Controladores yoke

Which system operates the primary flight controls. A. B. standby. A,B.

Which are the primary flight controls. Ailerons, rudder, elevators. Ailerons, elevators. Ailerons, spoilers,elevators. Ailerons, rudder.

Which controls may be operated manually without hydraulics if required. Ailerons and elevators. Rudder. elevators. ailerons.

Which hydraulic system power the secondary flight controls. B. A. A,B. Standby.

If A,B hydraulic fails, i can use the standby hydraulic system to operate the rudder?. True. False.

The secondary flight controls consist of. Trailing edge TE,flaps and leading edge LE, flaps and slats LE devices. Trailing edge TE,flaps and leading edge LE. Trailing edge TE,flaps and slats LE devices. flaps and leading edge LE, flaps and slats LE devices.

Which secondary flight control can be operated electrically if system B fails. TE flaps. LE flaps. Flaps and slats. TE slats.

The rudder becomes aerodynamically effective between... 40-60 kts. 25-60 kts. 30-60 kts. 40-65 kts.

Pitch control is provided by. 2 elevators, movable horizontal stabilizer. 1 elevator, movable horizontal stabilizer. movable horizontal stabilizer. 2 elevators and trim.

Roll control is provided by: 2 ailerons, 8 spoilers. 2 ailerons, 4 spoilers. 3 ailerons, 8 spoilers. 1 aileron, 8 spoilers.

If the aileron control system is jammed, which control is effective. FO. CAPT. Both. None.

If the spoiler control system is jammed, which control is effective. FO. CAPT. Both. None.

What happen if i move the aileron trim switches simultaneously with the AP engaged. The AP maintain heading and track. The AP is disengaged. Nothing happen. The roll control is affected.

How many spoilers are located in each wing. 8. 4. 2. 6.

When do spoilers deflect in degress during roll. 10. 8. 15. 12.

Mach trim is automatically acomplished above MACH... .615. .600. .586. .612.

What are the 2 stabilizer speed trim modes. High speed with flaps extended and low speed with flaps retracted. low speed with flaps extended and high speed with flaps retracted. low speed with flaps retracted. High speed with flaps extended.

The horizontal stabilizer control wheel have 3 modes to be operated... Trim switches control wheel, AP trim, stabilizer control wheel. AP trim, stabilizer control wheel. Trim switches control wheel,stabilizer control wheel. Trim switches control wheel, AP trim.

How does STS speed trim system help us to achieve desire airspeed. Pitch. None. Manual Thrust. Autothrotle.

Stall identification and control is enhanced by...... SMYD,EFS,STS. SMYD. EFS,STS. STS.

Above which airspeed is rudder authority limited. 137. 135. 140. 138.

In what cases are system A and B reduced 25% in rudder authority. Above 137 kts is reduced to 25% and restore below 132 kts. below 137 kts is reduced to 25% and restore below 132 kts. Above 135 kts is reduced to 25% and restore below 132 kts. Above 137 kts is reduced to 25% and restore below 130 kts.

Either yaw damper is capable of providing.... Dutch roll prevention, gust damping, and turn coordination. None. gust damping, and turn coordination. Dutch roll prevention, gust damping.

Yaw damper uses which hydraulic system. A. B. standby. A,B.

Below what altitude does the speed brakes ext light iluminate. 1000 ft AGL. 800 ft AGL. 1500 ft AGL. 2000 ft AGL.

Moving the speed brake lever beyond the flight detent causes buffeting and is prohibited in flight. True. False.

The auto speed brake system operates when: Speed brake lever arm, light iluminated, RA less than 10 ft, landing gear strut compresses,Thrust levers idle,main landing gear more than 60 kts. Speed brake lever arm, light iluminated, RA less than 15 ft, landing gear strut compresses,Thrust levers idle,main landing gear more than 60 kts. Speed brake lever arm, light iluminated, RA less than 50 ft, landing gear strut compresses,Thrust levers idle,main landing gear more than 60 kts. Speed brake lever arm, light iluminated, RA less than 10 ft, landing gear strut compresses,Thrust levers idle,main landing gear more than 88 kts.

When do TE flaps provide lift. 1-15. 40. 30. 15-40.

When do TE flaps provide lift and drag. 1-15. 40. 30. 15-40.

Normal landing flap position. 1-15. 30-40. 30. 15-40.

Autoslats are powered by..... and which flap position. B, 1-2-5. A, 1-2-5. A,B 1-2-5. All of the above.

the LE devices can be retracted by the standby hydraulic system. True. False.