Limitations Flashcards
L
Maximum takeoff and landing altitude
8,400ft
L
Maximum operating altitude
41,000ft
L
Maximum differential cabin pressure
9.1 psi
AUTO FAIL above 8.75psi
L
Maximum zero fuel weight
800- 61,688 kg
MAX- 64,818 kg
L
Minimum altitude for single channel autopilot use
158ft
L
Maximum and minimum glideslope for autoland
3.25-2.5 degrees
L
APU bleed + electrical load max alt
10,000 ft
L
APU bleed max alt
17,000 ft
L
APU electrical load max alt
41,000 ft
L
Max flap extension altitude
20,000 ft
L
Minimum alt for speedbrake
1,000 ft RA
L
Maximum fuel tank temperature
49 degrees
L
Minimum inflight tank temperature
3 degrees C above fuel freezing point or -43 degrees C, whichever is higher
L
Wingspan
800- 35.79m
MAX- 35.92m
L
Tail height
12.5m
L
Length
39.5m
L
When can un-factored reference distances be used
Uncontained fire/security threat
No alternate airfields available
Delay would compromise overall safety of the flight
L
Minimum width of pavement for 180 degree turn
800- 24.3m
MAX- 24.4m
L
Max gear extension speed
270kts IAS / 0.82m
L
Max gear extended speed
320kts IAS / 0.82m
L
Max gear retract speed
235kts IAS
L
Maximum wind speeds dual channel approach CAT II/III
Headwind 25 kts
Crosswind 20 kts
Tailwind 10kts
L
Maximum landing weight
800- 65,317 kg
MAX- 68,175 kg
L
Wingtip height
6.4m
L
Minimum obstacle distance from nose when turning away
800- 7.4m
MAX- 7.1m
L
Minimum obstacle distance from wingtip when turning away
800- 5.4m
MAX- 4.6m
