Systems Flashcards

(26 cards)

1
Q

234 Engines

A

Avco Lycoming AL5512 gas turbine engines

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2
Q

Fuel Capacity

A

UT two 500gal tanks (489 usable)

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3
Q

Cargo hook assembly is rated for

A

28,000lbs

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4
Q

Drive system consists of

A

5 transmissions, 2 engine drive shafts, 9 synchronizing shafts, and a vert shaft

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5
Q

Dimensions rotors turning

A

99ft long
60ft wide

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6
Q

How many oil coolers in the aft pylon

A

4

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7
Q

APU

A

Solar T62-T-2C

95 SHP

Includes a hydraulic motor/pump, a fuel control unit, and an automatic electronic sequencing unit

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8
Q

AGB

A

Auxiliary Gearbox

Provides complete electrical and hydraulic power for main engine start, and for flight control and electrical checks on ground

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9
Q

Reduction Drive Assembly

A

Drives the accessory drive, APU oil pump, APU speed detector and fuel control, and reduces RPM from 56,000 to 6000 and 4200.

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10
Q

Hydraulic APU Motor/Pump

A

Acts as a motor to start the APU

Acts as a pump to turn the AGB

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11
Q

What happens when the pilot moves the APU switch to the START position?

A

The airframe fuel pump takes fuel from the LH tank and pressurizes it to the fuel control assembly

This action also opens the hydraulic start valve, activating the hydraulic motor pump.

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12
Q

At what engine speed does the start fuel valve open?

A

5% engine speed

This is when a single igniter is activated to ignite vaporized fuel.

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13
Q

What occurs at 14% APU rated speed?

A

The APU main fuel solenoid valve opens, allowing maximum fuel flow to the fuel manifold

This flow is directed to six vaporizing tubes in the combustor.

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14
Q

How is fuel flow controlled after the main fuel solenoid valve opens?

A

By engine compressor discharge pressure acting on the diaphragm in the APU governor section

Fuel flow increases in proportion to increasing compressor pressure.

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15
Q

What happens at 70% rated speed?

A

The igniter, hydraulic pump, and start fuel solenoid are all switched off

Main injectors continue to supply fuel for combustion.

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16
Q

What indicates a failure to start the APU?

A

A fault indicator on the ESU will indicate ‘Fail to Start’ if the engine fails to reach 90% rated speed in 40 seconds

This is part of the fault logic in the ESU.

17
Q

How is engine speed governed in the APU?

A

By a flyweight assembly within the governor housing

The assembly reacts to changes in centrifugal force as the APU is loaded.

18
Q

What happens when the APU rotor shaft slows down?

A

A reduction of centrifugal force acting on the flyweights occurs

This reduction is felt through a bearing plate and valve assembly.

19
Q

Fill in the blank: The governor control spring expands, moving the fuel metering valve to _______.

A

increase fuel flow

This action continues until normal engine speed is regained.

20
Q

True or False: The same action that increases fuel flow can also protect the engine from overspeed.

A

True

The governor mechanism works in reverse to protect the engine.

22
Q

What happens when the engine is suddenly offloaded?

A

A minimum flow orifice installed in the fuel control housing bypasses the governor, allowing a small amount of fuel under pump pressure to flow to the main fuel nozzles.

23
Q

What is the function of aneroid bellows in the fuel system?

A

They register changes in ambient air pressure and increase or decrease the fuel flow accordingly.

24
Q

How does a pilot shut down the APU?

A

The pilot moves the OFF/RUN/START switch from RUN to OFF position.

25
What effect does moving the OFF/RUN/START switch to OFF have on the fuel pump?
It removes the 28-volt DC power supply from the airframe fuel pump solenoid, causing the fuel pump to stop.
26
What happens to the valve when the fuel pump stops?
The fuel solenoid closes the valve and starves the APU of fuel.