Limitations Flashcards
Maximum Takeoff and Landing Tailwind Component
15 knots
Do not operate HF radios when refueling.
Do not operate HF radios when refueling.
Severe Turbulent Air Penetration Speed
Severe turbulent air penetration speed (in severe turbulence) is defined as:
- 290 KIAS below 25,000 feet
- 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet.
Radar operation
Avoid weather radar operation in a hangar, or within 50 feet of fueling operations or a fuel spill.
Avoid weather radar operation when personnel are within the area normally enclosed by the aircraft nose radome.
Note: The hangar recommendation does not apply to the weather radar test mode.
AP ENGAGE
The autopilot must not be engaged below a minimum engage altitude of 200 feet AGL after takeoff.
Auto Land Capability
Autoland capability may only be used for operations into runways at or below 8400 feet airport field elevation.
Without Land 2/3
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 135 feet AGL.
Land 2/3 with glide slope greater than 3.25
With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below 100 feet AGL.
If the glidepath angle for approach is greater than 3.77 degrees, the autopilot must be disengaged no later than 50 feet below DH/MDA.
Low Visibility (HUD) Takeoff
Headwind - 25 knots
Tailwind- 15 knots
Crosswind - 20 knots
Automatic Landing
Headwind - 25 knots
Tailwind- 15 knots
Crosswind - 25 knots
Glide Slope angle
The maximum glideslope angle is 3.25 degrees.
The minimum glideslope angle is 2.5 degrees.
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) they may result in structural failure at any speed, including below V A .
