Flight Controls/Stall Protection Flashcards
Yaw Trim is automatically accomplished when the autopilot is on.
False
Stall protection is accomplished with ___.
stick shaker and AOA limiting (higher level function of the elevator).
The ___ provides higher level functions to the flight controls.
FCM (Flight Control Module)
All the flight controls are fly-by-wire except the ___.
Ailerons
The electric PBIT begins to run when ___ and takes ___ minutes to complete.
- AC power is established
- 3
The hydraulic PBIT begins to run when ___ and takes ___ minutes to complete.
- all three hydraulic systems are pressurized
- 1
The stick shaker will active if the airplane is pitched to the PLI (Pitch Limit Indicator) and/or the airspeed indicates in the LSA (Low Speed Awareness, red) region.
True
If the spoilers go into direct mode, ground spoilers are still available but must be manually deployed.
False
The Electric PBIT can be interrupted by turning on a hydraulic pump.
True
The takeoff configuration checks that the pitch trim is in the green range. If outside the green range, “NO TAKEOFF, TRIM” will be heard when adding power for takeoff.
True
The Hydraulic PBIT can be interrupted if a flight control surface is moved.
True
In ___ mode, the flight controls have higher level functions such as AOA limiting.
Normal
The electric and hydraulic PBIT tests, when successfully completed, last for ___ hours (clock runs when the aircraft is powered up).
50
In flight, the speed brakes will automatically stow if
- Thrusts levers near TOGA (70 degrees TLS)
- airspeed is slower than 180 KIAS
- Flaps 2 or greater.
Max Flap Speeds:
- Flaps 1 : 230 KIAS
- Flaps 2 : 215 KIAS
- Flaps 3 : 200 KIAS
- Flaps 4 : 180 KIAS
- Flaps 5 : 180 KIAS
- Flaps FULL : 165 KIAS
