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IN THE SLAT/FLAP SYSTEM: THE TORQUE SHAFT ( TORQUE TUBE) POSITIONS IN THE EXTERNAL TIP IS MEASURED AND FEED BACK THE SFCC BY THE: Asymmetry Position Pick Off Units (APPUs). Feedback Position Pick-off Unit (FPPU).

THE FLAP DISCONNECT SENSORS ARE MONITORED: By the Slat/Flap control Computers (SFCC's) via the LGCIUs. By the Spoiler Elevator Computers (SEC's) via the LGCIUs.

NORMALLY ROLL CONTROL IS DONE (ACCOMPLISHED) BY: ELAC´s and SEC´s controlling spoilers 2 to 5 and the ailerons. ELAC´s and SEC´s controlling spoilers 3 to 4 and the ailerons.

WHAT IS THE MEANING OF PARTIALY LIFT DAMPING (Ground Spoiler system)?. Spoiler 1-5 in left and right side extend partially at touchdown. Spoiler 2-5 in left and right side extend at touchdown.

THE RESET OF WING TIP BRAKES (WTB) IS POSSIBLE: On ground only. Un ground only.

HOW MANY SERVO CONTROLS HAVE EACH AILERON IN THE A320 FAMILY?. 2. 3. 4.

THE SLAT AND FLAP SYSTEM CONSISTS OF: One Slat/Flap Control Lever, two SFCC's, one Slat PCU and one Flap PCU. Two Slat/Flap Control Lever, two SFCC's, one Slat PCU and one Flap PCU.

HOW MANY PCU HAVE THE A320 FAMILY?. 2 PCUs. 3 PCUs. 4 PCUs.

THE REASONS THAT OPERATED THE WTB: Assymetric, overspeed, run away, uncommanded movement. Assymetric, , run away, uncommanded movement.

WHAT HAPPENDS IF A SPOILER SERVO CONTROLS FAILS?. The opposite surface retracts. Ground spoilers do not work.

IF ONE (1) SLAT FLAP CONTROL COMPUTER (SFCC) FAILS: The slat and flap systems operate at half speed. The slat and systems operate at half speed.

THE NAME OF THE 3 PAGES USED IN THE 320 FAMILY TO SHOW THE TOTAL INDICATION OF FLIGHT CONTROLS IN ECAM?. F / Control, Wheels, EWD. F / Control, EWD, Hyd.

WHAT IS THE MEANING OF AILERON DROOP?. Ailerons extends downward the help the flap function. Ailerons extends to help the spoiler function.

THE GROUND SPOILER OPERATION LOGIC INSIDE THE SEC 1, 2 AND 3 USES INFORMATION LIKE: Speed brake lever,Thrust Lever position, shock absorber Information and Radio Altimeter altitude information. Speed brake lever,Thrust Lever position,absorber Information and Radio Altimeter altitude.

WHAT SPOILERS ENSURING THE SPEED BRAKES FUNCTION?. Spoilers 2 thru 4. Spoilers 2 thru 5.

WHICH COMPUTER NORMALLY CONTROLS THE AILERONS?. ELAC 1. ELAC 2.

THE SLAT SYSTEM WING TIP BRAKES (WTB) ARE INSTALLED: At the wing tip. At the Flap tip. At the Slap tip.

WHAT IS THE PURPOSE OF PRESSURE OF BREAK (POB)?. To permit and stop the movement of the surface. No permit and stop the movement of the surface.

HOW MANY SPEED BRAKES SERVOCONTROLS HAS THE A320?. 6 Servo controls. 7 Servo controls. 5 Servo controls.

THE FLIGHT CONTROL SURFACES ARE MAINLY MADE OF: Composite material but Slats are made of aluminum Alloys. Composite material Slats are made of aluminum Alloys.