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CASA B1-1 Module 15B Gas Turbine Engines

Total questions: 28

Worksheet time: 16mins

Name
Class
Date
1.

The correct oil specification for an engine type can be found in the following...

a)

Aircraft Operator's Manual

b)

Aircraft Maintenance Manual

c)

Engine Maintenance Manual

d)

Engine Oil Tank Service Placard

2.

What components are used to aid in the transfer of heat in oil to the outside air/fuel

a)

Air/oil cooler

b)

Air cycle machine

c)

Fuel/oil heat exchanger

d)

Bypass valve

3.

Which is NOT a desirable characteristic of synthetic oils

a)

High viscosity index

b)

Low volatility

c)

High pour point

d)

Low lacquer and coke deposits

4.

The amount of pressure required to force out a film of oil from between two pieces of flat metal is referred to as...

a)

film strength

b)

volatility

c)

pour point

d)

viscosity point

5.

True or False: A high flash point means that the oil must be heated to a high temperature to give off flammable vapours

a)

True

b)

False

6.

Synthetic fluids routinely exhibit a nominal film strength that is ____ than mineral fluids

a)

Higher

b)

Lower

c)

Equal

7.

Viscosity is a fluids resistance to flow. What viscosity is more desirable in a gas turbine engine?

a)

High Viscosity

b)

Low Viscosity

8.

There are 3 types of synthetic oils currently in use. Can you mix Type I with Type II oils?

a)

Yes

b)

No

c)

Only in accordance with the AMM

9.

What causes the gradual darkening effect in a synthetic oil?

a)

Collection of coke, carbon and lacquer

b)

Oxygen absorption

c)

High viscosity

d)

Water contamination

10.

What factors can result in increased oil consumption

a)

Higher RPM & Temperatures`

b)

Larger Clearances

c)

Less Viscosity

d)

Ambient Pressure

11.

What must you take into account when handling synthetic oils?

a)

Read the SDS and use PPE

b)

Never use silicon-based grease

c)

Clean up spills immediately

12.

What is the alternative name for JET B fuel?

a)

AVGAS

b)

AVTURB

c)

JET A1

d)

AVTAG

13.

What are the disadvantages to using wide cut fuels in gas turbine engines?

a)

Greater losses to evaporation at high altitudes

b)

Greater risk of fire during handling

c)

Crashes of planes with wide cut fuels were less survivable

d)

Has a lower maximum freezing point than JET A1

14.

What colour is used to identify JET A-1 fuel?

a)

Grey

b)

Yellow

c)

Black

d)

White

15.

What colour is used to identify JET B fuel

a)

White

b)

Black

c)

Grey

d)

Yellow

16.

For what purpose are fuel tanks fitted with a National Advisory Commitment for Aeronautics (NACA) scoop?

a)

Increase vapour pressure

b)

Reduce vapour pressure

c)

Cool fuel tank

d)

Overflow for the fuel tank

17.

Jet A-1 has a ___ flash point than AVGAS

a)

Higher

b)

Lower

c)

Equal

18.

What is the easiest and most common method to find contaminants in a fuel sample?

a)

Water finding paste

b)

Dip stick

c)

Drain into a clear glass container

19.

Water contamination can be present in two forms. Which form can form into ice and be detrimental to engine operations?

a)

Free/Suspended

b)

Dissolved

20.

What is the correct order of earthing when refueling an aircraft?

a)

Person to Ground

Truck to Ground

Truck to Aircraft

Nozzle to Aircraft

b)

Nozzle to Aircraft

Truck to Aircraft

Truck to Ground

Person to Ground

c)

Person to Ground

Truck to Aircraft

Truck to Ground

Nozzle to Aircraft

21.

Suction lines from a fuel storage tank must be placed ___ the bottom of the tank

a)

Above

b)

Below

c)

Level with

22.

Fuel spills are an environmental and fire risk. What must you do immediately?

a)

Report to your supervisor & Clean up

b)

Evacuate the ramp

c)

Evacuate the aircraft

d)

Contact the local fire authority

23.

This image is an example of what type of contaminant?

a)

Microbial

b)

Swarf

c)

Dissolved Water

d)

Free water

24.

In a wet-sump system, where is the oil supply located?

a)

At the highest point in the engine

b)

In the middle of the engine

c)

In the rear of the engine

d)

At the lowest point of the engine

25.

In a dry-sump system, where is the oil supply located?

a)

At the highest point in the engine

b)

Separate Oil Reservoir within the Engine

c)

Separate Oil Reservoir externally

d)

At the lowest point of the engine

26.

The component in a lubrication system used to hold sufficient oil to allow for engine consumption at maximum flight operation and duration is called

a)

Wet sump

b)

Dry sump

c)

Oil tank

d)

Oil reservoir

27.

"Once the oil has lubricated the main bearings, it drains to low-lying areas, where scavenge pumps route it back to the sump or gearbox."

Which type of sump system is this?

a)

Wet

b)

Dry

c)

Moist?

28.

All oil reservoirs have an expansion space of at least...

a)

10% or 0.5gal

b)

5% or 0.10 gal

c)

10% or 10 gal

d)

5% or 0.5 gal