Lockheed Martin · United States · ICAO: C130 · 1996–Present ·
$75.5 million (2017)

Timeless Airlifter The Lockheed Martin C-130J Super Hercules

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Engine:
4× Rolls-Royce AE 2100D3
Engine type:
Turboprop
Power:
4 × 4,700 shp  ·  3,505 kW
Avionics:
Lockheed C-130X AMP Avionics
Wing Tips:
No winglets
Seats:
92
Cabin width:
10 ft 3 in · 3.12 m
Cabin height:
ft 12 in · 2.74 m
Cabin length:
55 ft 5 in · 16.90 m
Exterior length:
112 ft 9 in · 34.37 m
Tail height:
38 ft 10 in · 11.84 m
Fuselage diameter:
14 ft 2 in · 4.32 m
Wing span / rotor:
132 ft 7 in · 40.40 m
Baggage volume:
6,003 ft³  ·  170.0 
Max takeoff weight:
175,000 lb  ·  79,500 kg
Max landing weight:
130,000 lb  ·  59,000 kg
Max Payload:
47,400 lb  ·  21,500 kg
Fuel capacity:
9,700 gal  ·  36,600 L  ·  29,300 kg  (Jet A)
Max cruise speed:
365 kt  ·  420 mph  ·  676 km/h
Approach speed (Vref):
120 kt  ·  138 mph  ·  222 km/h
Range:
2,390 nm  ·  2,750 mi  ·  4,430 km
Fuel burn:
0.22 nm/gal  ·  0.11 km/L
Ceiling:
33,000 ft  ·  10,100 m
Rate of climb:
1,830 ft/min  ·  m/s
Takeoff distance:
5,150 ft  ·  1,570 m
Landing distance:
2,600 ft  ·  790 m
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