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KC-130J > Ch-4 > Flashcards

Ch-4 Flashcards

1
Q

Taxi and takeoff gross weight limitations:

A

Maximum normal: 164,000
Maximum alternate: 175,000

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2
Q

Landing gross weight limitations

A

Recommended: 142,000
Maximum normal: 164,000
Maximum alternate 175,000

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3
Q

Outboard tanks max

A

8310

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4
Q

Inboard tanks max

A

7650

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5
Q

Total main tanks

A

31,920

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6
Q

Aux tanks

A

5810

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7
Q

Total internal fuel weight max

A

43,540

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8
Q

External tanks

A

8,900

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9
Q

Fuselage tank

A

24,390

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10
Q

Total internal and external (fuel)

A

85,730

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11
Q

Primary fuel management

A

-Outboards contain 500-1000 more fuel than inboards
-main tanks full except start/taxi/takeoff fuel
-no less than 7060 in 1 & 4 and no less than 6410 in tanks 2 & 3 when external tanks have fuel

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12
Q

Alternate enroute fuel management

A

-May extend airframe service life
-when external and/or auxiliary tanks contain useable fuel 1&4 are maintained at max and 500-1000 more than 2&3
-w/ no fuel in aux & externals, 1&4 full, 2&3 used till 1520. 1&4 then used till 1520, tank-engine from there

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13
Q

Secondary fuel management

A

Anything not primary or alternate

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14
Q

Recommended loading limits

A

Area A: 3 g (symmetrical)
Area B & C: 2.5 g (symmetrical)

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15
Q

Alternate (cautionary) loading limits

A

Area D: 2.25 g (symmetrical)

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16
Q

Loading not recommended

A

Area E: 2 g (symmetrical)
Emergency situations

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17
Q

Landing gear doors removed

A

200 gear up
168 gear down

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18
Q

Flight is not permitted with forward nose gear door ______ and the aft door ______

A

Removed, installed

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19
Q

GS location - % Mac

A

15-30

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20
Q

External tank limits when fuselage tank is installed

A

If fuel is in the fuselage tank, external tanks should be empty when the fuselage tank contains less than 20,000 lbs. otherwise restricted to level flight

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21
Q

Taxing with inner brake locked, braking during revers taxiing

A

Prohibited

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22
Q

Taxi speeds & nose gear deflection
20 degrees
60 degrees

A

20 knots
5 knots

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23
Q

Taxiing w/ alternate gross weight

A

-Taxi & takeoff only on smooth surfaces free of dips depressions and holes
-max 10 knots
-taxi shortest distance possible
-minimum braking
-light braking in turns
-limit nose wheel to 5 degrees
-avoid abrupt or hard uneven brake applications

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24
Q

Max tire speeds
Nose-
Main-

A

139

174

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25
Q

Three categories of airfields (strength)

A

High strength
Marginal strength
Substandard

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26
Q

High strength airfields:
When Aircraft classification number (ACN) is greater than Pavement Classification Number (PCN)

A

Aircraft should normally NOT land on runway

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27
Q

Normal operation recommended tire deflection

A

35 %

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28
Q

Marginal strength airfields:
California bearing ratio (CBR) min

A

3,
Considerations should be given to operations having aircraft weights in excess of the weight limitation for 540 sink and on runways with CBR 6 or less

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29
Q

Predictions for number of passes on a marginal airfield are a function of _____ & _____ (figure 4.6-2)

A

Aircraft gross weight and CBR

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30
Q

Number of passes (for marginal field) based on recommendation of tire pressure corresponding to ____ tire deflection

A

39 %
(To prevent excessive tire damage, do not exceed 39 %)

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31
Q

Applicable airfield strength recommendations for marginal and substandard fields (8 thing)

