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C-130H > Limitations > Flashcards

Limitations Flashcards

1
Q

Normal oil quantity

A

4-12 gallons

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2
Q

Minimum oil quantity

A

4 gallons

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3
Q

Maximum oil quantity

A

12 gallons

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4
Q

Max allowable TIT

A

1083

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5
Q

Normal oil temperature

A

60-85

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6
Q

Maximum oil temperature on ground

A

85-100 for 30 minutes

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7
Q

Maximum oil temperature in flight

A

85-100 for 5 minutes

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8
Q

Minimum allowable oil temperature

A

40 and increasing

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9
Q

Normal GB oil pressure

A

150-250

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10
Q

Normal engine oil pressure

A

50-60

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11
Q

Maximum allowable engine oil pressure during start and warm up

A

100

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12
Q

Normal fuel pump pressure main tanks

A

15-24

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13
Q

Normal fuel pump pressure aux and external tanks

A

28-40

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14
Q

Normal cabin pressure range

A

-1.2 - 15.8 in hg

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15
Q

Normal auxiliary hydraulic system pressure

A

2900-3300

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16
Q

Maximum auxiliary hydraulic system pressure

A

3500

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17
Q

Normal generator frequency range

A

380-420 hz

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18
Q

Normal AC voltage

A

110-125 V

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19
Q

Normal DC voltage

A

25-30 V

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20
Q

Normal AC amperes

A

65-90 amps

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21
Q

Max allowable AC load

A

1.05

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22
Q

Max allowable DC load

A

1.03

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23
Q

Minimum PSI for one brake application with anti-skid OFF

A

2250

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24
Q

Minimum PSI for one brake application using emergency brakes

A

2900

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25
Q

Normal rudder boost pressure with flaps >15%

A

2900-3200

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26
Q

Normal rudder boost pressure with flaps 0-15%

A

1100-1400

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27
Q

Caution PSI range for rudder boost with flap 0-15%

A

1400-1600

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28
Q

Hydraulic pressure as low as ______ PSI may be experienced in LSGI, and is acceptable as long as normal limits are achieved when engines are on speed

A

2550

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29
Q

APU EGT range

A

260-650

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30
Q

Normal APU RPM range

A

95-105%

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31
Q

-1 LOX min and max

A

2.5-25 liters

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32
Q

Nose wheel turn range is ___ degrees when gross weight exceeds _______ pounds or taxi speed is ___ knots or higher

A

20 degrees

155,000 lbs.

20 knots

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33
Q

Max VVI for normal landing weight (130,000 lbs.)

A

540 FPM

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34
Q

Max VVI for weights > 130,000 lbs.

A

300 FPM

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35
Q

Flaps 10% airspeed

A

220

36
Q

Flaps 20% airspeed

A

210

37
Q

Flaps 30% airspeed

A

200

38
Q

Flaps 40% airspeed

A

190

39
Q

Flaps 50% airspeed

A

180

40
Q

Flaps 60% airspeed

A

165

41
Q

Flaps 70% airspeed

A

155

42
Q

Flaps 80% airspeed

A

150

43
Q

Flaps 90% airspeed

A

145

44
Q

Flaps 100% airspeed

A

145

45
Q

Maximum airspeed with cargo door and ramp open

A

150

46
Q

Maximum airspeed with cargo door open

A

185

47
Q

Air deflector door maximum airspeed

A

150

48
Q

Maximum speed with paratroop door open and pinned

A

250

49
Q

Maximum nosewheel speed

A

139

50
Q

Maximum main gear speed

A

174

51
Q

Thunderstorm penetration speed

A

65 knots above power off stall speed, not to exceed 180 KIAS

52
Q

Utility hydraulic system accumulator preload

A

1500 +/- 100 PSI

53
Q

Booster hydraulic system accumulator preload

A

1500 +/- 100 PSI

54
Q

Emergency brake accumulator preload

A

1000 +/- 100 PSI

55
Q

Engine starter duty limits

A

1 ON / 1 OFF

1 ON / 5 OFF

1 ON / 30 OFF

56
Q

The start valve open light should extinguish within ___ seconds after switch is released

A

15

57
Q

Propeller aux pump duty limits

A

1 minute ON, 1 minute OFF; not to exceed 2 minutes in 30 minutes

58
Q

The maximum time for the propellers to go from reverse to feather is:

A

25 seconds

59
Q

If the feather override button does not pop out within __ seconds after the propeller is feather, pull it out manually

A

6 seconds

60
Q

Inflight use of the APU is limited to ___. Do not attempt to use the APU inflight for _____ ___

A

AC generator use

Do not use the APU for bleed air in flight

61
Q

The APU must be on speed and warmed up for a minimum of ________ before applying a bleed air load

A

1 minute

62
Q

APU starter duty cycle

A

1 minute ON, 4 minutes OFF

63
Q

If APU RPM exceeds ___%, the APU automatically shuts down

A

110%

64
Q

Total useable fuel weight (tanks with foam)

A

61,364 lbs.

65
Q

Maximum speed with landing gear doors removed

A

200 KIAS

66
Q

Clean maneuver load limits

A

-1 / +3 Gs

67
Q

Maximum maneuver load limits dirty

A

+2Gs symmetrical

+1.5Gs unsymmetrical

68
Q

Primary fuel management

A

500-1000# between OBs and IBs

1000# between symmetricals

1500# wing to wing

69
Q

Maximum speed with maximum nose gear deflection of 60 degrees

A

5 knots

70
Q

LSGI RPM

A

69-75.5%

71
Q

Ground idle RPM

A

94-102%

72
Q

Maximum reverse RPM

A

96-106%

73
Q

Flight idle RPM on the ground

A

92.5-100.5%

74
Q

Normal engine RPM in flight

A

98-102%

75
Q

Maximum takeoff TIT range (5 minutes)

A

1067-1083

76
Q

Military power TIT and time limit

A

1049 for 30 minutes

77
Q

Max continuous TIT

A

1010

78
Q

Allowable oil pressure flux

A

+/- 20 PSI for GB

+/- 10 PSI for engine

79
Q

Minimum GB oil pressure for mission accomplishment

A

130 PSI

80
Q

Start TIT < 720

A

781/MX

81
Q

Start TIT 720-750

A

781 / temp cont check

82
Q

Start TIT 750-830

A

Normal

83
Q

Start TIT 830-850

A

Stop start / 781 / 1 restart

84
Q

Start TIT exceeds 965

A

Stop start / 781 / inspection

85
Q

Start TIT during power peak > 1083 for more than 5 seconds or > 1175 momentarily

A

781 / MX before the next flight

86
Q

Allowable prop RPM flux

A

+ / - 0.5% of stable RPM

C-130H (6 decks)

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