Limitations # Flashcards
(18 cards)
Severe Turbulent Air Penetration speed
280 KIAS / .76M, whichever is lower
Maximum Takeoff and Landing Tailwind
Component
Tailwind 15 knots #
Takeoff 15 knots #
HF Radio during refueling
Do not operate #
Aileron trim with the autopilot engaged
Use of aileron trim with the autopilot engaged is prohibited.#
Do not engage the autopilot for takeoff below
Do not engage the autopilot for takeoff below 400 feet AGL #
For single channel operation during approach, the autopilot shall not remain
engaged below
For single channel operation during approach, the autopilot shall not remain
engaged below 50 feet AGL.#
Autoland maximum wind
- Headwind 25 knots
- Crosswind 20 knots
- Tailwind 15 knots.
Autoland max and min glideslope
3.25 max and 2.5 min
Autoland flaps and engine req
Autoland capability may only be used with flaps 30 or 40 and both engines
operative.
Autoland landing alt
Autoland capability may only be used to runways at or below 8,400 ft pressure
altitude.
LVL CHG on final approach
Do not use LVL CHG on final approach below 1000 feet AFE #
Reverse Thrust
Intentional selection of reverse thrust in flight is prohibited.
APU bleed + electrical load - max alt
APU bleed + electrical load: max
alt 10,000 ft. #
APU bleed: max alt
Airplanes operating under FAA Rules: Ground only - APU bleed + electrical
load: max alt ?
# APU bleed: max alt ?
# APU electrical load: max alt ?
APU bleed: max alt 17,000 ft.
Airplanes operating under FAA Rules: Ground only - APU bleed + electrical
load: max alt 15,000 ft.
# APU bleed: max alt 17,000 ft.
# APU electrical load: max alt 41,000 ft.
The maximum altitude with flaps extended is
The maximum altitude with flaps extended is 20,000 ft. #
Holding in icing conditions with flaps extended is
Holding in icing conditions with flaps extended is prohibited.#
Avoid ___ and ___ alternating control inputs, especially in combination with
large changes in __, __, or __ (e.g. large side slip angles) as they may result
in structural failure at any speed, including below VA.
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.#
Do not deploy the speedbrakes in flight at radio altitudes less than
Do not deploy the speedbrakes in flight at radio altitudes less than 1,000 feet. #
