1) If the control column is moved forward and to the left Report

left aileron moves down, right aileron up, elevator down

left aileron moves up, right aileron down, elevator down

left aileron moves up, right aileron moves down, elevator up

2) On an aircraft fitted with spoilers for lateral control, roll to the right is caused by Report

left spoiler extending, right spoiler remaining retracted

right spoiler extending, left spoiler remaining retracted

both spoilers extending

3) When an aileron trim control in the cockpit is moved to counteract a tendency to fly left wing low, an aileron trim tab fitted to the port aileron will Report

move up and cause the left aileron to move down but the right aileron will remain neutral

move up and this will cause the left aileron to move down and the right aileron to move up

move up and cause the left aileron to move down and the right aileron to move down to a lesser degree

4) You have adjusted the elevator trim tab to correct for nose heavy. What was the direction of travel of the trim tab? Report

The elevator trim tab has moved up

The elevator trim tab has moved down

The port elevator tab has moved up and starboard moved down

5) Pulleys in a flight control system are made from Report

Brass

Stainless steel

Tufnol or aluminium alloy

6) A tension regulator in the flight control cable system of a large all metal aircraft is used primarily to Report

retain a set tension

increase cable tension in cold weather

decrease cable tension in cold weather

7) An interrupter arm incorporated in a flying control locking mechanism Report

locks the ailerons and elevators

restricts movement of the throttles

dampens the rudder movement

8) The yaw damper must be designed to allow the rudder to control in response to the aircraft's. Report

pitch Frequency

roll frequency

dutch roll frequency

9) The alpha vane signal can be fed to __________ when the aircraft is close to stall Report

flap position

throttle lever

fast/slow switch

10) Moving the elevator trim wheel fully aft, then the Report

aircraft tends to go nose down

aircraft tends to go nose up

aircraft tends to roll to the right

11) Ground spoilers are used to Report

increase wing loading on take-off

decrease wing loading on landing

prevent FOD ingestion into the engines on landing and taxiing

12) The outboard ailerons on some aircraft Report

are isolated at slow speeds

are isolated to improve sensitivity

are isolated to prevent aileron reversal

13) The effect of the rudder on an aircraft can be increased by Report

increasing the altitude of the aircraft

decreasing the velocity of the aircraft

increasing the distance of the control surfaces from the aircraft's centre of gravity

EASA Questions Module 11 Set 18: Flight Controls_1

Set 1: Theory of flight

Set 2: Airframe Structures

Set 3: Aeroplanes-Fuselage

Set 4: Cabin Pressurisation

Set 5: Instruments

Set 6: Avionic system

Set 7: Avionic system

Set 8: Navigation

Set 9: Electrical Power

Set 10: Electrical System

Set 11: Battery

Set 12: Equip & Furnishing

Set 13: Fire Protection

Set 14: Fuel Systems

Set 15: Hydraulic Power

Set 16: Ice & Rain

Set 17: Flight Controls

Set 18: Flight Controls_1

Set 19: Landing Gear

Set 20: Lights

Set 21: Oxygen

Set 22: Pneumatic

Set 23: Water & Waste