Engine Part 2 Flashcards

1
Q

What supplies fuel directly to the main fuel control system?

A

The main fuel pump (engine driven)

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2
Q

What are the two major systems of the main fuel control system?

A

The computer section and the fuel emtering seciton

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3
Q

Describe the main fuel control system’s computer section:

A

The computer section senses engine inlet air temperature (T2), compressor discharge temperature (P3), engine speed and throttle position to determine the metering valves position and then schedules the correct fuel flow through the entire range of engin operaiton

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4
Q

Describe the fuel metering section of the main fuel control system:

A

It delievers the computer fuel flow to the engine

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5
Q

What is an auxiliary function of the main fuel control system?

A

To schedule the variable geometry system (VGS).

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6
Q

How does the main fuel control system schedule the VGS?

A

Main fuel pump pressure as computed by the main fuel contol computer is diverted to the VGS actuator to operate the variable inlet guide vanes and the bleed air valves.

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7
Q

How does the overspeed governor work in the fuel system?

A

It mechanically monitors engine speed, in the event that an engine exceeds the maximum RPM, the overspeed governor will descrease fuel flow to the engine mainifold to reduce engine speed.

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8
Q

What two conditions must be met for the afterburner system to operate?

A
  1. Throttle must be in the MAX range

2. RPM must be stabilized at MIL

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9
Q

After afterburner initiation, when does fuel flow to the main afterburner spraybars?

A

Only when the nozzles are opening, a nozzle feedback cable provides this signal to the afterburner fuel control

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10
Q

What is the principle source for fuel after afterburner?

A

The 16 main afterburner spraybars.

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11
Q

By how much does the afterburner augment engine thrust?

A

By 5 to 40 percent greater than MIL power

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12
Q

What portion of the afterburner spraybar system is designed to initiate afterburning and prevent afterburner blowout?

A

The 4 pilot burner spraybars

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13
Q

What does the T38 airstart envelope depend on?

A

Airspeed, altitude, and air density

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14
Q

If you have one engine operating and are attempting an airstart, how many airstart attempts are you limited to?

A

You are not limited

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15
Q

If a dual engine flameout occurs, what engine should you start first? Why?

A

The right engine. To take advantage of the static inverter powering the right engine autosyn instruments

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16
Q

If you start the left engine first (or the right one fails to start) in a dual flameout airstart, what is the only indication of a sucessful start?

A

Rising RPM and EGT until…

The left generator begins to cut in at the 43 to 48% to view the AC instrument power indications

17
Q

What 4 things should you remember to aid in a succesful airstart?

A
  1. Descend below 25,000 ft. If the engine does not start at an altitude of 25,000, it may start with additional attempts at lower altitudes (10,000 feet or lower)
  2. Maintain an airspeed that will produce a minimum of 12% RPM (18-20% is the heart of the airstart envelope at all altitudes)
  3. Consider the electrical ignition source avaiable and do not rush the start - allow the full 30-second cycle
  4. If at extremely low altitude or a critical need for thrust exists, use the Alternate Airstart/Loss of Thrust (Low Altitude) procedure
18
Q

How long should you leave the throttles in IDLE before aborting an airstart attempt?

What can you check during this wait time?

A

30 seconds

Recheck the battery switch on

19
Q

What does the T2 sensor do?

A

Provides an input to the main fuel control and limits fuel flow as a function of inlet temperature

20
Q

What does the fuel flow transmitter measure?

A

Only main engine flow, not afterburner fuel flow

21
Q

How does the oil cooler work?

A

When fuel leaves the fuel flow transmitter, it passes through a honeycomb passageway. The hot engine oil passes through adjoining passage ways, allows a heat exchange to occur, cooling down the oil and heating up the fuel.

22
Q

What is the purpose of the pressurization and drain (P&D) valve?

A

The main fuel P&D valve prevents fow to the fuel manifold until the remainder of the fuel system is up to pressure. During engine shutdown, the P&D opens and dumps unburned fuel from the fuel manifold

23
Q

How does the T38 control fuel flow for afterburner operation?

A

It is done so by the afterburner fuel control (AFC) unit. The AFC schedules fuel flow to the afterburner main and pilot spray bars as a function of power lever angle and compressor discharge pressure. When the T5 system overrides the hydromechancial control of the variable exahust nozzle, it opens the nozzle. This action causes the AFC computer section to send a signal to the metering section to change the position of the lockout valve, controling fuel flow

24
Q

What is the relationship between the oil pump, tachometer generator, and the T5 alternator?

A

They all share the same drive shaft

25
Q

What are some common indications of a T5 failure?

A

High EGT (above 650) and a closed nozzle at or above approx 97% RPM.

26
Q

Will the afterburner light with a T5 system failure?

A

No

27
Q

If your nozzle is stuck open, what usually results?

A

Low EGT
High RPM
Reduce amount of available thrust

28
Q

If your nozzle is stuck closed, what usually results?

A

High EGT
High RPM
Possible of an engine overtemp, especially during rollout after landing

29
Q

At full MAX, what is the approximate fuel flow for each engine?

A

7300 PPH