Limits Flashcards
Max operating alt
42000
Max slope
2%
Max takeoff and landing alt
13500
Max takeoff and landing tailwind
15 kts
Turbulent air pen speed
290 or 0.78M, whichever is less
No latitudes greater than
87 degrees
Max altimeter difference for RVSM
200’
Max altimeter difference at sea level
40’
Max difference between altimeter and field elevation
75’
Do not operate WX radar within
50’ of personnel or fuel
Max taxi weight
256000 lbs
Max takeoff weight
255,000 lbs
Max landing weight
210,000 lbs
Max zero fuel weight
187,400 lbs
Max cabin differential
8.6 +- 0.05
Max cabin differential during climb
8.6 +- 0.10
Max cabin differential for takeoff and land
0.125
Equipment cooling for more than 20 min at 34-40C.
One forward and one aft door open OR one AC pack
Equipment cooling for more than 20 min at 41-49C
One AC pack
Equipment cooling for more than 20 min at more than 49C
Two AC packs
After takeoff, autopilot not below
200’
No autopilot below 100’ at fields above
8400
Max Autoland headwind or crosswind
25
Max Autoland tailwind
15
Use CONT ignition in
Severe turbulence
Max fuel temp
49C
Min fuel temp
Higher of 3 degrees above freeze or -45C
With less than full wing tanks and zero fuel limits applied, how much fuel can be in center tank
2000 lbs
Transfer of aux fuel shall begin before center tank reaches
39,300 lbs
Before aux fuel transfer
Flaps must be retracted
APU starter duty cycle
3 starts in 60 min (5 min cooling between each)
Max altitude for flaps
20,000’
IRU alignment must not be attempted
Above 78 degrees N or S
GPWS terrain display prohibited within
15 NM of an airport not in the database
SDS hazard zone
230’ from tail
Ground operating of SDS limited to 30 min with
Temp above 44F
SDS operating envelope
45,000’
-54C to plus 55C
SDS max maneuver rates
10 degrees per sec roll, pitch, or yaw
