Powerplant Flashcards

(50 cards)

1
Q

CRJ powerplant model

A

General Electric CF-34-8C5

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2
Q

Normal takeoff thrust for CF-34-8C5

A

13,360 lbs thrust

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3
Q

Automatic Performance Reserve (APR) thrust rating for the CF-34-8C5

A

14,510 lbs thrust

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4
Q

Max Continuous Thrust (MCT) for the CF-34-8C5

A

13,680 lbs thrust

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5
Q

Max temperature for takeoff and landing

A

ISA +40 degrees C

OAT of +51 degrees C

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6
Q

Min ambient air temperature for takeoff

A

-40 degrees C

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7
Q

Max altitude for windmill engine start

A

21,000 MSL

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8
Q

Max engine to engine N2 split at ground idle power

A

2%

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9
Q

How much thrust is produced by the core air

A

Approximately 20%

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10
Q

How much thrust is produced by the bypass air

A

Approximately 80%

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11
Q

How many compressor stages are there in the CF-34-8C5

A

10 stages

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12
Q

What accesories are driven off of the N2 accessory gear box

A

Engine driven fuel pump

IDG

Air Turbine Starter (ATS)

Oil pump

FADEC alternator

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13
Q

What stages supply bleed air to the common bleed air manifold

A

Normally the 6th stage, the 10th stage is also available when the demand exceeds the capabilities of the air in the 6th stage

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14
Q

What allows 10th stage bleed air availability

A

Air Conditioning System Controller (ACSC), automatically opens the High Pressure Valve (HPV)

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15
Q

What is the engine bleed air used for

A

Engine starts

Pressurization and air conditioning

Wing and cowl anti ice

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16
Q

What is the min bleed air pressure required for a cross bleed start

A

42 PSI at a max of 80% N2 for operating engine

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17
Q

What is the normal air source for the starting engine

A

APU bleed air

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18
Q

What source is used to start an engine when the APU is INOP or shut down

A

Ground air cart

Cross bleed starts from and operating engine may also be used

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19
Q

Where is the high pressure, ground air supply connection located

A

On the fuselage aft of the cargo bay door

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20
Q

What are the engine starter cranking limits

A

Attempt 1-2, 90 seconds ON / 10 seconds OFF

Attempt 3-5, 90 seconds ON / 5 minutes OFF

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21
Q

What are the dry motoring limits

A

Attempt 1, 90 seconds ON / 5 minutes OFF

Attempt 2-5, 30 seconds ON / 5 minutes OFF

22
Q

What causes the FADEC to automatically abort a start

A

Hot start

Hung start

23
Q

How many ignitors are installed in each engine

24
Q

What supplies power to the ignitors

A

IGN-A: AC ESS BUS

IGN-B: Static invertor on the battery bus

25
When must continuous ignition be used
Takeoffs and landings on contaminated runways Flight through moderate or heavy rain Flight through moderate or heavy turbulence Flight in the vicinity of thunderstorms
26
When is continuous ignition automatically activated
When approaching a high angle of attack
27
What conditions are required before advancing thrust levers to IDLE during an engine start
N2 greater than 20% ITT below 120 degrees C
28
What conditions would cause a takeoff configuration warning
Parking break set Autopilot ON Spoilers extended Flaps not 8 or 20 degrees Aileron trim out of green range Rudder trim out of green range
29
What is APR
Automatic Performance Reserve
30
When is APR armed for takeoff
When the N1 RPM of both engines is within 8% of scheduled takeoff power
31
When is APR armed for landing
Flaps 20 degrees or greater Landing gear is down
32
When will the APR system be activated
Thrust levers in TOGA N1 differs by 15% or greater on one engine after APR is armed Thrust levers set to MAX POWER HIGH PWR SCHEDULE switchlight is selected ON
33
What occurs when APR system activates
FADEC commands a thrust increase dependant on the thrust lever position
34
What indication is displayed when APR is activated
Green APR icon on N1 gauge
35
If an engine fails during a go-around, will the APR system activate
Yes
36
What is used to deploy the thrust reversers
L reverser uses hydraulic system 1 R reverser uses hydraulic system 2
37
What indications will be displayed during thrust reverser deployment
Amber REV icon on the N1 gauges during cowl transition Green REV icon on the N1 gauges when they are fully deployed
38
What is occuring during thrust reverser deployment
The translating cowls move aft, blocking the rearward flow of bypass air The fan discharge airflow is redirected forward through the cascade vanes
39
When do the thrust reversers need to either be stowed or at idle
60 knots
40
What are indications of an inadvertent thrust reverser deployment
Amber REV icon on the N1 gauge REV UNLOCKED caution message FADEC commands idle thrust of affected engine Note: Thrust levers will not move when when FADEC commands idle thrust
41
Minimum oil temperature for start
-40 degrees C
42
Maximum continuous oil temperature
155 degrees C
43
Maximum permissible oil temperature
163 degrees C | 15 minutes max
44
Maximum oil consumption
0.05 gallons per hour
45
Where can the oil quality be checked
EICAS menu page
46
When should oil capacity be checked
3 minutes - 2 hours after shutdown
47
When should the oil level be replenished
15 minutes- 2 hours after shutdown
48
How is oil cooled
Fuel/oil heat exchanger
49
Maximum oil refill before dry motoring is required
2 quarts
50
What is the total oil quantity of the engine oil tanks
7.2 quarts