Limitations Flashcards
Maximum Altitude 787-8 and 787-9
43,100ft.
Maximum Altitude 787-10
41,000 ft.
Maximum Takeoff and Landing Tailwind
15 knots
Turbulence penetration airspeeds
Below Flight level 250: 290 knots.
At an Above flight level 250: 310 knots or Mach .84 whichever is lower.
Max Takeoff Crosswind:
40 knots.
Maximum Landing Crosswind:
40 knots.
Icing Conditions exist when:
OAT on the ground or TAT inflight is 10 degrees or less.
Minimum Autopilot engagement altitude:
200 ft. AGL
Autoland Maximum Field Elevation:
8,400 ft.
Minumum Autopilot disengagement WITHOUT land 2 or 3:
135 ft AGL.
Minimum autopilot disengagement with LAND 2 or 3 annunciated and glide slope greater than 3.5 degrees
100 ft AGL
Minimum altitude for use of flight level change on approach
1000 ft AFE
Maximum takeoff wind component HUD
Headwind: 25 knots
Crosswind: 15 knots
Tailwind: 15 knots
Maximum Crosswind SA CATI approach
15 knots
Maximum glide slop angle.
3.25 degrees
Minimum glide slope angle
2.50 degrees
Do not operate HF radio during:
Fueling Operations
Minimum oil quantity prior to start:
18 quarts
Oil temperature must be greater than _____ for engine start.
-40 degrees Celsius
Intentional selection of reverse thrust in flight is
Prohibited
Backing the airplane with use of reverse thrust is
Prohibited
Avoid RAPID and LARGE alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in?
Structural Failure at any speed, including below VA
