17 000ft Bleed only

41 000ft Electrical only

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11
Q

Max and min Fuel Temps

A

49degrees

-43degrees, or 3degrees above fuel freeze point temp

(Jet A1) = -47degrees

(Jet A) = -40degrees

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12
Q

HGS Wind Limitations

A

25kt Headwind

15kt Crosswind

10kt Tailwind

5 500ft field elevation

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13
Q

Crosswind Limitations

Takeoff

A

Dry 33kts

Wet 25kts

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14
Q

Crosswind Limitations

Land

A

Dry/Wet 37kts

30m runway - 33kts

Reduce by 5kt on wet/contaminated runways whenever asymmetric reverse thrust is used

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15
Q

Crosswind Limitations - Low visibility

A

RV/RVR < 550m - 15kts

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16
Q

Max Take and Landing Altitude

A

8 400ft pressure altitude

17
Q

Severe Turbulence Air Penetration speed

A

280KIAS/.76M whichever is lower, in Climb and Descent only.

<15 000ft 250kts Descent

18
Q

Limitations below 1000ft

A

Do not deploy speedbrakes

Do not use LVL CHG