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Aircraft Exam MCQ

Total questions: 40

Worksheet time: 40mins

Name
Class
Date
1.

The most important properties of air that affect aerodynamic behaviour are its

a)

static pressure, temperature and density

b)

Dynamic pressure, temperature and density

c)

Temperature and density

d)

Air

2.

Afterburners will produce approximately ____ increase of thrust but with a corresponding ____ increase in fuel flow

a)

50% and 150% respectively

b)

100% and 100% respectively

c)

100% and 50%

d)

50% and 50%

3.

What is the term for movement of the rotor blades during a pitch angle change?

a)

Feathering

b)

Collective pitch change

c)

Pitching

d)

Hovering

4.

To activate normal pressure demand mode of oxygen supply the switches on the oxygen regulator panel must be set to:

a)

Emergency Level set to ‘Normal', Diluter Lever set to ‘Norm' and Mode Lever set to 'On’

b)

Emergency Level set to 'Normal', Diluter Lever set to Norm and Mode Lever set to no

c)

Emergency Level set to ‘Normal', Diluter Lever set to ‘Norm' and Mode Lever set to 'OFF:

d)

Emergency Level set to ‘Abnormal', Diluter Lever set to ‘Norm' and Mode Lever set to 'On’

5.

Name 2 of the items can be found in the Personal Survival Packs (PSP)?

a)

Salt tablets & strobe light

b)

Sweet Tablets & strobe light

c)

Salt tablets and stroke lights

d)

Salt tablets and stobe light

6.

Which of the following may be designed as the weighing points of an aircraft for weight and balance calculation?

i. Jacking points

ii. Centre of gravity point

iii. Nose and main landing gear.

a)

i and iii

b)

i and iiii

c)

i and ii

d)

1 and 3

7.

The high level indication light comes on during pressure refuelling when

a)

when tanks are full

b)

when tank are full

c)

when tanker are full

d)

when tanky is full

8.

 What happens when the pressure closing valve is shut?

a)

pressure in the converter continues to build up gradually

b)

pressure in the reducer continues to build up gradually

c)

the pressure opens th valve

d)

pressure in the converter continues to build up instantly

9.

Which part of the parachute is strong & contain some elasticity & it absorb much of the shock load?

a)

Suspension lines

b)

Suspension straps

c)

Suspense

d)

Suspending lines

10.

Which component is designed to operate within 2.5 seconds after being immersed in seawater?

a)

SEAWARS (Seawater ACTIVATED Release System)

b)

SEAWARS (Seawater Activation Release System)

c)

SEAWARS (Seawater Artificial Release System)

d)

SEAWARS (Seawater Activated Release System)

11.

What is the ply rating of an aircraft tire used to express?

a)

The relative strength of an aircraft's tire

b)

The relative strength of an aircraft tire

c)

The toughness of the aircraft tire

d)

The relative strength of an aircrafts tire

12.

In the anti-icing pneumatic system, the deicer consists of a series of

a)

Inflatable tubes

b)

Inflatable balloons

c)

Inflatable Boots

d)

Inflammable tubes

13.

Why is cabin pressurisation of military aircraft limited to a maximum differential pressure of about 3.5 psi?

a)

Due to the danger of rapid decompression

b)

Due to the danger of instant decompression

c)

Due to the danger of rapid compression

d)

Due to the danger of rapid decompressurisation

14.

When is a landing gear retraction check NOT required?

a)

After prolonged taxying

b)

After prolonged carying

c)

After prolonged waiting

d)

After hard landing

15.

The air conditioning system pressurises the fuselage during flight. Which of the following statements is correct?

a)

The best condition for aircraft structure would be no pressurisation during flight

b)

The best condition for aircraft structure would be limited pressurisation during flight

c)

The best condition for aircraft structure pressurisation to ground air

d)

The best condition for aircrew pressurisation would be no pressurisation during flight

16.

What is SARBE stands for

a)

Search and Rescue Beacon Equipment 

b)

Search and Rescue Beam Equipment

c)

Search and Rescue Bacon Equipment

d)

Search and Rescue Beacon

17.

What is the function of the afterburning principle?

a)

To improve aircraft take off, climb and combat performance

b)

To improve aircraft take off, climbing and combat performance

c)

To improve aircraft taking off, climb and combat performance

d)

To improve aircraft take off, climb and wombat performance

18.

In transonic flight, control effectiveness is reduced because of

a)

control surface is operating in 'aerodynamically dead' air mass

b)

control surface is operating in 'aerodynamically life' air mass

c)

control surface is operating in 'dynamically dead' air mass

d)

control surface is operating in 'aerodynamically dead' ground mass

19.

What causes the caution light in the cockpit to remain on?

a)

Insufficient fluid in reservoir

b)

Insufficient liquid in reservoir

c)

Presence of air in reservoir

d)

Caution light mulfunction

20.

The main purpose of the metering pin found in shock struct is for

a)

controlling the rate of fluid flow from the lower to the top chamber

b)

seperating the gas from the fluid

c)

controlling the rate of fluid flow from the middle to the middle chamber

d)

stopping the rate of fluid flow from the top to the lower chamber

21.

