wayground logo

Free Printable Worksheets

NEW

Font size

S
M
L
XL
Worksheets

Piston Aircraft Aerodynamic,Structure And System Mod 11B

Total questions: 72

Worksheet time: 36mins

Name
Class
Date
1.

which of the following control surface is used to yaw control about normal axis in an aircraft?

a)

rudder

b)

aileron

c)

elevator

2.

which of the following statement is true when a control column is push forward?

a)

the nose of the aircraft would drop

b)

the nose of the aircraft would move up

c)

the nose of the aircraft would remain on thhe current path

3.

where does the rudder located on aircraft?

a)

trailing edge of fin

b)

trailing edge of mainplane

c)

trailing edge of horizantal stabilizer

4.

what couse flying fault during normal flight?

a)

change in mass of the aircraft

b)

change in weight and centre of gravity

c)

change in velocity and centre of pressure

5.

which of the following component is used to adjust cable tension?

a)

fairleads

b)

end fitting

c)

tumbuckle

6.

aircraft fuel system can be classified into two board categories,that is ………………………

a)

pump-feed and motor-feed

b)

gravity-feed and pressure-feed

c)

kinatec-feed and potential-feed

7.

which of thee following is a tank that is part off basic structure of the aircraft ???

a)

integral tank

b)

bladder tank

c)

rigid removable tank

8.

which of the following is the source of heat used by the fuel heater?

a)

thermocouple

b)

engine turbine bleed air

c)

engine compressor bleed air

9.

a fuel crossfeed valve is usually in …………………during flight

a)

its last position

b)

the opened position

c)

the closed position

10.

what type of metarial is used to maske aircraft fuel hoses?

a)

teflon

b)

stainless steel

c)

synthetic rubber

11.

how long is the maximum storage life for seals from the date of cure?

a)

4 years

b)

5 years

c)

6years

12.

what is the disadvantage of skydrol?

a)

low viscosity

b)

easy to burn

c)

attack vinyi plastics

13.

in hydraulic system the sealing component is required to…………

a)

reduce heat for moving part

b)

prevent leakage pass union

c)

preven bubber in hydraulic system

14.

where is the temperature over heat switch located in a hydraulic pump?

a)

in the case drain

b)

in the suction line

c)

in the pressure line

15.

which of the following is a type ice formation,occur on a surface which is at temperature below the frost point og the adjacent water in contact with the surface?

a)

hoar frost

b)

rime ice

c)

glaze ice

16.

how to minimize the effect rain had on visibility in flight?

a)

apply rain repellent

b)

use anti- icing system

c)

anti raining system,which alert the pilot to divet to other area

17.

all of the following are information marked on all commercial aircraft tyre, EXCEPT

a)

size

b)

material

c)

skid depth

18.

what is the function of landing gear

a)

to support aircraft yawing during flight

b)

to support an aircrafrt rolling during flight

c)

to support an aircraft during ground manoeuvres

19.

tubeless tyres are stored………………………

a)

vertically

b)

at 15 to 20 p.s.i

c)

horizontally maximum of four high with smallest diameter tyre on top

20.

what is the function of landing and taxi light of an aircraft??

a)

provide spot light to heat the tarmac

b)

provide illumination during landing and taxing at night

c)

provide reflection toward the landing instrument on the runway

21.

which of the following lights is used to illuminate the escape routes on an aircraft?

a)

neon lamp

b)

halogen light

c)

fluorescent light

22.

the breathing oxygen used in aircraft system should comply with………..

a)

international standard ISO 2046

b)

international standard ISO 3000

c)

international standard ISO 4048

23.

how many fix installation are there in the aircraft oxygen system?

a)

2

b)

4

c)

3

24.

anoxia is due to…..

a)

lack of oxygen

b)

low air pressure on the body

c)

release of nitrogen bubbles in the blood

25.

what drives the compressor in the pneumatic pressure generating system?

a)

accessory gearbox

b)

electrical motor

c)

axillary power unit

26.

which of the following controlled the bleed valve in the pneumatic pressure general system

a)

pressure in the air bottle

b)

compressor in the bottle

c)

ram air from the engine

27.

