MEMORY (#) Aircraft Limitations Flashcards
Maximum Takeoff/Landing Tailwind component.
15 knots
Do not operate HF radios during ____ operations.
Refuelling
Severe Turbulence Penetration Speed is defined as:
- 290KIAS below 25,000ft
- 310KIAS/0.84M (whichever is
lower) at and above 25,000ft
Avoid weather radar operation in a _____.
Hangar
Autopilot/Flight Director System
Do not use FLCH on final approach below ________ AFE.
1,000ft AFE.
Autopilot/Flight Director System
The autopilot must not be engaged below a minimum engage altitude of _______ AGL after takeoff.
200ft
Autopilot/Flight Director System
Autoland capability may only be used for operations into runways at or below _______ airport field elevation.
8,400ft
Autopilot/Flight Director System
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below _______ AGL.
135ft
Autopilot/Flight Director System
With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below ______ AGL.
100ft
Low Visibility (HUD) Takeoff
Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:
Headwind: 25 knots
Tailwind: 15 knots
Crosswind: 20 knots
Automatic Landing
Maximum wind component speeds when landing weather minima are predicated on autoland operations:
Headwind: 25 knots
Tailwind: 15 knots
Crosswind: 25 knots
Automatic Landing
The maximum glideslope angle is:
3.25 degrees
Automatic Landing
The minimum glideslope angle is:
2.5 degrees
Engines
Oil temperature must be greater than _____ for engine start.
-40° C
Engines
Intentional selection of _______ in flight is prohibited.
reverse thrust