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C-17 Engine run > Engine Run > Flashcards

Engine Run Flashcards

1
Q

Engine Operations SHALL NOT BE accomplished without radio communication between ground, cockpit, and controlling agency.
True or False?

A

True

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2
Q

During the engine operation the sliding window (pilot or co-pilot’s) may be closed, Personnel may keep the window closed prior to opening the crew entry door.
True or False?

A

False

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3
Q

When a RIGHT MANIFOLD FAIL light appears on the ENVIR panel or a MANIFOLD FAIL aural warning sounds anytime during APU operation, immediately
A. Press #3 ENG boost pump switch light on the FUEL panel to extinguish the flow line.
B. Press APU switch on ENVIR panel to extinguish the flow line.
C. Ensure all personnel remain clear of the flare launch direction. Immediately perform a visual inspection of the flares for signs of protrusion from the ejection end of the canister prior to attempting any further fault isolation.
D. Both B&C

A

D. Both B & C

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4
Q

What is the minimum fuel quantity level to preform an engine run?
A.No Minimum fuel level is specified for engine operation.
B. 1,200 pounds of fuel per tank
C. 10,000 pounds of fuel between all 4 tanks
D. No less than 5,000 pounds displayed on fuel quantity totalizer.

A

A. No minimum fuel level is specified for engine operation

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5
Q

The APU shall not be operated when…
A. When the #3 engine left fan thrust reverser duct is open and the ambient air temperature is below 90F(32C)
B. When the #3 engine right fan thrust reverser duct is open and the ambient air temperature is above 90F (32F)
C. When the #3 engine right fan thrust reverser duct is open and the ambient air temperature is above 110F (43C)
D. When the #3 engine left fan thrust reverser duct is open and the ambient air temperature is above 90F (32C)

A

D. When the #3 engine left fan thrust reverser duct is open and the ambient air temperature is above 90F (32C)

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6
Q

APU may be operated for 15 minutes with the #3 engine left fan thrust reverser duct is open and the ambient air temperature is below 90F (32C)
True or False?

A

True

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7
Q 
Flaps/Slats shall be in the full up position when performing APU operations. APU may be started with flaps/slats down however they shall be set to full up position within?
A. 30 seconds after APU stabilization
B. 1 Min after APU stabilization
C. 3 Min after APU stabilization
D. 5 Min after APU stabilization
A

A. 30 seconds after APU stabilization

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8
Q

Icing conditions exist when the temperature is?
A. 10C (50F) or less and visible moisture (rain, drizzle, snow, sleet, ice crystal, or fog) is present
B.1C (34F) or less and visible moisture (rain, drizzle, snow, sleet, ice crystal, or fog) is present.
C. 6C (42F) or less and visible moisture (rain, drizzle, snow, sleet, ice crystal, or fog) is present.
D. none of the above.

A

C. 6C (42F) or less and visible moisture (rain, drizzle, snow, sleet, ice crystal, or fog) is present.

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9
Q

Use of minimum power settings in reverse and minimizing time above reverse idle may reduce the risk of FOD ingestion and engine surge.
True or False?

A

True

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10
Q

To prevent a possible APU fire, personnel shall position the START CONTR switch in the RUN position for?
A. 1 second prior to starting the APU
B. 2 second prior to starting the APU
C. 3 seconds second prior to starting the APU
D. 5 seconds second prior to starting the APU

A

B. 2 second prior to starting the APU

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11
Q

APU starter motor duty cycle shall not exceed three starts or attempts in 1 hour with minimum 1 minute off between starts or attempts. Failure to comply may cause damage to aircraft.
True or False?

A

True

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12
Q 
It takes approximately \_\_\_\_\_ seconds for the APU inlet door to open?
A.3
B.9
C. 7
D. none of the above
A

B. 9

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13
Q 
HIGH light comes on steady and the APU automatically shuts down when the maximum RPM of \_\_\_\_ is exceeded
A. 104%
B. 97%
C. 101%
D. 95%
A

A. 104%

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14
Q

HOT light comes on steady and the APU automatically shuts down when the RPM is above _____ and the maximum EGT of ____ is exceeded

A

B. 95%/ 621C

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15
Q 
APU RPM increases and stabilizes  at \_\_\_\_-\_\_\_ 
A. 95-104%
B.97-101%
C. 95-101%
D. 97-104%
A

B. 97-104%

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16
Q 
Circuit breaker \_\_\_\_\_shall be opened after the APU stabilization and remain open during APU operation to prevent an APU impolsion. The circuit breaker can be identified by a yellow ring around it,
A. c14
B. B14
C. E14
D. D14
]
A

D. D14

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17
Q

All AC packs must be operational for an engine run?