hiw does pneumatic system protect against dirt??

a)

filter

b)

sealent

c)

diaphragm

28.

the wheel brake control unit admits air to the brake units at a controlled pressure,proportional to…………..

a)

lever movement

b)

padel movement

c)

joystick movement

29.

which of the following is used to preciptate the moisture in the pneumatic system?

a)

filter

b)

anti freezer

c)

oil and water trap

30.

what type or water filter is used for aircraft portable water system?

a)

sintered metal

b)

wire wound filters

c)

paper base element

31.

where does the drain mast located on an aircraft?

a)

under wing

b)

under fuselage

c)

upper fuselage

32.

which of the following is not a type of toilet system used on the aircraft?

a)

bucket system

b)

pressure system

c)

vacuum toilet system

33.

what is the range of temperature need tobe sustained by the thermostatically controlled heating unit the main water tank?

a)

temperature of 110 degrees to 120 degrees F

b)

temperature 150 degrees to 160 degrees F

c)

temperature of 190 degrees 200 degrees F

34.

Which of the following is the function of rudder during maneuver of an aircraft?

a)

Yaw

b)

roll

c)

pitch

35.

How can a pilot operate an aileron on a aircraft?

a)

by rotating the joystick twice

b)

by moving the control coloumn laterally

c)

by pulling the hand wheel mounted on the control coloumn

36.

Which of the following is an example of drag induced device?

a)

Aileron

b)

Landing brake

c)

Flight spoiler

37.

The purpose of a slot in a wing is to_______________________

a)

provide housing for the slat

b)

speed up the airflow and increase lift

c)

act venturi, accelerate the air and re-energise boundary layer

38.

On an aircraft with an all moving tail plane, pitch up is caused by____________

a)

Increase tail plane incidence

b)

Decrease tail plane incidence

c)

Up movement of the elevator trim tab

39.

When the trailing edge flaps lowered, the aircraft will____________

a)

Sink

b)

Pitch nose up

c)

Pitch nose down

40.

Where usually wing station (WS) numbers are measured from?

a)

The end of pylon

b)

Tangent of the fuselage

c)

The centre line of the fuselage

41.

How many structural classifications are there in aircraft?

a)

2

b)

3

c)

4

42.

Shear stress is described as

_________________

a)

Pulling forces

b)

Compressing force

c)

Slip away under the action of forces

43.

Why an aircraft typically has circular cross section?

a)

Suitable shape that easy to assemble

b)

Suitable shape for quick corrective action

c)

Suitable shape to contain differential pressure

44.

Why sealing compound is used to all joint in pressurize structure?

a)

Prevent joint to loose

b)

Prevent leakage of pressure

c)

Prevent the sealant from corrode

45.

Which of the following components is used to slow the growth of any skin cracks which might develop in service?

a)

Bulkhead

b)

Tear stopping bands

c)

L-shape stringers

46.

Why windscreen must be heated?

a)

To increase the formation of mist on the passenger windows

b)

To improve the impact resistance of the windscreen at low temperature

c)

To make sure temperature sensing elements can be used extensively in the snow surrounding.

47.

What is Empennage?

a)

Tail assembly consist of aileron, horizontal stabilizer, vertical stabilizer and rudder

b)

Tail assembly consist of elevator, engine nacelle, vertical stabilizer and rudder

c)

Tail assembly consist of elevator, horizontal stabilizer, vertical stabilizer and rudder

48.

What is the unit used in the measurement of the ultimate tensile strength of the material in an aircraft?

a)

Lbs/in square

b)

J/km square

c)

Pascal

49.

Which of the following statements is true about truss?

a)

Is the main longitudinal member of a fuselage or nacelle

b)

Is the lateral fuselage or nacelle member giving cross-sectional shape which is often circular

c)

. Is an assemblage of members forming a rigid framework, which may consist of bars,beams, rods, tubes and wires

50.

