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unnamed > E8 L3 Gouge Deck > Flashcards

E8 L3 Gouge Deck Flashcards

1
Q

Pounds of thrust at sea level/temperature range

A

17,500 pounds at sea level

-50°C to +28.5°C

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2
Q

Driven by numbers 2, 3, 4 turbine wheels

A

N1 (low pressure)

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3
Q

Driven by number 1 turbine wheel

A

N2 (high-pressure)

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4
Q

Surge bleed valve operation, opens/closes

A

Spring-loaded open <55% N1

Closes above 55% N1

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5
Q

Normal N1

A

25 to 107% (110% max)

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6
Q

Normal N2

A

55 to 101% (106% max)

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7
Q

Normal N2 at idle

A

58 to 62% no load (within two min)

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8
Q

Duct pressure required for engine start

A

25 to 60 PSIG

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9
Q

Duct pressure to cool equipment (engine running)

A

22 PSIG

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10
Q

Burner cans with igniter plugs

A

4 & 5

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11
Q

Ignition system should not exceed…

A

10 minutes with 10 minutes cooling

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12
Q

Starter duty cycles

A

1 min on, 1 min off for 1st attempt

1 min on, 5 min off for subsequent attempts

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13
Q

Release start selector and announce start valve closed

A

35% N2

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14
Q

Call NO CUTOUT and close wing isol valve to remove bleed air source before 45% N2

A

40% N2

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15
Q

Motor engine for hot, wet, or hung starts

A

15 sec

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16
Q

Time wait after stop start before restart

A

30 seconds after N2 rotation stops

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17
Q

Terminate start if no EGT increase during start

A

20 seconds after start lever moved to start

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18
Q

Terminate start if no oil pressure observed

A

30 seconds after start initiation

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19
Q

Designated engine oil

A

Mil-L-7808, Mil-L-23699

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20
Q

Maximum oil system capacity

A

8.3 gallons

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21
Q

Oil tank capacity

A

6.1 gallons

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22
Q

Usable oil

A

3.41 gallons

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23
Q

Normal oil temperature

A

40 to 132°C

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24
Q

Recommended oil temperature

A

80 to 100°C

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25
Q

Oil temperature 10 minutes limit

A

132 to 143°C

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26
Q

Max oil temperature

A

143°C

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27
Q

Minimum oil quantity after engine start

A

2 gal +1/4 gal/hr

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28
Q

Max oil consumption

A

1/4 gal/hr/engine/24 hr mission = 9.1 pints per hour

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29
Q

Minimum oil pressure (idle)

A

35 psi

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30
Q

Minimum oil pressure (rapid deceleration)

A

30 PSI (increases to about 35 PSI within 10 minutes)

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31
Q

Low caution oil pressure

A

35 to 40 PSI

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32
Q

Normal oil pressure

A

40 to 60 PSI

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33
Q

High caution oil pressure

A

60 to 65 PSI

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34
Q

Max oil pressure

A

65 PSI

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35
Q

Max oil pressure during rapid advancement to TRT or go around power provided decrease to normal during climb out

A

65 PSI

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36
Q

Low oil pressure light illuminates

A

32 (+/-2) PSI or at 50 PSID

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37
Q

Low oil pressure light goes out

A

36 PSI

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38
Q

Oil pressure caution light can remain illuminated during cold weather ops (0° and below) for how long?

A

2 minutes after oil temperature reaches +40°C

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39
Q

Hot start EGT

A

450°C

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40
Q

EGT to “stop start” to avoid a hot start

A

450°C

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41
Q

EGT limit during start requires visual inspection of turbine/exhaust section for damage/failure

A

450 to 575°C (15 seconds or less)

575 to 585°C (five seconds or less)

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42
Q

EGT limit during start requires engine removal

A

450 to 575°C (15 seconds or more)

Above 575°C (5 seconds or more)

43
Q

Normal maximum idle EGT (reference/guide)

A

340°C

44
Q

EGT & time limit for MCT power and below

A

510°C/continuous

45
Q

EGT & time limit for above MCT power (TRT, reduced thrust, and go around)

A

575°C/5 minutes (see page 5–11)