A developer is applied on the surface of the test material to draw out the penetrant from the flaw by

a)

capillary action

b)

caterpillar action

c)

capiliary action

d)

capillary

22.

What is the advantage of a temperature control circuit using electronic components?

a)

There are no mechanical parts that can cause wear

b)

There are no mechanical parts that can wear

c)

There are no hydraulic parts that will wear

d)

Electric is fast

23.

What are the surfaces that require electrical heating in the turbo-propeller engine installation?

a)

Air intake cowling of engine, propeller blades and spinner assembly

b)

Air intake cowling of engine

c)

Leading edge of propeller

d)

Pilot chair

24.

Fire detectors are used in areas where the risks of fire are at their highest due to the

i high volume of air flow

ii. high ambient temperature

iii. presence of inflammable fluid lines

iv. use of non heat resistant material for the aircraft structure

a)

ii and iii

b)

i and iii

c)

2 and 3

d)

two and three

25.

The purpose of the inlet coalescing filter

a)

remove contaminant and moisture from ECS air

b)

remove contaminant and moisture from ambient air

c)

remove dust and moisture from ECS air

d)

remove contaminant and moisture from cockpit

26.

Jet aircraft use nose wheel landing gears and not tail wheel landing gears because

a)

the nose gear has better directional stability and it prevents nosing over during brake applications

b)

the nose gear allows for better view around

c)

the nose gear allows for better maneuverability on ground

d)

the nose gear allows for better steering

27.

Name the 4 primary components in a basic hydraulic system

a)

pump, control valve, jack, and reservoir

b)

pressure valve, jack and tank

c)

pump, control valve

d)

jack and reservoir

28.

What is the cooling principle of the vapour cycle machine?

a)

The refrigerant is compressed and expanded in a closed circuit and cooled by ambient air

b)

The refrigerant is compressed and expanded in a open circuit and cooled by ambient air

c)

The refrigerant is compressed and expanded in a closed circuit and cooled by ECS air

d)

The refrigerant is expanded and compressed in a closet circuit and cooled by ambient air

29.

Which is NOT a characteristic of a Pressure Demand Oxygen System?

a)

Oxygen is delivered directly into the cabin and correct proportion of oxygen/air is mixed for aircrew as a factor of altitude

b)

Oxygen is delivered directly into the cockpit and correct proportion of oxygen/air is mixed for aircrew as a factor of altitude

c)

When inhaling, oxygen is supplied

d)

When on oxygen is supplied

30.

In the rotor brake system, if the pilot move the braking lever into the static braking notch, the pressure in the rotor brake will be

a)

100 bar

b)

200 bar

c)

One Hundred Bar

d)

1 Hundred Bar

31.

Bernoulli's equation for subsonic flow states:

a)

If the velocity of an air stream within a tube increases, the static pressure of the air decreases, but the sum of the static pressure and the dynamic pressure remains constant.

b)

If the velocity of an air stream within a tube increases, the dynamic pressure of the air decreases, but the sum of the static pressure and the dynamic pressure remains constant.

c)

If the velocity of an air stream within a tube increases, the static pressure of the air decreases, but the sum of the dynamic pressure and the static pressure remains constant.

d)

If the velocity of an air stream within a tube increases, the static pressure of the air decreases, but the sum of the static pressure and the dynamic pressure decreases as well

32.

Air turbine starter generally incorporate a reduction gear to convert the?

a)

High speed low torque of the turbine wheel to a low speed high torque to the output shaft

b)

High speed high torque of the turbine wheel to a low speed high torque to the output shaft

c)

Low speed low torque of the turbine wheel to a low speed high torque to the output shaft

d)

High speed low torque of the turbine wheel to a high speed high torque to the output shaft

33.

The aircraft life is usually determined by

a)

flight hours

b)

life hours

c)

ground hours

d)

flying hours

34.

In the typical cabin pressure regulator, how is the control chamber exposed to the atmosphere?

a)

through the needle valve

b)

through the control valve

c)

through the orifice

d)

through the valves

35.

In a typical helicopter fuel system, what is the function of the jet pump?

a)

Transfer fuel from other tank into the feeder tank

b)

Transfer fuel from feeder tanks into the other tank

c)

Transfer fuel from drop tanks into the feeder tank

d)

Transfer fuel from other tanks to the feeder tank

36.

Which of the following is an advantage of the cable control system over the push-pull rod system?

a)

it has less mechanical play

b)

it has no lapse in control

c)

it is fast to reaction

d)

it is more cost efficient

37.

Arresting gear is extended by _____ pressure and retracted by _________ pressure?

a)

air, hydraulic

b)

air, hydraulics

c)

air, hydrocele

d)

air, hydrofoam

38.

What is the advantage of AVGAS fuel?

a)

easier to start engine

b)

Cost efficient

c)

easier to refuel

d)

easier to start wings

39.

During normal flight, what is the normal cabin pressurisation?

a)

8000 feet above sea level

b)

18000 feet above sea level

c)

80000 feet above sea level

d)

80,000 feet above sea level

40.

When is a landing gear retraction check NOT required?

a)

After prolonged taxying

b)

After prolonged taxing

c)

After prolonged trucking

d)

After prolonged tax-ing