Flight Controls

In-flight, roll control is achieved by?

Two ailerons only

Two ailerons each one with a spring tab.

Two ailerons each one with a spring tab and two spoilers.

Two ailerons each one with a spring tab and two speed-brakes.

Roll control is achieved by actuating?

Mechanically the ailerons and hydraulically the spoilers.

Mechanically the spoilers and hydraulically the ailerons.

Mechanically the spoilers and ailerons.

Hydraulically the aileron and the spoilers.

Roll trim is performed using?

Only right aileron tab

Only left aileron tab

Both left and right aileron tab

Both spoilers

The spoiler cyan triangle light illuminates to indicate that?

The associated spoiler has failed.

The associated spoiler is in retracted position.

The associated spoiler is not in retracted position.

The spoiler is Jammed

Each spoiler has a hydraulic actuator which is controlled?

Mechanically by the associated aileron linkage.

Mechanically by aileron deflection.

Electrically by control of the wheel position.

Electrically by the associated aileron linkage.

The spring tab provides?

A flexible compensation of the left aileron only.

A flexible compensation which increases automatically with the aerodynamic load on the ailerons.

A fixed compensation of left aileron.

A fixed compensation of both ailerons.

What does it mean when the aileron trim indicator becomes white on the EWD?

The auto-pilot is disengaged and the aileron trim is not inhibited.

The aileron trim is iammed.

The aileron is locked by the gust lock system.

The auto-pilot is engaged and the aileron trim is inhibited.

Spoilers start to move after a given aileron deflection (2.5 deg.)

At low speeds (after landing gear extended).

At low speeds (flaps fully extended).

Electrically by control wheel position.

At all speeds.

The yaw trim is actuated by?

An electrical trim actuator, shifting the trim tab zero position.

A hydraulic trim actuator, shifting the rudder zero position.

An electrical trim actuator, shifting the rudder zero position.

Pedals Position.

The stick pusher actuator is attached to the linkage of the?

CAPT's control column.

F/Os Control column

CAPTs and F/Os control columns

CAPTs and F/os rudder pedals

Pitch control is achieved by?

Two hydraulic elevators.

Two mechanical drive elevators, each fitted with an automatic tab.

One mechanical drive elevator.

One hydraulic elevator.

The yaw trim position indicator shows?

Units of trim motor displacement from neutral.

Rudder position

Tab position.

Pedals position.

Roll trim is controlled using?

Only right aileron tab.

Only left aileron tab.

Both left and right aileron tabs.

None of the above.

The standby pitch control switch?

Is located on the the overhead panel

Is located on the CAPTs control column

The action of this switch will disengage the autopilot

Can only be used in flight

In case of a pitch jam pilot control can be recovered by?

Disengaging the autopilot only

Disengaging the pitch control coupling system, applying a force of 52 dan

Switching coupling to the other side

Applying pitch trim

Flight Controls

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