Engines And General Knowledge Flashcards

1
Q

What kind of engines power the CRJ-700?

A

2 General Electric CF34-8C5B1 High Bypass Turbofans.

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2
Q

What is the range of the CRJ-700?

A

Standard 1685 nm.

Extended 1985 nm.

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3
Q

What are the dimensions of the CRJ-700?

A

Height 24’10”.
Length 106’8”.
Span 76’3”.

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4
Q

What are the intake and exhaust danger areas?

A

Idle - Intake 13 ft exhaust 100 ft.

Maximum - Intake 26 ft exhaust 300 ft.

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5
Q

What can be controlled from the flight attendant’s control panel?

A

Cabin lighting.
Emergency lighting.
Main passenger door.
Interphone system.

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6
Q

What is the maximum speed and altitude of the CRJ550?

A

0.85 Mach.

41,000 ft.

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7
Q

What is the minimum pavement width required for a 180 degree turn?

A

75 ft.

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8
Q

What is the size of the APU exhaust danger area?

A

15 ft.

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9
Q

What emergency equipment is located behind the Captain’s and First Officer’s seats.

A

CA - Flashlight and PBE.

FO - Flashlight, crash axe and fire extinguiser.

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10
Q

How much thrust is developed by each engine?

A

12,670 lb at take-off.
13,790 at APR.
13,280 at MCT.

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11
Q

Decribe the major sections of the N1 and N2 spools.

A

N1 - Outer section including 1 large turbine and a 4 stage low pressure turbine.
N2 - Inner section including a 10 stage axial compressor and a 2 stage high pressure turbine.

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12
Q

What components are located on the accesory gearbox?

A
Oil pump.
Fuel pump.
Hydraulic pump.
FADEC alternator.
Integrated Drive Generator (IDG).
Fuel metering unit.
Air Turbine Starter.
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13
Q

What is the purpose of the N2 variable geometry?

A

To prevent compressor stall and surges.

It also improves overall efficiency.

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14
Q

How the is the N2 variable geometry operated?

A

Controlled by FADEC.

Fuel is used to actuate the vanes.

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15
Q

Where is the N2 varibale gemoetry located?

A

On the first 4 stages of the N2 compressor.

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16
Q

What does the FADEC control?

A

Fuel control system.
Engine start and ignition system.
Compressor airflow.

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17
Q

How many chanels does each FADEC have and when do they operate?

A

Two, an A and B channel.
One channel is ‘in control’ the other is in standby.
Both channels simultaneously operate and share data but only the ‘in control’ channel provides actual engine commands.

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18
Q

When does the FADEC’s standby channel provide commands to the engine?

A

In an engine overspeed condition. The result is an engine flame out then an auto relight once the N2 spools below a set threshold.

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19
Q

How is the FADEC powered?

A

Below 50% N2 RPM by the aircraft’s electrical system.

Above 50% N2 RPM by it’s own alternator driven by it’s onside engine.

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20
Q

When does the FADEC stop updating the target thrust?

A

At 65 kt on take-off until 400 ft AGL or the thrust levers are taken out of the detent.

21
Q

What are the different N2 idle speeds?

A

Flight idle - In flight, gear up, flaps at 20 degrees or less.
Approach idle - In flight, gear down OR flaps greater than 20 degrees.
Landing idle - In between ground and reverse idle.
Reverse idle - Weight on wheels or wheel spin up, thrust reverser lever is raised and the engine reverser cowl is not stowed.
Ground idle - When on ground and thrust lever is in idle.

22
Q

What does the FADEC do in the event of an engine failure?

A

Depending upon thrust lever position:
In cruise - a proportional increase in N1 speed.
In climb detent - maximum continuous thrust.
In TOGA - APR.

23
Q

When does the FADEC detect an N1 speed mismatch?

A

When the N1 on each engine differ by 15%.

24
Q

When does the FADEC command APR to an engine?

A

When the difference in N1 is greater than 15%.

When thrust levers are in the MAX PWR detent.

25
Q

When will the FADEC synchronise N1 or N2?

A

When the SYNCH switch is selected to either N1 or N2 and the thrust levers are in the cruise range.
N1 must be within 1.5% of eachother and N2 must be within 2.5% of eachother.

26
Q

What is required for the FADEC to start the engine?

A

DC power and bleed air.

27
Q

During engine start, when does the starter motor cutout?

A

At 50% N2.

28
Q

When can the starter be reingaged after an aborted start?

A

At any N2 speed below 45%.

29
Q

Decsribe the engine ignition system for the engine?

A

Each engine has an A and B exciter. A is AC ESS BUS driver, B is DC BATT BUS battery driven through a static inverter.

30
Q

How is engine ignition activated?

A

Normally by FADEC.

Use of the continuous ignition switch.

31
Q

When does the FADEC switch off ignition during engine start?

A

At starter motor cutout (50% N2).

32
Q

When does continuous ignition automatically come on in flight?

A

During a stall.
Disruption in engine airflow.
During engine flameout.

33
Q

What does the engine operability valve do?

A

Opens when commanded to prevent a compressor stall.

34
Q

How is the engine fuel shutoff valve operated?

A

L or R ENG FIRE PUSH switchlight.

35
Q

How many fuel pumps are contained within the engine fuel pump unit?

A

Three. One draws fuel into the unit, one proiveds motive flow back out and one provides pressurised fuel to the engine.

36
Q

Where is the fuel temperature displayed on the EICAS measured?

A

Downstream of the fuel pump unit, and after passing through the fuel/oil heat exchanger.

37
Q

What is fuel coming from the fuel metering unit is used for?

A

Engine operation.
Variable geometry.
Operability valve.

38
Q

Where is bleed air obtained?

A

From the 6th and 10th stage of the high pressure (N2) compressor.

39
Q

What should happen if a thrust reverser is inoperative?

A

A thrust reverser lock-out plate should be correctly installed.

40
Q

What does the thrust lever position supply information to?

A
FADECs.
Flight control computers.
Data concentrator unit.
Landing gear warning system.
Take-off configuration warning system.
Cabin pressurisation system.
Ground lift dumping system.
41
Q

What does pressing the TOGA buttons do?

A

Sends commands to the flight director and the flight management system.

42
Q

Starter re engagement is prohibited above?

A

45% N2.

43
Q

What happens if during start, the FADEC detects a failed igniter?

A

It will automatically switch to the other igniter after 15 seconds.

44
Q

During landing, when is maximum reverse thrust is prohibited?

A

Below 75 kt.

Reverse idle should be achieved by 60 kt.

45
Q

When does FADEC provide engine overspeed protection?

A

When N2 exceeds 107%.

46
Q

When does FADEC change in control and standby channels?

A

Every second start when N2 reaches 7%.

47
Q

When is APR power armed during take-off?

A

When N1 RPM are within 8% of the take-off N1 reference value.

48
Q

When is a FLEX take-off prohibited?

A
Wing or cowl anti-ice is required.
Runway is contaminated.
Windshear warnings.
Anti-skid is inoperative.
Engine cannot produce full rated thrust.