Block 4 - EA-18G Power Plants Flashcards

1
Q

Model type engine used in the Growler

A

F414-GE-400

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2
Q

Three modes of operation for the Auxiliary Power Unit (APU)

A

1) GMM - Ground
2) MES - Main Engine Start
3) ECS - Environmental Control System

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3
Q

Purpose of the In-Flight Refueling (IFR) probe

A

Allows for refueling while flying

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4
Q

What does the Aircraft Fuel Storage System consist of?

A
  • 4 main bags/fuel cells
  • 2 wing tanks
  • 5 external drop tanks
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5
Q

Purpose of the foam-lined wing tanks

A

Allows aircraft to self seal small external damage

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6
Q

What does the Secondary Power Systems consist of?

A
  • Auxiliary Power Unit (APU)
  • Airframe Mounted Accessory Drive (AMAD)
  • Secondary Power Compressed Air
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7
Q

Purpose of the APU

A

Gas Turbine Engine; Supplies air to ECS

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8
Q

Purpose of the AMAD

A

Transmits power to engine for starting

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9
Q

Purpose of Secondary Power Compressed Air

A

Provides pneumatic power for operating the ECS

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10
Q

What are the related systems in the Power Plant?

A
  • Ignition
  • Lubrication
  • Main Fuel
  • Afterburner Fuel
  • Variable Exhaust Nozzle (VEN)
  • Variable Geometry
  • Anti-Icing
  • Full Authority Digital Engine Control (FADEC)
  • Throttle
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11
Q

Explain VEN

A

Cam and link-positioned hinged-flap, convergent-divergent nozzle mounted to the aft end of the afterburner case.

Helps push exhaust gases out the plane

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12
Q

Explain Variable Geometry

A

Consists of Fan Variable Geometry (FVG) and Compressor Variable Geometry (CVG)

  • FVG provides better efficiency of the fan
  • CVG provides better efficiency of the compressor
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13
Q

Explain Full Authority Digital Engine Control (FADEC)

A

Receives aircraft and engine sensor information and determines what will help the engine operate to its full potential

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14
Q

Components driven by the AMAD

A

Used to drive:

  • Fuel boost / Motive flow pump
  • Electrical generator
  • 3000/5000 psi hydraulic pump
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15
Q

How does the AMAD interface with the APU and engine?

A

Pneumatically connected to APU through the Air Turbine Starts (ATS)

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16
Q

Safety precautions that must be observed during engine ground turn-up

A
  • PPE is required
  • Distance of 9 ft radius from intakes
  • 25 ft radius at MIL or MAX to prevent being pulled in
17
Q

Safety precautions that apply to fueling and defueling

A
  • PPE is required

- Must not be done within 100 ft of radio equipment or 300 ft from ground RADAR equipment