Engine Flashcards

1
Q

What types of engines are on the aircraft?

A

2 General Electric CF-34-8E5

-HI-bypass, 2 spool, axial flow, turbo fan

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2
Q

How much thrust do the engines produce?

A

13,800-14,200lbs (ISA)

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3
Q

Describe N1 spool

A
  • Single stage fan

- 4 stage LP turbine

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4
Q

Describe N2 spool

A
  • 10-stage compressor (gas generator)

- 2-stage HP turbine

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5
Q

How many igniters per engine?

A

2 per engine

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6
Q

How many igniters activate for engine start?

A

Ground - 1 igniter (switch in Auto)

Flight - 2 igniters (switch in Auto)

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7
Q

What happens when the ignition switch is selected to OVRD?

A

Activates both igniters on the ground or in flight

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8
Q

Can the igniters be turned off during flight?

A
  • The switch may be moved to the OFF position but the FADEC disregards the command
  • The OFF position is used for DRY motoring on the ground only
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9
Q

What controls the engine?

A
  • A two channel FADEC

- One channel is active and the other remains in standby as a backup

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10
Q

Is only one FADEC channel used every flight?

A

NO. They automatically alternate with each engine start

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11
Q

What does the Cyan line on the N1 gauge represent during the approach? When does it appear?

A
  • The minimum N1 for bleed requirements in icing conditions

- Configured for landing

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12
Q

What sources are available for engine starting?

A
  • APU
  • Ground Source (Huffer cart or Air bottle)
  • Opposite engine
  • Windmill start
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13
Q

Does the FADEC provide engine start protection?

A

Only on the ground for a hot start, hung start, or no light Off

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14
Q

What will the FADEC automatically do in case of a Hot-start?

A
  • FADEC will not allow FF if ITT > 120°C

- FADEC will automatically dry motor engine and introduce fuel when ITT

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15
Q

What does WML mean on the engine indications?

A
  • Windmilling Engine
  • The FADEC has detected a flame-out and is attempting an auto-relight, or
  • An assisted start has been commanded
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16
Q

What provides under-speed and over-speed protection?

A
  • The FADEC via the FMU

- Approximately 52% N2 and 102% N2 respectively

17
Q

What happens after 3 overspeed detection events?

A

FADEC will NOT re-light the engine

18
Q

What heats the fuel and cools the engine oil?

A

Fuel/oil Heat exchanger

19
Q

What is ATTCS? What controls it?

A
  • Automatic Takeoff Thrust Control System
  • Provides Max thrust reserve (RSV) according to current rate previously selected via the MCDU
  • FADEC controlled
20
Q

What will trigger an ATTCS event?

A
  • N1 difference > 15% between engines
  • Engine failure during TOGA
  • Windshear detected
21
Q

When is thrust reverse available?

A

Weight on Wheels (WOW)

22
Q

What happens if a thrust reverser inadvertently deploys?

A

FADEC limits respective engine thrust to idle

23
Q

What engine thrust rating(s) may only be used for 5 minutes?

A
  • TO 1
  • TO 2
  • TO-RSV (TL beyond TOGA)
  • GA (2 engine go around)
  • GA-RSV (one engine GA or windshear)
24
Q

What is FLEX?

A

Reduced T/O thrust based on assumed temperature (telling the FADEC that it is warmer than it actually is so it will reduce the thrust)

25
Q

Can the FLEX thrust be reduced lower than CLB thrust?

A

NO