Limitations -9 (# items) Flashcards
This card deck presents the limitations and operational information listed in the FCOM Limitations Chapter and that must be memorized (memory items) and are marked with a (#) symbol.
Maximum Takeoff and Landing Tailwind Component is ____.
15 knots
Are HF radios allowed during refueling?
No. Do not operate HF radios when refueling.
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.
Use of weather radar operation in a hangar…
Avoid weather radar operation in a hangar.
The autopilot must not be engaged below a minimum engage altitude of ________ after takeoff.
200 feet AGL
Autoland capability may only be used for operations into runways _____________ airport field elevation.
At or below 8400 feet
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below _________.
135 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
Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations (headwind, crosswind, tailwind):
Headwind: 25kt
Crosswind: 20kt
Tailwind: 15kt
Automatic Landing
Maximum wind component speeds when landing weather minima are predicated on autoland and CAT II/III operations (headwind, crosswind, tailwind):
Headwind: 25kt
Crosswind: 25kt
Tailwind: 10kt
The maximum glideslope angle is _____ degrees.
3.25
The minimum glideslope angle is _____ degrees.
2.5
Do not use FLCH on final approach ___________.
below 1,000 feet AFE
Oil temperature must be greater than ______ for engine start.
-40° C
What AFM limitations should we observe regarding the use of reverse thrust?
- Intentional selection of reverse thrust in flight is prohibited.
- Backing the airplane with use of reverse thrust is prohibited.
What AFM limitation should we observe regarding the use of 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.
