Limitations (Required) (#) Flashcards
Maximum T/O and Landing Tailwind Component
15 Knots
HF use when refueling
Do not operate HF radios when refueling.
Severe Turbulent Air Penetration Speed
290 KIAS below 25,000 feet
310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet.
Wx Radar use
Avoid weather radar operation in a hangar.
Autopilot/Flight Director System
- The autopilot must not be engaged below a minimum engage altitude of 200 feet AGL after takeoff
- Autoland capability may only be used for operations into runways at or below 8400 feet airport field elevation
- Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 100 feet AGL
- With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below 100 feet AGL.
Low Visibility (HUD) Takeoff
Headwind - 25 knots
Tailwind - 15 knots
Crosswind - 20 knots
Automatic Landing
Headwind - 25 knots
Tailwind - 15 knots
Crosswind - 25 knots
- The maximum glideslope angle is 3.25 degrees
- The minimum glideslope angle is 2.5 degrees
Lowest Altitude to use FLCH?
Do not use FLCH on final approach below 1,000 feet AFE.
Engine Oil System
Oil temperature must be greater than -40° C for engine start
Reverse Thrust
- Intentional selection of reverse thrust in flight is prohibited
- Backing the airplane with use of reverse thrust is prohibited
Flight Controls
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.