True or False?

A

False

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18
Q 
Hydraulic system 2 may require  \_\_\_ seconds to reach full system pressure.
A. 45
B. 30
C. 10
D. 60
A

A.45

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19
Q 
Normal  hydraulic pressure PSI is \_\_\_\_-\_\_\_\_ 
A. 3900-4300
B. 3500-4500
C. 3800-4200
D. 3700-4000
A

C. 3800-4200

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20
Q 
Minimum oil quantity for an engine run is how many quarts?
A. 14
B. 18
C. 23
D. 20
A

A. 14

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21
Q 
Hydraulic systems \_\_\_\_ are required to operate nose steering and aircraft breaks?
A. 1 and 4
B. 2 and 3
C. 1 and 3
D. 2 and 4
A

B. 2 and 3

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22
Q

What is immediately required if an engine experiences a hung start?
A. Shut down engine, wait 1 minute try again.
B. Motor engine to ensure there is no fuel present, inspect exhaust and try again.
C. Shut down engine, switch to a different ignition system and try again.
D. Bump throttles up, to speed up engine start.

A

B. Motor engine to ensure there is no fuel present, inspect exhaust and try again.

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23
Q 
When engine start is required within 30 minutes after engine shutdown, engines shall be motored until EGT is below \_\_\_\_.
A. 190c
B. 180C
C. 170C
D. none of the above.
A

A. 190C

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24
Q

Engines may be operated during icing condition when cowl anit-ice is not available or system is malfunctioning?
True or False?

A

False

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25
Q

When ambient temperature is below 0C, selection of A and B ignition may be required to facilitate engine start?
True or False?

A

True

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26
Q

One fuel boost pump per tank may be inoperative during engine run?
True or False?

A

True

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27
Q 
N2 rotation shall occur within  \_\_\_\_ seconds after the starter light comes on.Engine start shall be terminated when N2 RPM is not indicated.
A. 20
B. 25
C. 30
D.45
A

A. 20

28
Q 
Oil pressure indication shall occur within \_\_\_\_seconds of N2 rotation.
A. 20
B. 25
C. 30
D. 45
A

A. 20 seconds

29
Q 
N1 rotation shall occur within \_\_\_\_ seconds after starter light comes on.
A. 60
B. 70
C. 80
D. 90
A

D. 90

30
Q

When starting engines, do not exceed started duty cycle of five minutes on, and 15 minutes off. Each start attempt there after shall require five minutes on, ten minutes off for cooling. Don not exceed five attempts within one hour.
True or False?

A

True

31
Q 
In event of an aborted start, engine shall be motored for a minimum of  \_\_\_\_ seconds to prevent engine fire.
A. 30
B. 45
C. 60
D.90
A

A. 30 seconds

32
Q 
After the start button is pushed, the SUPLLY PRESS PSI on the ENVIR panel increases to what minimum  PSI?
A. 20
B. 18
C. 14
D. 12
A

B. 18 PSI

33
Q

If the oil pressure decreases or quantity drops to zero , you may continue and determine the problem once done with engine operations?
True or False?

A

False

34
Q 
Fuel flow shall not exceed \_\_\_\_\_ PPH ( pounds per Hour)  prior to light off. When fuel flow is exceeded, engine start shall be terminated.
A. 800
B. 700
C. 600
D. 500
A

B. 700 PPH

35
Q 
Light off shall occur within \_\_\_\_ seconds after the ENG SHUT OFF switch is rotated to the ON position,
A. 20 
B.25
C. 30
D.35
A

A. 20 seconds

36
Q 
EGT shall not exceed \_\_\_\_ during engine start.
A. 821C
B. 621C
C. 595C
D. 495C
A

D. 495C

37
Q 
In the event of an aborted start after light off, the engine shall be motored until EGT is below \_\_\_\_C
A. 160
B. 170
C.160
D. 190
A