A

-inflate/deflate main gear tires to recommended psi
-empty externals
-do not exceed 10 knots during taxi
-minimize breaking if porpoising
-minimize nose gear loads using elevator on landing rollout and T/O, load with mid or aft CH
-minimize reverse on unpaved
-shut off flight station AC on unpaved (prevents clogging of heat exchanger)
-limit gross weight to 164,000

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32
Q

Gross weight limits for substandard field

A

-Correspond to 540 sink rate
-Decision to use substandard should be made by appropriate authority
-Allow for increased maintenance and accelerated inspections

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33
Q

Maximum passenger load for extended over water operating more than 50 nautical miles from shore

A

-80 passengers including crew
-with mixed cargo and passengers, 35 per overhead exit

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34
Q

With any flap extension, load factor is

A

2 g symmetrical
1.5 unsymmetrical

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35
Q

Load factor limits:
Area A-

A

-1 - 3 symmetrical
0 - 2.33 rolling

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36
Q

Load factor limits:
Area B

A

0 - 2.5 symmetrical
0 - 2 rolling

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37
Q

Load factor limits:
Area C

A

0 - 2.5 symmetrical
0 - 2 rolling

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38
Q

Load factor limits:
Area D

A

0 - 2.25 symmetrical
0 - 1.83 rolling

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39
Q

Load factor limits:
Area E

A

Not recommended

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40
Q

High bank-angle limitations

A

-Apply to maneuvers beyond 60 degrees (flaps up) 45 degrees ( flaps extended)
-large aileron inputs should be made between 0.5 and 1.5 g

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41
Q

Prohibited maneuvers

A

-Aerobatics and spins
-practice stalls with power above 1000 HP
-practice asymmetric power stalls
-intentional zero or negative G maneuvers lasting longer than 7 seconds
-sustained airspeed below stick pusher speed
-intentionally maneuvering into a slide slip for a RUDDER alert
-abrupt longitudinal control inputs at high speeds (faster than 1 g per second increase or decrease)
-rapid toll reversals
Moderate to large rudder inputs held until slideslip followed by opposite rudder

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42
Q

Because of propulsion system limitations, avoid intentional negative and zero g maneuvers lasting longer than ______

A

7 seconds

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43
Q

Air start can be conducted with or without use of starter below ______

A

25,000 ft

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44
Q

Max air start elevation for Jp-4

A

22,500 ft

45
Q

With bleed air available, starter assisted air start can be accomplished at any speeds loss than ______

A

250 KIAS
(NG below 29)

46
Q

With bleed air not available,
NG 15-29
If prop is windmilling at 100% NP, NG will stabilize at _________

A

15, at speeds as low as 110-130

47
Q

If propeller is feathered, speed as high as ______ may be required to achieve 15 % NG

A

200-250

48
Q

Static propeller feathering is limited to _____ cycles before propeller gearbox must be ______ or _____

A

2
Drained
Engine started

49
Q

Total auxiliary feather pump operation shall not exceed _____ seconds

A

80

50
Q

Mgt start limits

A

807 for 2 seconds (max 175 to start)

51
Q

Mgt ground

A

600

52
Q

Mgt reverse

A

833

53
Q

Mgt takeoff

A

852

54
Q

Mgt max continuous

A

833

55
Q

Min oil temp for start

A

-40

56
Q

Engine power limited to idle when oil temp is less than _____
And to 1000 when oil temp is less than _____

A

0, 45

57
Q

GPSI

A

15 seconds of rotation
110-210 LSGI
170-210 GI and above

58
Q

EPSI

A

15 seconds of gas generator rotation
40-90

59
Q

Oil temp

A

60-85

60
Q

Shutdown engine if oil temp exceeds

A

93
86-93 for > 5 minutes

61
Q

Starter duty cycle

A

70 sec on, 60 sec off for 5 cycles
Then 20 min cooling

62
Q

Takeoff crosswind restrictions

Not pointed into wind +/- 45 degrees, with a component 15-35

A

2,500 HP max until greater than 35 KIAS

63
Q

With WINDMILLING propeller (greater than one half revolutions per minute) and oil supplied (fire handle in), engine should be started within _____ and operated at Flt idle for at least ____

