Engine Flashcards

1
Q

Max thrust continuous?

A

13,800 lbs

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2
Q

How much thrust do the engines produce?

A

13,800-14,200 lbs (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 channel 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 approach? When does it appear?

A

The minimum N1 for bleed requirements in icing conditions

Configured for landing less than 1200’ RA ( when anti-ice is ON)

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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 (in flight only)

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13
Q

Does the FADEC provide engine start protection?

A

Only on 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 start on the ground?

A

FADEC will not allow FF if ITT is greater than 120 degrees C

FADEC will automatically dry motor engine and introduce fuel when ITT is less than 120 degrees C

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15
Q

Describe the engine start sequence

A
1.start switch momentarily to START:
7% N2......ignition
20% N2 ......fuel flow
20% N2 +5 sec.....light off
50% N2....... Ignition off, Starter Cut-Out
2. Engine stabilizes
N1.....27%
ITT.....460 degrees C
N2.....62% 
FF.......550 lbs/hour
Oil pressure..... Greater than 25 psi
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16
Q

What does WML mean on the engine indications?

A

Windmilling engine
The FADEC has detected a flame-out and is attempting to auto re-light, or
An assisted start has been commanded

17
Q

What provides underspeed and overspeed protection?

A

The FADEC via the FMU

Approximately 52% N2 and 102% N2 respectively

18
Q

What happens after 3 overspeed detection events?

A

FADEC will no re-light the engine

19
Q

What heats the fuel and cools the engine oil?

A

Fuel/oil heat exchanger

20
Q

What is ATTCS? What controls it?

A

Automatic Take-off Thrust Control System
Provides max thrust reserve (RSV) according to current rate previously selected in the MCDU
FADEC controlled

21
Q

What will trigger an ATTCS event?

A

N1 difference greater than 15% between engines
Engine failure during TOGA
Windshear detected

22
Q

When is thrust reverse available?

A

Weight-on-wheels (ground use only)

23
Q

What happens if a thrust reverser inadvertently deploys?

A

FADEC limits respective engine thrust to IDLE

24
Q

What engine thrust rating(s) may only be used for 10 minutes?

A

TO-1
TO-RSV (TL beyond TOGA)
GA (two-engine go-around)
GA-RSV (one-engine go-around or windshear)

25
Q

What is FLEX?

A

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

26
Q

Can the FLEX thrust be reduced lower than CLB thrust?

A

No

27
Q

What type of engines are on the aircraft?

A

2 GE CF34-8E5

Hi-Bypass, 2-spool, axial-flow, turbo-fan

28
Q

Max Thrust RSV?

A

14,200 lbs at ISA

29
Q

Thrust reverser speeds? Idle and stow

A

Idle: 60kts

Stowed: 30 kts

30
Q

Minimum oil pressure?

A

25 psi