Limitaciones Flashcards
Flight Maneuvering Load Acceleration Limits
in clean configuration
-1 g to +2.5 g
Flight Maneuvering Load Acceleration Limits in other configurations
0 g to +2 g
Runway slope (mean)
±2 %
Runway altitude
9200 ft
Nominal runway width
45 m
Minimal runway width
30 m
Maximum demonstrated crosswind (takeoff and landing)
38 kt (gust included)
Maximum tailwind for takeoff
15 kts or 10 kts depending on the model
Maximum tailwind for landing
15 kts or 10 kts depending on the model
maximum wind for passenger door operation is ?
65 knots
The maximum wind for FWD and AFT cargo door operation is
40 kt (or 50 kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side)
Oil limit on CEO engines
11 qts and consumes .3 qts/h
The bird is computed from IRS data and is affected by inertial errors. Usually up to….
+ - 2º