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6320 Chap C: Engine Starting

Total questions: 25

Worksheet time: 10mins

Name
Class
Date
1.

Basic Engine Starting Circuit: Once the start cycle has been initiated, the RPM sensing unit holds start button No1, until the engine reaches what?

a)

Ground Idle

b)

Self Sustaining

c)

start-up

d)

Flight mode

2.

Describe a turbojet engine?

a)

used to drive an aircraft propeller

b)

produces shaft power to drive machinery

c)

simplest design, provides thrust power

d)

High bypass engine

3.

Describe a turboshaft engine?

a)

used to drive an aircraft propeller

b)

produces shaft power to drive machinery

c)

simplest design, provides thrust power

d)

High bypass engine

4.

Once a HEIU has been switched off, what is the minimum time for safety that you must wait before touching any part of the system?

a)

2 minutes

b)

1 minute

c)

3 minutes

5.

Basic Engine Start Circuit: Energising what ?? will allow DC power to H.E.I.U which produces the power for the igniter plug.

a)

start relay

b)

ignition relay

c)

hold on relay

d)

fuel on relay

6.

Merlin No1 engine starting using an air starter (APU): The engine must be either in accessory drive, or main drive with blades spread and the rotor brake on.

a)

False

b)

True

7.

Electrical starters can be configured to perform the dual role of driving the engine for starting and subsequently being driven by the engine to generate electrical power for the aircraft systems.

a)

True

b)

False

8.

Engine Starting: The drive shaft of an air turbine starter is permanently coupled to the engine.

a)

False

b)

True

9.

Engine Starting: The APU can provide power for both electrical and air starters.

a)

False

b)

True

10.

gas turbine engines: This engine is used in rotary wing aircraft:

  • A free turbine is used to produce shaft power to drive machinery instead of producing thrust.

a)

Jet

b)

TurboFan

c)

TurboShaft

d)

TurboProp

11.

VENT

Which of the following is NOT an occasion when it is required to motor the engine without fuel or ignition:

a)

Replacement of a component in the starter systems.

b)

An oil system needs to be primed or bled.

c)

Replacement of an EECU or ECU

d)

The fuel system needs to be primed or bled.

12.

Engine Torque is a measure of the output ______ being developed by the engine. 

a)

POWER

b)

SPEED

c)

ANGLE

d)

Pressure

13.

A PTIT harness is made up of five dual thermocouple sensors which are electrically connected in series and arranged concentrically at the rear of the combustion chamber.

a)

FALSE

b)

TRUE

14.

Aircraft thermocouples are made of two dissimilar metals called

a)

Alumon

b)

Alumel

c)

Chromel

d)

Chromium

15.

A Compressor Inlet Temperature (CIT) Sensor is an example of a thermocouple.


a)

TRUE

b)

FALSE

16.

Thermocouples: The magnitude of the EMF will depend upon the types of dissimilar metals used

a)

TRUE

b)

FALSE

17.

The engine start procedure for a Merlin is to start the APU first using battery power:

  • The APU is controlled by the?

a)

ECU

b)

ESU

c)

CPU

d)

EECU

18.

Select two items:

State A & H

a)

Discharge Gap

b)

Discharge Resistors

c)

Reservoir Capacitor

d)

Primary Capacitor

19.

H.E.I.U

State the LT and HT energy levels?

a)

LT: 24V DC

HT: 1500 V 2000 A

b)

LT: 28 V DC

HT: 2000 V 1500 A

c)

LT: 28 V DC

HT: 2500 V 1000 A

20.

A starter/generator must be connected to the engine through a clutch mechanism which engages at commencement of the start cycle and disengages as the engine reaches self-sustaining speed.

a)

True

b)

False

21.

Which of the following is NOT an occasion when it is required to motor the engine without fuel or ignition:

Multiple choice 1 Question 24

a)

The fuel system needs to be primed or bled.

b)

Replacement of a component in the starter systems.

c)

The hydraulic system needs to be primed or bled.

d)

A compressor wash is required.

22.

The Compressor Inlet Temperature sensor produces resistance value signals proportional to the inlet air temperature which are fed to each ECU to provide cold junction compensation for the thermocouple circuit.

a)

TRUE

b)

FALSE

23.

POWER TURBINE SPEED SENSOR (NP):

The sensor is a dual coil magnetic variable reluctance pickup speed sensor which senses the speed of the 76-tooth gear which drives the oil pump

a)

True

b)

False

24.

Engine oil pressure and gearbox oil pressure are sensed by oil pressure ________ on the engines and the gearboxes which are displayed in the cockpit.

a)

Probes

b)

Transmitters

c)

Thermocouple

d)

switch

25.

Thermocouple Operation:

When two wires of dissimilar metals are joined at their ends to form a closed loop and heat is applied to both ends, an EMF is produced

a)

TRUE

b)

FALSE