D. 190C

38
Q 
Rotate ENG SHUT OFF switch on fuel panel to ON at what percent?
A.16-22%
B.17-23%
C. 18-24%
D. 20-25%
A

C. 18-24%

39
Q 
The ENG START SWITCH button disengages at what percent N2 RPM?
A. 50-54%
B. 51-55%
C. 50-55%
D. none of the above
A

B. 51-55%

40
Q 
The ENG START SWITCH should disengage at \_\_\_\_% N2 RPM. ENG START SWITCH shall be pulled out at \_\_\_\_\_%
A. 50/54%
B. 51/55%
C. 50/55%
D. none of the above
A

B. 51/55%

41
Q 
After ENG START SWITCH button pops out, within how many seconds should the light go off?
A.20
B.30
C.40
D.45
A

B.30 seconds

42
Q

Idle N2 % RPM target is 120 seconds. This may be exceeded provided starter limits are not exceeded, N2 RPM is increasing, and no other out of limits conditions exist?
True or False

A

True

43
Q 
What is the target idle N2 % RPM?
A.55-65%
B. 50-60%
C.51-55%
D.60-65%
A

A. 55-65%

44
Q

When all 4 engines are being started for an above idle run, what steps must be done?
A. Ensure EXT PWR switch on the electrical panel is set in the on position and shut down generator set and move clear of aircraft after starting engines number 1 and number 2, but before starting engines number 3 and or number 4.
B. Ensure EXT PWR switch on electrical panel is set in the on position and start engines from left to right
C. Set EXT PWR switch on electrical panel to off and shut down generator set and move clear of aircraft after starting engines number 3 and number 4, but before starting engines number 1 and number 2.
D. Set EXT PWR switch on electrical panel to off and shut down generator set and move clear of the aircraft. After starting engines number 1 and number 2, but before starting engines number 3 and number 4.

A

D. Set EXT PWR switch on electrical panel to off and shut down generator set and move clear of the aircraft. After starting engines number 1 and number 2, but before starting engines number 3 and number 4.

45
Q 
Once the engine is at idle, the display oil quantity limits are \_\_\_-\_\_\_ quarts
A.8-12
B.10-12
C.4-12
D.6-12
A

C. 4-12

46
Q 
Once the engine is at idle, what is the minimum PRESS PSI for oil?
A. 50
B. 60
C. 70
D. 80
A

C. 70 PSI

47
Q 
Once the engine is at idle, what is the maximum TEMP for oil?
A. 163C
B. 153C
C. 143C
D. 177C
A

D. 177C

48
Q 
Oil TEMP shall be \_\_\_\_\_ continuously, caution is \_\_\_\_\_-\_\_\_\_ for 20 minutes and MAX TEMP is?
A. 163C, 164-177C, 177C
B. 153C, 163-173C, 173C
C. 143C, 153-163C, 163C
D. none of the above
A

A. 163C, 164-177C, 177C

49
Q 
MAX oil PRESS while engines are above idle is \_\_\_\_\_.
A. 250 PSI
B. 249 PSI
C. 248 PSI
D. 245 PSI
A

B. 249 PSI

50
Q 
Limit reverse IDLE operation to \_\_\_\_\_ min
A. 5
B. 10
C. 15
D. 20
A

A. 5 Minutes

51
Q 
Engines should be stabilized at IDLE for no less than \_\_\_\_\_ minutes prior to power.
A. 3
B. 4
C. 5 
D. 6
A

C. 5 minutes

52
Q 
Reverse engine operation in lieu of forward thrust is authorized above IDLE up to 1.18 EPR and may be accomplished for a maximum \_\_\_\_ minutes. Operation above 1.18 EPR is limited to \_\_\_\_\_seconds.
A. 3, 20
B. 5, 45
C. 2, 30
D. 3, 45
A

