Powerplant Flashcards

1
Q

What is the CRJ-900 Powerplant Model Number

A

General Electric CF34-8C5

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

What is the thrust rating without APR/with APR

A

Without APR 13,360 lbs

With APR 14,510 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What is the Max ambient air temperature for takeoff and landing

A

ISA + 40°C, limited to a maximum OAT 51°C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

What is the Min ambient air temperature for takeoff and landing

A

-40°C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

What is the Max Altitude for a windmill start

A

21,000 ft MSL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Max engine to engine N2 split at ground idle power

A

2%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

How much of the thrust is produced by core air

A

Approximately 20%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

How much thrust is produced by by-pass air

A

Approximately 80%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

How many stages of compression do we have

A

10 stages, The engine is equipped with a 10 stage axial flow compressor.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What accessories are driven off the N2 accessory gear box?

A
Engine driven Fuel pump,
IDG,
air turbine Starter,
engine driven Hydraulic pump,
Oil pump,
FADEC alternator
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What is the engine bleed air used for

A

Engine start
air conditioning / pressurization
wing and cowl anti-ice

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

What stages of bleed air are used

A

Normally 6th stage, 10th stage used when demand exceeds capability of 6th stage.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

What allows 10th stage bleed air availability

A

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

How many igniters are installed on each engine

A

Two, IGN-A and IGN- B

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

What are the required parameters before fuel is introduced during a ground engine start

A

N2 20% or greater

ITT <120°C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What occurs when the APR system activates

A

FADEC commands an N1 speed increase dependent on thrust lever position

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

What indication will we have of APR activation

A

Green APR icon on operable engine N1 gauge

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

If an engine fails during a go-around, will the APR system activate

A

Yes

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

What is used to deploy and stow the thrust reversers

A

Hydraulics
L reverser uses hydraulic system #1
R reverser uses hydraulic system #2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

How are the thrust reversers deployed

A

Thrust levers must be at idle. The reverse thrust levers are raised by engaging the thrust reverse release triggers. A solenoid lock stops reverse thrust lever movement while the reversers deploy. Once deployed, the lock releases and N1 may be increased by raising the reverse thrust levers.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

What is occurring during thrust reverser deployment

A

The translating cowls move aft, blocking the rearward flow of bypass air.
The fan discharge airflow is redirected forward though the cascase vanes.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

What indications will be during thrust reverser deployment

A

Amber REV icon on the N1 gauges during cowl transition.

Green REV icon on N1 gauges when the reversers are fully deployed.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

When do the thrust reversers need to be either stowed or at idle

A

60 kts

24
Q

What happens when a thrust reverser inadvertently deploys

A

FADEC commands thrust to be set to idle on affected engine

25
Q

What are the indications of an inadvertent thrust reverser deployment?

A

Amber REV icon on N1 gauge,
REV UNLOCKED caution message
FADEC commands idle thrust on affected engine.
NOTE: Thrust levers will NOT move when FADEC command idle thust

26
Q

What is the normal air source for engine starts

A

APU or cross-bleed if doing a single engine taxi

27
Q

What source is used if the APU is INOP

A

Ground air cart or bottle attached to the high pressure air ground connection to start one engine.
A cross bleed start is then used to start the other engine after clearing it with ground control.

28
Q

When will the starter cut-out during an engine start

A

50% N2 RPM

29
Q

Max continuous thrust (MCT) for the CF34-8C5

A

13,680

30
Q

What is the engine bleed air used for?

A

Engine start
Air conditioning / pressurization
Wing and cowl anti-ice

31
Q

What is the normal source used for engine starting?

A

APU bleed air

32
Q

What is the minimum bleed air pressure required for a cross bleed start?

A

42 PSI at a mixmum of 80% N2 for the operating engine

33
Q

Where is the high pressure, ground air supply connection located?

A

On the fuselage, aft of the cargo bay door.

34
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

35
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

36
Q

What would cause the FADEC to automatically abort the start?

A

Hot start or Hung start

37
Q

What supplies power to the ignitors

A

IGN-A AC ESS Bus

IGN-B Static inverter on the battery bus

38
Q

When must continuous ignition be used?

A

Takeoffs and landings on contaminated runways.
Flight though moderate or heavier intensity rain.
Flight though moderate or heavier intensity turbulence.
Flight in the vicinity of thunderstorms.

39
Q

When is continuous ignition automatically activated?

A

When approaching a high angle of attack

40
Q

What conditions would cause takeoff configuration warning?

A
MEMORY AID PASSFAR

Parking brake SET
Autopilot ON
Spoilers Extended (flight or ground spoilers)
Stab trim out of green range
Flaps not set 8° or 20°
Aileron trim out of green range
Rudder trim out of green range
41
Q

What is APR?

A

Automatic Performance Reserve thrust

42
Q

When is APR armed for takeoff?

A

When N1 RPM of both engines is within 8% of scheduled takeoff power.

43
Q

When is APR armed for landing?

A

When flaps are greater than 20°, and the landing gear is down.

44
Q

When will the APR system be activated?

A

Thrust levers in TOGA, and N1s differ by 15% or greater after APT has been armed.
When the trust levers are set in the MAX POWER detent.
When the HIGH PWR SCHEDULE switch light is selected ON

45
Q

What occurs when the APR system activated?

A

FADEC commands a thrust increase dependent on thrust lever position.

46
Q

What indication is displayed when APR is activated?

A

Green APR icon on the n1 gauge

47
Q

If an engine fails during a go-around, will the APT system activate?

A

Yes

48
Q

Minimum Oil temerature for start

A

-40°C

49
Q

Max contininous oil temerature

A

155°C

50
Q

Max permissible oil temperature

A

163°C (15 minutes max)

51
Q

Max oil consumption

A

0.05 gallons/hr

52
Q

Where can the oil quantity be checked?

A

On the EICAS MENU? page

53
Q

When should the Oil capacity be checked?

A

3 minutes to 2 hours after shutdown

54
Q

When should the engine oil level be replenished?

A

15 minutes to 2 hours after shutdown

55
Q

Max oil refill before dry motoring is required

A

2 quarts

56
Q

How is the oil cooled?

A

Fuel/oil heat exchanger

57
Q

WHat is the total quantity of the engine oil tanks?

A

7.2 quarts