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MC-130J #'s > Numbers > Flashcards

Numbers Flashcards

1
Q

Nose Gear Deflected Maximum Speed:

20 Degrees

A

20 KGS

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2
Q

Nose Gear Deflected Maximum Speed:

60 Degrees

A

5 KGS

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3
Q

Above 164,000 pounds:

Maximum Taxi Speed

A

10 KGS

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4
Q

Above 164,000 pounds:

Max. Nose Gear Deflection

A

20 deg

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5
Q

Maximum Tire Speeds:

Nose

A

139 KGS

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6
Q

Maximum Tire Speeds:

Main

A

174 KGS

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7
Q

Maneuver Load Factor Limitations:

Flaps Up in Area A (Symmetrical)

A

-1 to 3 Gs

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8
Q

Maneuver Load Factor Limitations:

Flaps Up in Area A (Unsymmetrical)

A

2.33 Gs

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9
Q

Maneuver Load Factor Limitations:

Flaps Up in Area C (Symmetrical)

A

2.5 Gs

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10
Q

Maneuver Load Factor Limitations:

Flaps Up in Area C (Unsymmetrical)

A

2 Gs

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11
Q 
Maneuver Load Factor Limitations:
Flaps Extended (Symmetrical)
A

2 Gs

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12
Q 
Maneuver Load Factor Limitations:
Flaps Extended (Unsymmetrical)
A

1.5 Gs

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13
Q

Engine and Propeller Limitations:

Maximum Airstart Altitude

A

25,000’

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14
Q

Engine and Propeller Limitations:

Static Propeller Feathering Cycles

A

2 cycles

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15
Q

Engine and Propeller Limitations:

Feathering Commands

A

4

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16
Q

Relative Wind Not Within 45°:

Static Ground Runs (1-4K HP)

A

15 knots

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17
Q

Relative Wind Not Within 45°:

Crosswind >15kt, T/O procedure

A

2500 HP (35 KIAS)

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18
Q

UNfeathered Propeller Windmilling:

Fire Handle In > 3% NP

A

5 min

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19
Q

UNfeathered Propeller Windmilling:

Fire Handle In ≤ 3% NP

A

1 hr

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20
Q

Feathered Propeller Windmilling:

Fire Handle Out > 3% NP

A

2 hrs

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21
Q

Feathered Propeller Windmilling:

Fire Handle Out ≤ 3% NP

A

6 hrs

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22
Q

ACAWS Inhibited:

KIAS

A

70 - 140

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23
Q

ACAWS Inhibited:

Alt

A

0 - 400 AGL

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24
Q

Personnel Static Lines:

Tailgate Drops

A

20 per pass

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25
Q

Personnel Static Lines:

Manually Retrieved

A

10 per paratroop door

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26
Q

Personnel Static Lines:

Retriever Winch

A

20 per cable

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27
Q

Accommodations:

Ground Troops

A

78

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28
Q

Accommodations:

With wheel well seats

A

92

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29
Q

Accommodations:

Paratroops

A

64

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30
Q

Accommodations:

Litters / Attendants

A

70 / 6

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31
Q

Accommodations:

CDS Bundles

A

16

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32
Q

Accommodations:

Pallets

A

6

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33
Q

Accommodations:

Heavy Equipment

A

42,000 lbs

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34
Q

Accommodations:

Life Rafts

A

4 x 20 pers

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35
Q

Taxi and Takeoff Weight:

Maximum Normal

A

164,000 lbs

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36
Q

Taxi and Takeoff Weight:

Maximum Alternate

A

175,000 lbs

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37
Q

Landing Weight @ Rate of Sink:

Recommended

A

142,000 lbs @ 540 FPM

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38
Q

Landing Weight @ Rate of Sink:

Maximum Normal

A

164,000 lbs @ 300 FPM

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39
Q

Landing Weight @ Rate of Sink:

Maximum Alternate

A

175,000 lbs @ 300 FPM

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40
Q

Max Fuel in Tanks for Taxi and Takeoff:

No. 1 & 4

A

8310 lbs

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41
Q

Max Fuel in Tanks for Taxi and Takeoff:

No. 2 & 3

A

7660 lbs

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42
Q

Max Fuel in Tanks for Taxi and Takeoff:

AUXs (ea)

A

5810 lbs

43
Q

Max Fuel in Tanks for Taxi and Takeoff:

EXTs (ea)

A

8900 lbs

44
Q

Max Fuel in Tanks for Taxi and Takeoff:

Total Main

A

31,940 lbs

45
Q

Max Fuel in Tanks for Taxi and Takeoff:

Total Internal

A

43,560 lbs

46
Q

Max Fuel in Tanks for Taxi and Takeoff:

Total Internal Plus External

A

61,360 lbs

47
Q

Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:

No. 1 and No. 4

A

7323 lbs

48
Q

Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:

Main Tanks Total

A

28,000 lbs

49
Q

Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:

Aux Tanks Total

A

no restrictions

50
Q

Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:

EXTs (ea)

A

<500 lbs

51
Q

Airspeed Limitations:

Severe Turbulence

A

181 KIAS

52
Q

Airspeed Limitations:

Inoperative Windshield Anti-Icing <10,000 Feet

A

187 KIAS

53
Q

Airspeed Limitations:

High Speed Drogue Min

A

185 KIAS

54
Q

Airspeed Limitations:

HS Drogue Extending / MAX

A

250 KIAS / 35,000’

55
Q

Airspeed Limitations:

Low Speed Drogue Min

A

105 KIAS

56
Q

Airspeed Limitations:

LS Drogue Extending

A

120 KIAS

57
Q

Airspeed Limitations:

LS Drogue Max

A

130 KIAS

58
Q

APU Limitations:

Percentage the START light extinguishes

A

50%

59
Q

APU Limitations:

Warm-up time before applying a bleed air load

A

1 min

60
Q

APU Limitations:

Warm-up time before applying a bleed air load (≤-26°C)

A

4 min

61
Q

APU Limitations:

Starter Duty cycle times

A

1 min on / 4 min off

62
Q

APU Limitations:

Maximum continuous EGT (overtemp)

A

680 deg C (710 deg C for 3 sec)

63
Q

APU Limitations:

Cool down time without a bleed air load

A

1 min

64
Q

Fuel Limitations – Maximum weight difference between:

Symmetrical main tanks

A

1000 lbs

65
Q

Fuel Limitations – Maximum weight difference between:

Left and right wings

A

1500 lbs

66
Q

Autopilot Engagement Limitations:

Minimum altitude during an ILS/IPRA

A

200’ (100’ CAT II)

67
Q

Autopilot Engagement Limitations:

Maximum gross weight

A

155,000 lbs

68
Q

Autopilot Engagement Limitations:

Maximum airspeed

A

Vh

69
Q

Autopilot Engagement Limitations:

Min. non-approach operations altitude

A

500’

70
Q

Engine Start Limitations:

Maximum MGT prior to start

A

175 deg C

71
Q

Engine Start Limitations:

Minimum bleed air pressure

A

22 psi

72
Q

Engine Start Limitations:

Before attempting ground restarts, wait ___ seconds after NG reaches 0.

A

30 sec

73
Q

Engine Start Limitations:
Starter duty cycle is __ sec on, __ sec off
for __ cycles, then a __ min cooling time.

A

70 sec on, 60 sec off

5 cycles, 20 min cooling

74
Q

Engine Start Limitations:

NG must be indicated within __ sec after actuation of the ENGINE START switch to START.

A

10 sec

75
Q

Engine Start Limitations:

An indication of increasing eng oil press must be noted within __ sec of gas generator (NG) rotation.

A

15 sec

76
Q

Engine Start Limitations:

An indication of increasing gearbox oil press must be noted w/in __ sec of propeller rotation.

A

15 sec

77
Q

Miscellaneous Limitations:

LSGI should be selected for __ min prior to eng shutdown to allow engine temp to stabilize.

A

2 min

78
Q

Miscellaneous Limitations:

Replace a battery if the voltage is less than:

A

22 VDC

79
Q

Miscellaneous Limitations:

The minimum battery voltage allowed for takeoff is:

A

24 VDC

80
Q

Miscellaneous Limitations:

Check HP w/in ___ of takeoff prediction NLT __ secs after power levers reach TAKEOFF.

A

w/in 200 HP w/in 5 sec

81
Q

Miscellaneous Limitations:

Before Starting Engines checklist, ensure radar altimeter reads between __ and __ feet

A

1 and -3 ft

82
Q

Miscellaneous Limitations:

The maximum altimeter error to the elevation of a known checkpoint is +/- __ feet

A

40 ft

83
Q

Miscellaneous Limitations:

When accomplishing the propeller controls cycle, the oil temperature must be:

A

45 deg C

84
Q

Flap Retraction:

Less than 100K pounds (start)

A

135 KIAS

85
Q

Flap Retraction:

100-140K (start & end)

A

135 KIAS / FUSS

86
Q

Flap Retraction:

Greater than 140K (start & end)

A

Vobs + 5 / FUSS, 10% in 5 kt increments

87
Q

Minimum Runway Length for Landing:

100% Flaps

A

5000’

88
Q

Minimum Runway Length for Landing:

0% or 50% Flaps

A

6000’

89
Q 
Minimum Runway Length for Landing:
Max Effort (marked zone)
A

Ground Roll + 500’

90
Q 
Minimum Runway Length for Landing:
Max Effort (unmarked zone)
A

Ground Roll + 1000’

91
Q

Minimum Runway Width:

A

60’

92
Q

Minimum Taxiway Width:

A

30’

93
Q

Minimum Runway for Takeoff:

Normal

A

Critical Field Length

94
Q

Minimum Runway for Takeoff:

AMAX

A

AMFLMETO

95
Q

Minimum Runway for Takeoff:

MAX

A

MFLMETO

96
Q

Minimum Runway Length for Landing:

Normal

A

Landing Distance

97
Q

Minimum Runway Length for Landing:

Training

A

3000’ (or Landing Distance, whichever is greater)

98
Q

A “Dash One” Preflight is good for ___ hours, provided the aircraft is _____.

A

72 hours provided the aircraft is sealed

99
Q

CAT II:

Min HAT

A

100’

100
Q

CAT II:

Min RVR

A

1200

101
Q

CAT II:

Max Crosswind

A

10 kts

102
Q 
CAT II:
Max Crosswind (Training with min wx)
A

15 kts (with 200, 1/2)

103
Q

Max # of people on Flight Deck:

A

9

MC-130J #'s (1 decks)

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