Module 13 - AME Quiz

Module 13 quiz contains 180 question based on the syllabus for module 13 examination for B2 category.

The time limit for the quiz is 225 min.

The number of attempts allowed are unlimited.

All the best.

Name

If you add an aerial, to strengthen the airframe you add

an internal doubler

an intercostals

external doubler

What does a trim tab do?

Allows the C of G to be outside the normal limit

Provides finer control movements by the pilot

Eases control loading for pilot

What frequency increases radar relative range

low

high

Radar relative range cannot be increased by frequency change

What preventative maintenance can be carried out in case of HIRF

Shielding of all sensitive equipment

Check of aircraft structure

Bonding and insulation tests

Stand off errors on localiser approach are washed out by

integrating course error

integrating deviation signal

differentiating deviation signal

Satellite transmits updates on every

13th orbit

2nd orbit

9th orbit

What do ruddervators do

Control pitch and roll

Control pitch and yaw

Control yaw and roll

What is power at pulse

Average power

Pulsed power

Peak power

Galley and cabin lighting operate on

DC bus

AC bus

GND services

10.

Runway visual range in (RVR) is obtained by

three sets of instruments at the side of the runway

one set of instruments the threshold of the runway

information obtained the local Meteorological Office

11.

Buffer amp on transmitter is between

local oscillator and modulator

modulator and power amp

local oscillator and demodulator

12.

Flaps at landing position

decrease landing speed

decrease take off and landing speed

decrease take off speed

13.

What is the 'Q' code for runway heading

QDM

QDH

QDR

14.

Which side of the pilot is the collective

In between legs

Right

Left

15.

How many satellites required for GNS

16.

The wheel height at which the approach path has been visually assessed as satisfactory to continue the approach to a landing is known as the

alert height

decision height

intercept height

17.

The purpose of a yaw damper is to

block the Dutch roll frequency

produce a co-ordinated turn

assist the aerodynamic response

18.

A full operational autopilot system will ensure that

the automatic pilot will automatically disengage whenever any failure is detected

the automatic pilot will automatically cause the aircraft to overshoot if any failure is detected

the aircraft will continue its automatic landing in the event of a single failure

19.

An automatic throttle, engaged in the EPR mode, will control

the engine throttles to maintain a constant acceleration rate

the aircraft altitude to maintain constant engine input pressure

the engine throttles to maintain a constant engine power setting

20.

Relative velocity of rotor

increases at fwd travelling blade

is equal for all blades

increases at retreating blade

21.

What effect does the ground have on a helicopter

Increases lift

Increases thrust

No effect

22.

If an 80 ohm coaxial cable is connected to an 80 ohm dipole aerial, resistance would be

0 ohm

80 ohm

160 ohm

23.

With autothrottle selected in the SPEED MODE compatible autopilot modes are

V/S and ALT ARM

VOR ARM and HDG HOLD

IAS HOLD and ALT ARM

24.

Pushing the left rudder pedal

yaws the aircraft left but has no effect on the wing

yaws the aircraft left and possibly the right wing will rise

yaws the aircraft left and possibly the left wing will rise

25.

What happens when battery master is switched off in flight

Battery disconnected from charge circuit

Electrical systems shut down

No effect

26.

Adding 6 foot of cable to TX RX aerials on rad alt would give you

3 ft error

6 ft error

12 ft error

27.

What controls pitch and roll on a delta wing aircraft?

Ailerons

Elevators

Elevons

28.

in MLS, what is the beam angle away from runway

20 degrees

15 degrees

10 degrees

29.

Maximum power on a wave guide is governed by the

widest width

narrowest width

number of joints and bends

30.

How does a balance tab move?

In the opposite direction proportional to the control surface it is attached to

In the same direction a small amount

In the same direction proportional to the control surface it is attached to

31.

during an automatic landing, the aircraft descent rate is sensed by

radio altimeters

pitch rate gyros

vertical accelerometers

32.

Lowering of the flaps

increases drag and lift

increases lift

increases drag

33.

If on a lead-acid battery, several cell checks of SG read consistently low. Battery needs

recharging

replacing

topping up with distilled water

34.

A category 3B aircraft using fail operational automatic landing equipment which fail operational control and roll out guidance will have

a decision height of about 50 feet

a decision height depending upon the RVR

no decision height

35.

Aircraft is North of VOR beacon on a course of 090 RMI pointer points to

180

36.

in a triplex system, the detection of a failure of one simplex system will disconnect

the failed system and continue with a manual approach

the failed system and carry on with an autoland

all channels

37.

The International Civil Aviation Organisation weather category 3A is

operation down to and along the surface of the runway without external reference

operation down to sixty meters and RVR of 800 meters

operation down to and along the surface of the runway with RVR of 200 meters

38.

If radar pulse is reduced there is

increased relative range

reduced relative range

no effect

1 out of 1

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