Engine Flashcards

1
Q

How many Oil Sumps are there and How many Bearings

A

SUMP A = Bearings 1,2,3
SUMP B = Bearing 4
SUMP C = Bearing 5

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2
Q

What is on AGB

A

Fuel EDP, IDG, ATS, Hydraulic EDP, Lube & Scavenge, Chip Detector

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3
Q

What does the Oil System lubricate

A

AGB and 5 Bearings

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4
Q

What is Vx and Vy

A
Vx = Green Dot
Vy = Green Dot + 50kts
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5
Q

What are Thrust Reversers Lockouts used for

A

They are Red and used to denote a MEL’d TR

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6
Q

What does a Cyan Line on the N1 gauge represent during Approach and when does it appear

A

Min N1 to meet Bleed Requirements and will appear when configured for Landing < 1200’ RA when A/I is ON

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7
Q

What within FADEC provides the Under - Overspeed Protection and at what %

A

FMU in the FADEC 52% (Underspeed) and 102% (Overspeed) N2

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8
Q

What 4 Scenarios does the ATTCS command RSV Power Automatic

A
Automatic:
15% Difference of N1 values
OEI T/O
OEI G/A
Windshear

Manual:
Thrust Levers to Max detent

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9
Q

Which IDLEs increase Min N1 due to Ice speeds

A

FLT IDLE & APPROACH IDLE for Bleed Protection

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10
Q

What is Max Oil qty AMS Usable Oil qty

A
Max = 10.5 qts
Usable = 7.5 qts
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11
Q

What does a Cyan OFF on the N1 EICAS indication indicate

A

Cyan OFF indication is displayed when the Engine is shutdown in FLT by Pilot action

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12
Q

What are 2 Major Components of the Starter System

A

Starter Control Valve (SCV) and Air Turbine Starter (ATS)

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13
Q

What is the purpose of the SCV

A

Opens to allow Bleed Air from APU, Cross side Engine or GRD source to Power the ATS

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14
Q

Describe N2 Spool

A

10 Stage Axial Flow Compressor with a 2 Stage High Pressure Turbine

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15
Q

Describe the Variable Geometry Actuators

A

2 VGA’s per Engine, master/slave configuration, Fuel Pressure driven that control Compressor Stator Vanes Stage 1 - 4

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16
Q

Describe the Interlock function of the FADEC

A

Prevents inadvertent deployment of the Thrust Reversers 2 main actuators and Cowl lock. Cowl lock itself is the main defense against TR deployment

17
Q

How many Fan blades are on the CF-34 8E5

A

28 Fan Blades

18
Q

Describe N1 Spool

A

Single Stage Turbofan and 4 Low Pressure Turbines

19
Q

How are TR activated and what type are they

A

Actuated by Hydraulic Power and are of the Cascade type

20
Q

Where is the Oil Pressurized

A

In the Oil Lubrication Pump then passes thru the Filter then Heat Exchanger (bottom right side of Eng.) then dispersed through Engine