A

5 minutes
5 minutes

64
Q

With FEATHERED propeller (less than than one half revolutions per minute) and oil supplied (fire handle in), engine should be started within _____ and operated at Flt idle for at least ____

A

6 hours
20 minutes

65
Q

APU starter cycle

A

90 sec on 5 min off for three cycles,
Min 60 minutes before subsequent start attempts

66
Q

Max APU RPM

A

110
Shuts down if exceeded

67
Q

APU bleed air pressure

A

40-50 psi

68
Q

APU EGT

A

Max continuous-680
710 for 3 seconds

69
Q

APU generator voltage

A

108-117

70
Q

Boost pump psi

A

15-24

71
Q

Transfer pump psi

A

28-40

72
Q

Fuselage transfer pump psi

A

28-46

73
Q

Fuel unbalance

A

1000 lbs between symmetrical tanks
1500 lbs between wings
One aux can be full with the other empty as long as all other tanks are symmetrically fueled or unbalanced towards the opposite side

74
Q

Do not operate with autopilot when:

A

-Takeoff and landing
-above Vh
-ILS coupled below 200 feet HAT (cat 1) 100 feet HAT (cat 2)
- below MDA on non precision
-IPRA below 200 HAT
-below 500 AGL for non approach operations
-in RVSM unless able to hold +/- 65 feet
-above 164,000 if below 1000 agl, during configuration or approach

75
Q

Automatic flight
Turn knob max bank angle

A

Approximately 35 degrees

76
Q

Automatic flight
Pilot/copilot engage bank angle

A

25 +/-3

77
Q

Automatic flight
Course intercept bank angle

A

25 +/- 3

78
Q

Automatic flight
On course bank angle

A

10

79
Q

Automatic flight
Localizer tracking

A

15 +/- 3

80
Q

Vertical functions
IAS hold

A

+/- 3

81
Q

Vertical functions
VS hold

A

+/- 70 fpm at 1000 fpm

82
Q

Vertical functions
ALT hold

A

+/- 40 feet of initial altitude

83
Q

Vertical functions
ALT SEL

A

+/- 40 feet with +/- 75 foot overshoot at 1000 fpm

84
Q

Outflow valve differential control

A

14.3 +/- .2 in. Hg

85
Q

Safety valve

A

15.0 +/- 0.3 in Hg (do not exceed 16)

86
Q

Cabin differential pressure

A

Max 15.2 in. Hg

87
Q

Flaps 10 percent

A

220

88
Q

Flaps 20 percent

A

210

89
Q

Flaps 30 percent

A

200

90
Q

Flaps 40 percent

A

190

91
Q

Flaps 50 percent

A

183

92
Q

Flaps 60 percent

A

165

93
Q

Flaps 70 percent

A

155

94
Q

Flaps 80 percent

A

150

95
Q

Flaps 90 percent

A

145

96
Q

Flaps 100 percent

A

145

97
Q

Landing gear extended

A

168

98
Q

Landing lights extended

A

250

99
Q

Cargo door open and locked, ramp up and locked

A

250

100
Q

Paratroop air deflectors (opening)

A

150

101
Q

Paratroop doors open and locked

A

250

102
Q

High speed drogue

A

185-250

103
Q

Low speed drogue (extending and retracting)

A

105-120

104
Q

Low speed drogue (receiver engaged)

A

130

105
Q

Severe turbulent air operations

A

180

106
Q

Inoperative windshield ain’t-ice below 10k

A

187

107
Q

Oxygen regulator pressure

A

270-340 (breathing)
270-455 (no flow)

108
Q

Battery voltage

A

24 Vdc
Min to charge 22

109
Q

Loads (% of normal rated)

A

Ac generator 0-125
Ess and main DC busses 0-125

KC-130J (7 decks)

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