EXAMEN AVA ATA 27

IN THE SLAT/FLAP SYSTEM: THE PCU GEARS POSITION AND TIP TRANSMISION POSITION OF THE SYSTEM IS MEASURE BY THE: WTB. PPU. POB.

ON WHICH OF THE FOLLOWING AXIS ROTATE THE AIRCRAFT IF THE ELEVATORS ARE USED?. LONGITUDINAL AXIS. LATERAL AXIS. VERTICAL AXIS.

NORMALLY ROLL CONTROL IS ACHIEVED BY: 3 Spoiler Elevator Computers (SEC) controlling spoilers 2 to 4 and the ailerons. ELAC's and SEC's controlling spoilers 1 to 4 and the ailerons. ELAC's and SEC's controlling spoilers 2 to 5 and the ailerons.

HOW MANY RUDDER SERVOCONTROLS HAS THE A320?. 4 Servo controls. 2 Servo controls. 3 Servo controls.

THE SLAT SYSTEM WING TIP BRAKES (WTB) ARE INSTALLED: At the wing tip. At the wing root. n the slat PCU.

THE RESET OF WING TIP BRAKES (WTB) IS POSSIBLE: In flight, by making any new selection with the control lever. In flight, by making a reverse selection with the control lever. On ground only.

IF SLAT AND FLAP LEVER POSITION IS IN POSITION 1, THESE ARE IN: Slats in 22 and flaps in 20 degrees. Slats in 18 and flaps in 15 degrees. Slats in 18 and flaps in 10 degrees.

THE SLAT AND FLAP SYSTEM CONSISTS OF: One Slat/Flap Control lever, one Slat Flap Control Computer (SFCC), one Slat/Flap Power Control Unit (PCU). One Slat/Flap Control Lever, two SFCC's, one Slat PCU and one Flap PCU. One Slat Control Lever, one Flap Control Lever, two SFCC's, one Slat PCU and one Flap PCU.

IF SLAT AND FLAP LEVER POSITION IS IN POSITION 3 THERE ARE IN: Slats in 22 and flaps in 20 degrees. Slats in 22 and flaps in 15 degrees. Slats in 27 and flaps in 25 degrees.

WHICH OF THE FOLLOWING ARE FCC?. ABCU & BSCU. 2 LGCIU. 2 ELAC.

HOW MANY SLATS ARE THERE IN THE A320 FAMILY?. 10 alum alloys slat numbers from the tip to the root. 10 composites material slat numbers from the root to the tip. 10 alum alloys slat number from the root to the tip.

ON WHICH OF THE FOLLOWING AXIS ROTATE THE AIRCRAFT IF THE RUDDER IS USED?. LONGITUDINAL AXIS. LATERAL AXIS. VERTICAL AXIS.

HOW MANY SPEED BRAKES SERVOCONTROLS HAS THE A320?. 10 Servo controls. 8 Servo controls. 6 Servo controls.

THE REASONS THAT OPERATED THE WTB: Assymetric, overspeed, run away, uncommanded movement. Assymetric, engine fail, run away, uncommanded movement. Dutch roll, overspeed, run away, uncommanded movement.

WHAT IS THE MEANING OF AILERON DROOP?. Ailerons extends as other slat. Ailerons extends as other flap. Ailerons retracts because they can not extended.

WHICH ARE THE REASONS THAT MAKES THE RUDDERS TO WORK IN FLIGHT?. Dutch roll, 1 engine failure, cross winds and uncommanded movement. Assymetric, overspeed, run away, uncommanded movement. Dutch roll, 1 engine failure, cross winds and coordinated turn.

WHERE IS LOCATED THE THS TRIM WHEELS CONTROL?. CENTER PEDESTAL. OVERHEAD PANEL. MAIN INSTRUMENT PANEL.

WHERE IS LOCATED THE FLIGHT CONTROL PANEL (PUSH BOTTONS) USED TO TURN OFF/ON & RESET SOME FCC?. CENTER PEDESTAL. OVERHEAD PANEL. MAIN INSTRUMENT PANEL.

WHICH COMPONENT IS USED TO MOVE THE THS?. THS SERVOCONTROLS. THS ACTUATOR. 1 PCU FOR THE THS.

ON WHICH OF THE FOLLOWING AXIS ROTATE THE AIRCRAFT IF THE AILERON AND ROLL SPOILER ARE USED?. LONGITUDINAL AXIS. LATERAL AXIS. VERTICAL AXIS.