What is the function of liquid receiver in the vapour cycle cooling system?

a)

To control and monitor the liquid refrigerant into the evaporator

b)

To provide a storage area for the liquid refrigerant into the evaporator

c)

To provide the motive force for refrigerant re-ccirculation and work in conjuction with thermostatic expansion valve.

51.

When does the proof pressure check of air conditioning is carried out?

a)

During manufacturing

b)

During night stop

c)

During maintenance at MRO

52.

How many primary flight instrument consist in the pitot static system?

a)

3

b)

4

c)

5

53.

What is the dynamic pressure?

a)

Difference between total pressure and static pressure

b)

Difference between static pressure and pitot pressure

c)

Difference between boundary pressure and static pressure

54.

What is the purpose of an aircraft altimeter?

a)

Provide indication of the aircraft’s height above a sea level

b)

Provide an accurate indication of the aircraft’s height below a sea level

c)

Provide inaccurate indication of the aircraft’s height above certain predetermined level

55.

A gyroscope is defined as____________________

a)

A pivoted support that allows the rotation of an object about a single axis

b)

A device for measuring orientation, based on the principles of angular momentum

c)

A spinning mass mounted in such a way the spin axis is free to rotate about one or two axis at right angles to the spin axis

56.

Function of communication system is_______________

a)

To transfer information from one point another

b)

To delivery signal from aircraft to satellite

c)

To find the emergency location during crash and emergency

57.

All the following statements are true about external electrical power, except

a)

For the starting engines

b)

For the purpose of anti-icing system on aircraft

c)

For the testing of electrical systems during routine maintenances

58.

Which of the following are the types of inverter used on aircraft electrical system?

a)

Rotary and static inverter

b)

Stator and rotary inverter

c)

Static and dynamic inverter

59.

What is the purpose of batteries in aircraft?

a)

To start up APU for ground run

b)

To start up yhe engine for take off

c)

To store energy for emergency situations

60.

Which of the following is NOT one of AC power generations subdivision?

a)

Primary

b)

secondary

c)

emergency

61.

What type of power supply used to operate certain flight control in the event of a total loss of primary power?

a)

aircraft battery

b)

Secondary power supply

c)

Auxiliary power unit

62.

FAR part 25 is valid for_____

a)

Transport helicopter

b)

. Small aircraft

c)

C. commercial aircraft

63.

When designing cabin equipment, attention must be paid to____________

a)

Inflammable and self floating material used

b)

Low inflammbility and toxicity of the materials used

c)

High tension and flame resistance material used

64.

How to prevent hand luggage from gliding forward under the seats?

a)

A barrier under the seats installed

b)

A hook under the seat installed

c)

Passenger must hold the luggage

65.

. How are the galleys installed in the aircraft cabin without damage during flight?

a)

Belt is used to hold the galley

b)

The galley is fitted in the seat rail profiles on the ground

c)

The galley is weld together to the structure of the aircraft

66.

Why the backrest of the passenger seats designed so that they fold forward during a crash landing?

a)

Prvent from breaking his/her neck during the accident

b)

Prevent the backrest to break off

c)

Prevent rear passenger head to hit the back rest in front of him

67.

What is the lavotary designed with rounded corner

a)

To prevent injuries

b)

To improve strength

c)

To create an aerodynamic surfac

68.

Which of the following is not a cargo compartment in the lower lobe of an aircraft?

a)

Aft compartment

b)

Bulk compartment

c)

Central compartment

69.

What type of equipment is used to hold the pallets in its final position on the aircraft?

a)

Cargo net

b)

Locking pawl

c)

Lashing rope

70.

The testing of the control circuit of the fire extinguishing system must be carried out at the check periods specified in the_______________

a)

Approved Structure Repair manual

b)

Approved Maintenance Schedule

c)

Approved Electrical Wiring Manual

71.

. Which of the following fire detector is called ‘Continous Loop

a)

Tubular detector

b)

Thermocouple detector

c)

Thermal switch detector

72.

. What type of the fire extinguisher can be found in the cockpit of an aircraft?

a)

CO2 extinguisher

b)

Halon extinguisher

c)

Dry chemical extinguisher