Installation Flashcards

1
Q

How are multiple
Engines identified on the same aircraft

A

Left (port) engine is No1
Right (Starboard) engine is No2

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2
Q

In what 2 ways can an engine be referred to as

A

Engine - without any supporting accessories
Engine change unit - containing supporting accessories

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3
Q

What pre installation checks must be carried out before installing a replacement engine

A

Log cards
Modification state
Checklist - Topic 3
Removed ECU

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4
Q

What checks must be carried out before ground running the replaced engine?

A

Independent inspections
Loose article check
Fuel flow
Tool control
MoDF700

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5
Q

What are blanks used for and when

A

To prevent the ingress of dirt and moisture, as soon as pipes or tubes are disconnected

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6
Q

What can lead to misalignment of the engine

A

Degradation of vibration absorbing materials

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7
Q

What 2 mounts attach the engine to the fuselage

A

Rear
Forward

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8
Q

What methods can be used to absorb the torque reaction between the engine and airframe?

A

Twin engine mount
Thrust bar

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9
Q

What is a gimbal ring used for

A

To connect the engine front mounting and the MRGB support assembly

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10
Q

What is a side stay and its purpose

A

Used to laterally restraint the engine
Supports lugs on spherical bearings to keep the engine still

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11
Q

What is a vibration mount used for

A

Carries the vertical weight of the engine, absorbs vibrations travelling to the fuselage

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12
Q

How is vibration minimised through the vibration mount

A

Rubber dampeners

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13
Q

What should be done before lifting an engine

A

Examine lifting points on ECU
Pre-use check on lifting tackle
Correct lifting beam
PPE, do not stand underneath

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14
Q

Where are lifting points located on an engine

A

Located around the centre of balance

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15
Q

What is ground running

A

Running the engines without flying the aircraft, for great range of testing and maintenance

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16
Q

Why is ground running better than flying the aircraft

A

Risk to life is much lower

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17
Q

What does a typical ground team consist of

A

Supervisor
Operator
Safety person

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18
Q

Who will the operator of the ground test be

19
Q

What are the 4 danger areas of a helicopter

A

Main rotor
Tail rotor
Air intakes
Exhaust

20
Q

Where should you leave the rotor disk while the engine is running?

21
Q

What is blade sailing

A

Gusts of wind cause the rotor blades to drop below head height while rotating

22
Q

What are the typical reasons for ground running

A

Engine testing after installation
Engine testing after component change
Engine accessories testing
Carry out maintenance
Verify faults

23
Q

What is a wet start

A

Residual fuel in the combustion chamber following a failed attempt to start

24
Q

What is a vent run

A

Using compressor air to blow fuel out of the system. Done using starter motor

25
What is a drying out run
Compressor wash followed by full engine run, preventing corrosion
26
What is a hung start
Engine does not accelerate during start (can be caused by fuel starvation)
27
What is a hot start
Turbine temperature too high, HP cock closed and reason identified
28
What is run down time
Closing of the hp cock to the engine stopping rotating
29
What are the ISA values for temperature and pressure
15 degrees 1013.25 millibar
30
What is placard data
The datum information for all future tests and to gauge the engines performance and condition, based on a test bed run or installed ground run
31
What is a flat rating
The extra power that is available for use by a pilot on a hot day or in higher elevations
32
What is the purpose of compressor washing
Remove accumulation of salt dust and industrial products
33
What are some fluids used for typical washing
ZOK 27 Demineralised water Methanol - cold
34
What is a washing rig normally pressurised to
35 lbs in - 40 lbs in
35
What is EDF
Early detection faliure
36
What is SOAP
Spectrometric Oil Analysis Program
37
What are the advantages of WDM
Minimise cost of remedial action Assist with maintenance plans Assist repair agencies Reduce contamination and component damage
38
When is EFD normally carried out
IAW the AMM After post installation ground run On completion of 5-10 flying hours On recommendation of 1710 NAS Upon heavy landing / bird strike / over torque
39
When should the compressor be washed
IAW AMM Salt laden atmosphere In industrial areas Sudden drop in engine performance
40
What is the minimum capacity you should pour into the juniper rig
25 litres
41
42
When should oil be sampled from the aircraft system
Within 30 minutes of shut down After a running time of at least 15 minutes Before any replenishment
43
What mod form accompanies SOAP bottles
MOD F730 - accompanies bottle MOD F730C - adhesive label for each bottle