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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
Oil temperature 10 minutes limit
132 to 143°C
26
Max oil temperature
143°C
27
Minimum oil quantity after engine start
2 gal +1/4 gal/hr
28
Max oil consumption
1/4 gal/hr/engine/24 hr mission = 9.1 pints per hour
29
Minimum oil pressure (idle)
35 psi
30
Minimum oil pressure (rapid deceleration)
30 PSI (increases to about 35 PSI within 10 minutes)
31
Low caution oil pressure
35 to 40 PSI
32
Normal oil pressure
40 to 60 PSI
33
High caution oil pressure
60 to 65 PSI
34
Max oil pressure
65 PSI
35
Max oil pressure during rapid advancement to TRT or go around power provided decrease to normal during climb out
65 PSI
36
Low oil pressure light illuminates
32 (+/-2) PSI or at 50 PSID
37
Low oil pressure light goes out
36 PSI
38
Oil pressure caution light can remain illuminated during cold weather ops (0° and below) for how long?
2 minutes after oil temperature reaches +40°C
39
Hot start EGT
450°C
40
EGT to "stop start" to avoid a hot start
450°C
41
EGT limit during start requires visual inspection of turbine/exhaust section for damage/failure
450 to 575°C (15 seconds or less) | 575 to 585°C (five seconds or less)
42
EGT limit during start requires engine removal
450 to 575°C (15 seconds or more) | Above 575°C (5 seconds or more)
43
Normal maximum idle EGT (reference/guide)
340°C
44
EGT & time limit for MCT power and below
510°C/continuous
45
EGT & time limit for above MCT power (TRT, reduced thrust, and go around)
575°C/5 minutes (see page 5–11)
46
Reduced EPR takeoff EGT limit
Use acceleration EGT limit of 575°C
47
Cool engine for five minutes prior to shutdown
Any power setting above 85% N2
48
Normal fuel flow at light off
<1000pph
49
Fuel flow at light off indicating a possible hot start
Sustained 1400 pph or greater
50
Fuel flow stabilizes at idle
1100 PPH
51
Fuel filter icing light illuminates
4.5 PSID
52
Fuel filter bypasses
5.8 PSID
53
Requirement for fuel heat usage fuel flow
5 minutes at idle or 1500 PPH
54
Fuel heat usage prior to take off
Fuel temp 0°C or below/on for one minute
55
Fuel usage for fuel without icing inhibitors (0°C and below)
1 minute out of every 30 minutes
56
Ensure 1500 PPH fuel flow after fuel heat turn off
2 minutes
57
Nacelle droop strip alignment before acceptance for flight
Within 1/8 inch
58
Fire bottle (engine) normal system pressure
600 psi (+/-50) at 50°F
59
In-flight wait between bottle discharges
30 seconds
60
Red disc missing
Thermal relief
61
Yellow disc missing
Electrically fired bottle
62
In reverse thrust, do not exceed
Go around N1 RPM
63
In reverse thrust, call out
97% N1
64
Generator load rating
``` 120 kVA (348 amps) continuous 140 kVA (406 amps) 5 minutes 200 kVA (580 amps) 5 seconds ```
65
APU normal frequency range
400 (+/-7) Hz
66
Max oscillation within the 400 (+/-7) Hz band
2 Hz
67
Max APU load allowed starting the VCM
Below 100 amps
68
APU battery type/rating
24 V, 44 amp/hour nickel cadmium
69
Minimum voltage to start APU
22 V
70
APU starter duty cycles
1 minute on – 1 minute off 1 minute on – 1 minute off 1 minute on – 1 hour off (three per hour)
71
APU fuel supply
3 main tank
72
Time left in RUN during start for ECB self test
5 seconds
73
Time in START position then released to RUN
2 seconds
74
Peak EGT during APU start occurs between
40 to 60% RPM
75
Normal APU EGT
330°C
76
APU high caution EGT
605 to 675°C
77
APU Max EGT
675°C
78
If EGT rapidly exceeds during the APU start – shutdown
900°C
79
Bleed air provided by APU
300 to 400 ppm at 45 PSIA (minimum)
80
Cool down period (no load) before shutdown
2 minutes
81
APU fire bottle capacity and type
2.5 pounds of Halon 1301
82
Normal fire bottle pressure
600 psi at 70°C
83
APU fuel consumption (bleed air & gen load)
450 PPH
84
APU FIRE LIGHT
Fire inside shroud
85
APU OVERHEAT
Fire outside shroud
86
Swapping APU power to A/C generator
APU amps <261 amps
87
Swapping APU power to A/C generator if more than 261 amps
2nd engine generator on within 5 seconds
88
Fuel manifold max pressure
50 psi
89
Fuel pressure disconnect switch during A/R
75 (+/-3) PSIG
90
Defueling rate through SPR
50 GPM
91
Undumpable fuel
17,861 pounds
92
Mexican airspeed fuel dump chute transition
240 KIAS/.83M
93
Max airspeed fuel dump chute extended
275 KIAS/.83M
94
Fuel dump in critical decent attitude
Approximately 3600 ppm all tanks simultaneous at 275 KIAS
95
Minimum altitude for fuel dumping
5000 feet AGL
96
Don't dump if possibility of fire in…
Wheel well and/or inboard engines
97
Fuel dripstick reading level
Point of last visible graduation
98
Max gross weight for 1 & 4 reserves empty
280,000 pounds
99
Normal gross weight for 1 & 4 reserves empty
Below 220,000 pounds
100
1 & 4 mains max before transfer from reserves
12,000 pounds
101
Main tanks full before exceeding in center wing
20,000 pounds
102
Flameout can occur if any main tank < 2500 pounds
Exceed 8° nose up or 10° nose down
103
Don't exceed during A/R – percent center wing tank
90%
104
Engine model and series
TF 33 – PW – 102C

unnamed (11 decks)

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