Module 11A Set-2 | DGCA MODULE

ALL THE BEST

Results

CONGRATULATIONS!!

Will you do a favour for me by clicking on any ads…

SORRY PRACTICE AGAIN..

Will you do a favour for me by clicking on any ads…

#1. ___________ IS USED IN WARNING LIGHT TO SEPARATE THE WARNING LIGHT.

DIODE

ZENER DIODE

THYRISTER

#2. PILOT SEAT BELT HAVE

#3. POSITIVE DYNAMIC STABILITY ?

MOTION OF AMPLITUDE INCREASE WITH TIME

MOTION OF AMPLITUDE DECREASE WITH TIME

STAY REMAIN SAME

#4. MTCS ABOUT VENT TANK ?

MUST BE ATLEAST ONE VENT IN TANK

MUST BE ATLEAST TWO VENT IN TANK

MUST BE ATLEAST FOUR VENT IN TANK

#5. MAX DEVIATION IN D.R COMPASS ?

10 DEG

5 DEG

15 DEG

#6. ACARS HAVE DATA LINK FROM A/C TO GROUND ?

UP LINK

CROSS LINK

DOWN LINK

#7. ACARS HAVE FREQUENCY RANGE ?

129-137 MHZ

150-535 KHZ

30-3000 MHZ

#8. ZONE 300 ?

ABOVE PRESSURE BULKHEAD

ENGINE, POWERPLANT AND NACELLE

EMPHENAGE, REAR PRESSURE BULKHEAD

#9. CABIN FURNISHING MATERIAL TESTING ____________

SMOKE

FLAMABILITY

SMOKE AND FLAMABILITY

#10. Primary structure is any portion of the aircraft structure that, if it fails, on the ground or in flight, would likely cause

A loss of control of the aircraft.

Catastrophic structural collapse.

Injury to occupants.

All of the above &Power unit failure.

#11. The examples of primary structure are

Wings spars, engine mounts, fuselage frames, and main floor structural members.

Wing ribs, fuselage stringers and specified sections of the aircraft skin.

Fairings, fillets, various support brackets,

All of the above.

#12. The structure has been evaluated, usually by the manufacturer, to assure that catastrophic failure is not probable after fatigue failure or obvious partial failure of a single, principal structural element. means

Fail safe structural element

Safe life structural element

Damage tolerance

#13. -------structural elements are those which have a very low risk of unacceptable degradation or failure for a stated amount of time.

Fail safe

Safe life

Damage tolerance

#14. MTCS regarding Fuselage station (FS).

FS are numbered in inches from a reference or zero point known as the reference datum.

The reference datum is an imaginary vertical plane at or near the nose of the aircraft from which all fore and aft distances are measured.

Some manufacturers may call the fuselage station a body station.

All of the above.

#15. Water line station no. is used to locate

Vertical stabilizer

Horizontal stabilizer

As in (a) & Landing gear

All of the above

#16. ------ is a material's internal resistance, or counterforce, that opposes deformation.

Stress

Strain

Tension stress

Shear stress

#17. Water line is

The measurement of height in inches perpendicular from a horizontal plane usually located at the ground, cabin floor, or some other easily referenced location.

Measured perpendicular to the rear beam of the wing and parallel to, and outboard from, the inboard edge of the flap.

A vertical reference plane down the center of the aircraft from which measurements left or right can be made.

Measured either forward of or behind the front spar of the wing and perpendicular to a designated water line

#18. The engine pulls the aircraft forward, but air resistance tries to hold it back.

Compression

Tension

Bending

Shear

#19. Which stress act on the wing