Limitations Flashcards

1
Q

L

Maximum takeoff and landing altitude

A

8,400ft

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2
Q

L

Maximum operating altitude

A

41,000ft

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3
Q

L

Maximum differential cabin pressure

A

9.1 psi

AUTO FAIL above 8.75psi

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4
Q

L

Maximum zero fuel weight

A

800- 61,688 kg

MAX- 64,818 kg

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5
Q

L

Minimum altitude for single channel autopilot use

A

158ft

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6
Q

L

Maximum and minimum glideslope for autoland

A

3.25-2.5 degrees

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7
Q

L

APU bleed + electrical load max alt

A

10,000 ft

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8
Q

L

APU bleed max alt

A

17,000 ft

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9
Q

L

APU electrical load max alt

A

41,000 ft

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10
Q

L

Max flap extension altitude

A

20,000 ft

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11
Q

L

Minimum alt for speedbrake

A

1,000 ft RA

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12
Q

L

Maximum fuel tank temperature

A

49 degrees

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13
Q

L

Minimum inflight tank temperature

A

3 degrees C above fuel freezing point or -43 degrees C, whichever is higher

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14
Q

L

Wingspan

A

800- 35.79m

MAX- 35.92m

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15
Q

L

Tail height

A

12.5m

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16
Q

L

Length

A

39.5m

17
Q

L

When can un-factored reference distances be used

A

Uncontained fire/security threat

No alternate airfields available

Delay would compromise overall safety of the flight

18
Q

L

Minimum width of pavement for 180 degree turn

A

800- 24.3m

MAX- 24.4m

19
Q

L

Max gear extension speed

A

270kts IAS / 0.82m

20
Q

L

Max gear extended speed

A

320kts IAS / 0.82m

21
Q

L

Max gear retract speed

A

235kts IAS

22
Q

L

Maximum wind speeds dual channel approach CAT II/III

A

Headwind 25 kts
Crosswind 20 kts
Tailwind 10kts

23
Q

L

Maximum landing weight

A

800- 65,317 kg

MAX- 68,175 kg

24
Q

L

Wingtip height

A

6.4m

25
Q

L

Minimum obstacle distance from nose when turning away

A

800- 7.4m

MAX- 7.1m

26
Q

L

Minimum obstacle distance from wingtip when turning away

A

800- 5.4m

MAX- 4.6m