Engine System Flashcards

(32 cards)

1
Q

N1 Componets

A

Fan
Low Pressure Compressor
Low Pressure Turbine

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2
Q

N2 Componets

A

High Pressure Compressor
High Pressure Turbine

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3
Q

What does N2 Drive

A

Engine Gearbox

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4
Q

What Starts N2 Compressor?

A

Bleed Air Power Starter

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5
Q

Accessory Gear Box Components

A

Oil Pump
Fuel Pump
Integrated Drive Generator
Starter
Hydraulic Pump

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6
Q

What Operates the Accessory Gear Box

A

N2 powers Inlet Gearbox rotor and Transfer Gearbox

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7
Q

Other Components of Engine

A

Thrust Reverse
Fire/Overheat Protection
Pneumatic Ducts
Cowling
Common and Central Display Units
Potable Water Pressurization Tubes

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8
Q

How many EEC’s

A

2 Controllers

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9
Q

Which EEC is the main?

A

Alternate between every start attempt and automatically transfer for failures

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10
Q

EEC Modes

A

Normal
Soft Alternate
Hard Alternate
Idle

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11
Q

Normal EEC Mode

A

Sets N1 based on flight conditions and bleed air requirements.
Compares actual to commanded N1 and adjusts HMU accordingly

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12
Q

Soft Alternate

A

Required signals are not available. Uses the last valid flight condition for parameters.

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13
Q

How to get into Hard Alternate EEC Mode?

A

Thrust Levers to Idle
Manually Select EEC Switch

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14
Q

EEC Protection/Limitations

A

Some Overboost protection but only use for emergencies (EGPWS) in Alternate
No EGT Exceedance

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15
Q

Hard Alternate EEC Mode

A

Alternate mode thrust schedule
Always equal to or greater thrust than normal mode positions

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15
Q

When are you in Ground Idle?

A

Ground operations
5 seconds after rollout

16
Q

Idle Thrust

A

Ground
Flight
Approach

17
Q

When are you in Flight Idle

A

Most Phases of flight

18
Q

When are you in Approach Idle

A

Below 15,500’ MSL with the landing gear down or the flaps in the landing position
Engine Anti-Ice On
Below 15,000’ MSL if there is an issue with the signal

19
Q

Importance of Approach Idle

A

Gives a higher minimum thrust to decrease spool up time in case of a go around

19
Q

Engine Fuel System Flow

A

Fuel Tank Pumps
Engine Spar Valve (mounted in the engine mounting wing stations)
First stage engine fuel pump
IDG Oil Fuel heat exchanger
Main Engine Oil Fuel Heat exchanger
Fuel Filter
Second State Engine Fuel Pump
Hydromechanical Unit
Engine Fuel Shutoff Valve
Fuel Flow Transmitter

20
Q

Purpose of Engine Oil

A

Cool and lubricate engine bearings and accessory gear box

21
Q

Engine Oil Flow

A

Engine Driven Oil Pump
Oil Temperature Sensor
Oil Pressure Sensor
Bearings/Gear Box
Scavenge Pump
Filter
Main Engine Oil Cooler

22
Q

What do starts requrie?

A

Pressurized air
Electrical Power

23
Engine Start Switch Modes
Ground Auto Cont Flight
24
Ground Start Mode
Close Engine Bleed Air Valve Open Start Valve (Engine Start Valve Alert) Starter rotates the N2 Compressor In Flight- Both Powered On Ground - Selected Powered
25
Auto Start Mode
Ignition Normally Off Both Active When: -Uncomanded Rapid N2 decrease -N2 between 57 and 50% -N2 between Idle and 5% in flight One Active when: -Flaps not up below 18,000' -Engine Anti Ice On
26
CONT Start Mode
Ignition to selected igniter Both ignited for engine fail
27
FLT Start Mode
Both Ignited
28
When are thrust reversers active?
10'RA or Air Ground Safety sensor in ground
29
Thrust Reverser Process
Electromechanical Lock Release Isolation Valve opens Hydraulic pressure unlocks and deploys reverser Interlock mechanism restricts movement
30
Reverser Lights
On for stowing Reverse for 10 seconds. 12 seconds+ is a malfunction