Power plant Flashcards

1
Q

Identify the three engine mounted components that have impending bypass indicators that should be checked on pre-flight inspection?

A

Main fuel filter
In-line fuel filter
Main oil filter

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2
Q

Identify at what Power Turbine Inlet Temperature, time limited operation begins?

A

Above 816 deg C

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3
Q

Identify the component that supplies the engine oil pressure signal that is seen on the powertrain portion of the engine interment page?

A

Oil pressure transmitter

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4
Q

What does the load share switch on the FADEC control panel allow the pilot to choose for engine load share?

A

TRQ

PTIT

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5
Q

In relation to FADEC system what component is installed in the flight control closet for the purpose of sending thrust position and rate information to the ECU’s to eliminating rotor droop?

A

Thrust CPT

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6
Q

Before turning on the backup power switch during engine startup what CAUTION’s are you looking for to be ACTIVE?

A

1 and 2 FADEC Cautions

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7
Q

What Position should the ECL’s be in to see Bit Codes on the DECU/ECU’S?

A

Ground (ground to flight)

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8
Q

Engine FAULT detected by the DECU/ECU that does not impact the normal control of the engine is a _____ Fault.

A

Soft fault

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9
Q

An engine FAULT that could cause unacceptable engine or aircraft performance is a ______ Fault.

A

Hard fault

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10
Q

When the Ignition Lock Switch (key) is in and ON this supplies power to the circuit of what two components on the engine for the purpose of engine starting?

A

ignition Exciters and start fuel solenoids

Spark and fuel

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11
Q

Explain why you should delay turning second generator ON for 2 seconds when turning APU GEN Off and turning on Main GEN’s?

A

Will give the ECU time to sample power without causing a soft fault

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12
Q

Identify the FADEC Modes of operation the Bleed Band system automatically operates?

A
Primary modes (“snaps”)
Reversionary modes (“modulates”)
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13
Q

When ENG1 or ENG2 FADEC and/or REV1 or REV2 FAIL Cautions are active, what switch can be toggled to reboot the microprocessor’s in the DECU/ECU?

A

PRI/REV switch

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14
Q

With a FADEC 1 or FADEC 2 failure, what does the pilot use to keep the engines matched in torque or PTIT Load shear?

A

INC/DEC switch

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15
Q

In the event of an engine compressor stall what is the first step?

A
  1. Thrust CONT lever — Reduce.
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16
Q

Identify the Underlined Steps for ABORT START.

A

(1) 1. ENG COND Lever — STOP.

2) 2. ENG START Switch — Motor (if high PTIT is indicated

17
Q

Identify the Underlined Steps for EMER ENG SHUTDOWN.

A

ENG COND Lever -Stop

Fire PULL Handle-Pull

Fire PULL Handle-Twist

18
Q

FADEC
HMA
RDPS
AGB

A

Full Authority Digital Electronic Control
Hydromechanical Metering Assembly
Ratio Detector Power Supply
Accessory Gear Box

19
Q

What is the efficacy of EAPS and how are they mounted?

A

EAPS is 94% effective at filtering the air, EAPS is mounted on a rail system

20
Q

What oil do the engines use?

A

Green can oil

21
Q

Where do NG indications come from?

A

from the NG speed sensor on the back of the oil pump

22
Q

If you are in a fixed fuel situation how do you reset the computer?

A

cycle the PRI/REV switch

23
Q

what is the purpose of the oil flow programming valve?

A

prevent coking

24
Q

what inhibits NP overspeed?

A

overspeed solenoid valve

25
Q

What should you refer to when checking the fire bottle suppression pressure?

A

The checklist

26
Q

what component provides fuel for engine start?

A

start fuel solenoid valve

27
Q

How do we detect PTIT?

A

Probes and thermal bus bar

28
Q

What provides engine torque data to EICAS?

A

Torque junction box

29
Q

during pre-flight inspection what are you checking engine fluid lines for?

A

Leaks and chaffing

30
Q

functions of liquid to liquid cooler?

A

cool oil and heat fuel