46
Q

Reduced EPR takeoff EGT limit

A

Use acceleration EGT limit of 575°C

47
Q

Cool engine for five minutes prior to shutdown

A

Any power setting above 85% N2

48
Q

Normal fuel flow at light off

A

<1000pph

49
Q

Fuel flow at light off indicating a possible hot start

A

Sustained 1400 pph or greater

50
Q

Fuel flow stabilizes at idle

A

1100 PPH

51
Q

Fuel filter icing light illuminates

A

4.5 PSID

52
Q

Fuel filter bypasses

A

5.8 PSID

53
Q

Requirement for fuel heat usage fuel flow

A

5 minutes at idle or 1500 PPH

54
Q

Fuel heat usage prior to take off

A

Fuel temp 0°C or below/on for one minute

55
Q

Fuel usage for fuel without icing inhibitors (0°C and below)

A

1 minute out of every 30 minutes

56
Q

Ensure 1500 PPH fuel flow after fuel heat turn off

A

2 minutes

57
Q

Nacelle droop strip alignment before acceptance for flight

A

Within 1/8 inch

58
Q

Fire bottle (engine) normal system pressure

A

600 psi (+/-50) at 50°F

59
Q

In-flight wait between bottle discharges

A

30 seconds

60
Q

Red disc missing

A

Thermal relief

61
Q

Yellow disc missing

A

Electrically fired bottle

62
Q

In reverse thrust, do not exceed

A

Go around N1 RPM

63
Q

In reverse thrust, call out

A

97% N1

64
Q

Generator load rating

A 
120 kVA (348 amps) continuous
140 kVA (406 amps) 5 minutes
200 kVA (580 amps) 5 seconds
65
Q

APU normal frequency range

A

400 (+/-7) Hz

66
Q

Max oscillation within the 400 (+/-7) Hz band

A

2 Hz

67
Q

Max APU load allowed starting the VCM

A

Below 100 amps

68
Q

APU battery type/rating

A

24 V, 44 amp/hour nickel cadmium

69
Q

Minimum voltage to start APU

A

22 V

70
Q

APU starter duty cycles

A

1 minute on – 1 minute off
1 minute on – 1 minute off
1 minute on – 1 hour off (three per hour)

71
Q

APU fuel supply

A

3 main tank

72
Q

Time left in RUN during start for ECB self test

A

5 seconds

73
Q

Time in START position then released to RUN

A

2 seconds

74
Q

Peak EGT during APU start occurs between

A

40 to 60% RPM

75
Q

Normal APU EGT

A

330°C

76
Q

APU high caution EGT

A

605 to 675°C

77
Q

APU Max EGT

A

675°C

78
Q

If EGT rapidly exceeds during the APU start – shutdown

A

900°C

79
Q

Bleed air provided by APU

A

300 to 400 ppm at 45 PSIA (minimum)

80
Q

Cool down period (no load) before shutdown

A

2 minutes

81
Q

APU fire bottle capacity and type

A

2.5 pounds of Halon 1301

82
Q

Normal fire bottle pressure

A

600 psi at 70°C

83
Q

APU fuel consumption (bleed air & gen load)

A

450 PPH

84
Q

APU FIRE LIGHT

A

Fire inside shroud

85
Q

APU OVERHEAT

A

Fire outside shroud

86
Q

Swapping APU power to A/C generator

A

APU amps <261 amps

87
Q

Swapping APU power to A/C generator if more than 261 amps

A

2nd engine generator on within 5 seconds

88
Q

Fuel manifold max pressure

A

50 psi

89
Q

Fuel pressure disconnect switch during A/R

A

75 (+/-3) PSIG

90
Q

Defueling rate through SPR

A

50 GPM

91
Q

Undumpable fuel

A

17,861 pounds

92
Q

Mexican airspeed fuel dump chute transition

A

240 KIAS/.83M

93
Q

Max airspeed fuel dump chute extended

A

275 KIAS/.83M

94
Q

Fuel dump in critical decent attitude

A

Approximately 3600 ppm all tanks simultaneous at 275 KIAS

95
Q

Minimum altitude for fuel dumping

A

5000 feet AGL

96
Q

Don’t dump if possibility of fire in…

A

Wheel well and/or inboard engines

97
Q

Fuel dripstick reading level

A

Point of last visible graduation

98
Q

Max gross weight for 1 & 4 reserves empty

A

280,000 pounds

99
Q

Normal gross weight for 1 & 4 reserves empty

A

Below 220,000 pounds

100
Q

1 & 4 mains max before transfer from reserves

A

12,000 pounds

101
Q

Main tanks full before exceeding in center wing

A

20,000 pounds

102
Q

Flameout can occur if any main tank < 2500 pounds

A

Exceed 8° nose up or 10° nose down

103
Q

Don’t exceed during A/R – percent center wing tank

A

90%

104
Q

Engine model and series

A

TF 33 – PW – 102C

unnamed (11 decks)

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