Wing Flaps 1-38

Question 1

What type is the T-6 flap?

Answer 1

The aircraft is equipped with hydraulically operated, electrically controlled, four-segment split flaps

Question 2

Confirm the flaps position with the rear cockpit pilot, due to the restricted flap visibility from the front cockpit.

Answer 2

False. The flap position cannot be visually verified from either cockpit because the flaps are
hinged to the lower surface of the wing.

Question 3

Flap T/O position in degrees?

Answer 3

takeoff, 23° deflection

Question 4

Flap landing position in degrees?

Answer 4

landing, 50° deflection

Question 5

Normal flap operation and position indication is unavailable anytime the battery bus has failed, and one other time - when?

Answer 5

If the auxiliary battery is the

only source of electrical power.

Question 6

Emergency flap operation is not available when?

Answer 6

when the auxiliary battery is the only source of electrical power.

Question 7

If power to the flap control circuit is lost (e.g., loss of power to the battery bus, or the FLAP CONT circuit breaker has opened), the flaps will be stuck in the present position, flap position will not be visible from the cockpit, and the flap indication will be unreliable.

Answer 7

False. the flaps will retract to the UP position, flap position will not be visible from the cockpit, and the flap indication will be unreliable.

Question 8

The flaps cannot be retracted after emergency extension until the aircraft is serviced by maintenance.

Answer 8

True

Question 9

When power is removed from the flap indicator (e.g., battery

switch OFF or battery failure), the position pointer moves to a position ___________.

Answer 9

counterclockwise of the UP position