C. 2, 20

53
Q 
Allow APU to operate with no load for a minimum of \_\_\_\_\_ minute(s) prior to shut down.
A. 1
B. 2
C. 3
D. 5
A

B. 2 minutes

54
Q

Rotate SEL switch on STBY ENG displat to ____ for power runs.
A. N2
B. EPR

A

B. EPR

55
Q 
Do not operate all 4 engines simultaneously above \_\_\_\_\_% N2
A. 60
B. 65
C. 70
D. 75
A

D. 75%

56
Q 
Do not operate engines at MAX EPR for more than \_\_\_\_\_ minutes.
A. 3
B. 10
C. 15
D. 20
A

B. 10 minutes

57
Q 
Engine runs above idle that exceed 1.15 EPR require engine stabilization of \_\_\_\_ minutes at idle prior to shut down.
A. 5
B. 10
C. 15
D. 20
A

B. 10 minutes

58
Q 
When APU RPM is \_\_\_\_% or less, close APU door circuit breaker on overhead circuit breaker panel, row \_\_\_\_ column\_\_\_\_
A. 7, D14
B. 7, C14
C. 8, D14
D. 5, C14
A

A. 7, D14

59
Q 
MAX N1 speed is \_\_\_\_\_ and MAX N2 speed is 
A. 100.7, 100.5%
B. 100.5,100.7%
C. 100.3, 100.5%
D. 100.5, 100.3%
A

B. 100.5, 100.7%

60
Q 
MAX EGT for startup is \_\_\_\_, MAX of up to \_\_\_\_ continuously and and \_\_\_-\_\_\_ for no more than 5 minutes.
A. 395C, 495C, 525C-555C
B. 495C, 595C, 655C-695C
C. 495C, 625C, 626C-655C
D. 395C, 625C, 626C-655C
A

C. 495C, 625C, 626C-655C

61
Q 
For aircrafts in transient, EGT limits of 656C-670C are allowed for no more than \_\_\_\_ seconds.
A. 1
B. 2
C. 3
D. 5
A

D.5 seconds

62
Q 
a MAX of \_\_\_\_\_ seconds are allowed for EGT limits of 626C-655C while in reverse.
A. 20
B. 25
C. 30
D. 45
A

C. 30 seconds

63
Q 
For engines with more than 50 hours: \_\_\_ knots tail wind, \_\_\_\_ side to side of the intakes and \_\_\_ knots directly into the intake.
A. 0, 15, 36
B. 5, 15, 36
C. 5, 25, 36
D. 0, 25, 50
A

B. 5, 15, 36

64
Q

What are the emergency procedures for APU fire shut down?
A. Press of arm switch light on apu panel
lift guard press agent/disch switchlight
B. Push off/arm switchlight on apu panel
Raise guard and press agent/ disch switchlight.

A

A. Press of arm switch light on apu panel

lift guard press agent/disch switchlight

65
Q

What are the emergency procedures for engine shut down?
A. Move throttle levers to 1.15 EPR
Rotate eng shut off switch on fuel panel to off
B. Move throttle levers to idle
Rotate eng shut off switch on fuel panel to off

A

B. Move throttle levers to idle

Rotate eng shut off switch on fuel panel to off

66
Q

What are the emergency procedures for engine fire shut down?
A. Move all throttle levers to idle
Pull fire pull handle on instrument panel for effected engine.
B. Move all throttle levers to idle
Pull and rotate fire pull handle for effected engine.

A

B. Move all throttle levers to idle

Pull and rotate fire pull handle for effected engine.

67
Q

What are the emergency procedures for engine tail pipe fire during engine start?
A. Rotate eng shut off switch on fuel panel to off
motor engine till fire is extinguished
Monitor fuel flow on MFD. If fuel flow does not go to zero or fire is not extinguished after 30 seconds of motoring, pull but not rotate fire pull handle for effected engine.
B. Rotate engine shut off switch on fuel panel to off
Motor engine until fire is extinguished
Monitor fuel flow on MFD. If fuel flow does not go to zero or fire is not extinguished after 30 seconds of motoring, pull and rotate fire pull handle for effected engine.

A

A. Rotate eng shut off switch on fuel panel to off
motor engine till fire is extinguished
Monitor fuel flow on MFD. If fuel flow does not go to zero or fire is not extinguished after 30 seconds of motoring, pull but not rotate fire pull handle for effected engine.

C-17 Engine run (1 decks)

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