TECNI DATA 5

What is the fliqht control surface that gives the roll movements?. Rudder. Aileron. Elevators.

What is the flght control surface that gives the pitch movements?. Rudder. Aileron. Elevators.

What is the flight control surface that gives additional lift during takeoff and landing?. Traulıng edge flap. Leading edge slat. Leading edge flap.

How is numbered the spoilers?. 0 thru 9 from rght to left. 0 thru 9 from left to right. 1 thru 10 from left to righ.

What devices provide the pilots with contral feel ?. The feel mechan sm (ailerons & rudder) and the elevator feel computer. The feel mechanısm (elevator & rudder) and the rudder feel computer. The feel mechanism (ailerons & elevator) and the aileron feel computer.

Alternate operat on with all hydraulic power lost is. by manual control for the alerons and elevators. by the standby system for the ailerons, elevators and rudder. by manual control for the rudder only.

A stall warning system is provided to alert the pilots of an approaching stall condition. The warning is accomplished by. Applying vibrations to captain's control column only. Applying vibrations to both pilot's seats. Apphying vibrations to both pilots control columns.

The leadıng edge flaps and slats are normally aperated. by hydrulic system A. by hydraulic system B. by standby hydraulic system.

Regarding to Flight Control Switches. Normal operat ion is ON (guarded position). Normal operation is OFF (quarded position). Normal operation is STDBY RUD (guarded position).

Regarding to Alternate Flap Master Switch. Normal operation is ON (guarded position). Normal operation is OFF (guarded position). Normal operation is ARM (guarded pasition).

Which of the following indicates position of left and right outboard traling edge flaps and provides trailing edge flaps asymimetry protection circuit?. Flap Position Indicator. Flap Load Relief Indicator. Slat Position Indicator.

The aileron and aileron trim control system provides. Airplahe lateral control about the lateral axis. Airplane longitudinal control about the lateral axis. Airplane lateral control about the longitudinal axis.

The ailerons may be actuated. Hydraulically only. Mechanically only. Either hydraulically or mechanically.

Which of the following sentences is true?. One aileron is installed on each wing to provide arplane lateral control. One aileron is installed on the airplane to provide airplane lateral control. Two ilerons are installed on each wing to provide airplane longitudinal control.

Tabs are fitted to the. Ailerons and Elevators. Rudder, Ailerons and Elevator. Rudder and Elevator.

The Leading Edge devices are normally powered by Hydraulic system. System A. System A and B. System B.

At what setting(s) should the leadıng edge FLAPS be partially extended. The leading edge FLAPS should never be partially extended. 1 degree of flap. 10 degrees of flap.

The Takeoff Configuration Warning system receives signals from. The Leading Edge FLAPS and SLATS. The Leading Edge FLAPS. The Leading Edge SLATS.

With all hydraulic pressure lost, how are the controls moved?. The control surfaces are being aperated directly, not through tab movement. The control surfaces aren't being aperated directly, through tab movement. The control surfaces are being operated electrically.

In the event of a jammed aileron condition, what controls could the first Officer operate?. The spoilers only. The Krueger flap. Elevators.

What powers the yaw damper?. "B" system hydraulics. "A" system hydraulícs. "Standby system hydraulics.

What is the normal pressure source for the autoslats?. "B" system. "A" system hydraulics. "Standby" system hydraulics.

The Flap Lood Limiter. Is instal led in the trailing edge flap drive system and retracts the flaps to flaps 25 (flap lever in the 40 position) when the airspeed is in excess of 162 knots. Is installed in the trailing edge flap drive system and retracts the flaps to flaps 30 (flap lever in the 40 position) when the airspeed is in excess of l62 knots. Is installed in the leading edge flap drive system and retracts the flaps to flaps 30 (flap lever in the 40 position) when the airspeed is in excess of 162 knats.

The Yaw Damper operation results in. Rudder pedal movement. No rudder pedal movement. No rudder pedal movement provided the autopilot is engaged.

The Yaw Damper uses. Hydraulic system A pressure only. Both hydraulic systems A and B pressure. Hydraulic system B pressure only.

The Ground Spoilers are powered by. Both A and B hydraulic systems. The A hydraulic system. The B hydraulic system.

The primary flight controls are. Ailerons, Horizontal Stabilizer, Elevators and Rudder. Ailerons, Elevators and Rudder. Ailerons, Spoilers, Elevators and Rudder.

The elevator Feel Different al Pressure lght illuminated indicates that there is. Failure of an FCC channel. Normal pressure in the elevator feel computer. Excessive differential pressure in the elevator feel computer.

In the event of jammed aileron system, rotation of the co-pılot's control wheel operates the. Flight Spoilers for roll control. Aileron tabs for roll control. Ailerons for roll control.

Elevator balance tabs. Operate continuously during normal or manual reversion operations. Operate during marual reversion operations only. Are not fitted to the B737.

Tabs are fitted to the. Rudder, Ailerons and Elevator. Rudder and Elevator. Ailerons and Elevators.