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C-130J Specifications and Performance

External Dimensions
Wing Span 132.6 ft / 40.41 m
Wing Aspect Ratio 10.1
Length (Overall) 97.75 ft / 29.79 m
Height (Overall) 38.8 ft / 11.84 m
Tailplane Span 52.7 ft / 16.05 m
Wheel Track 14.25 ft / 4.34 m
Propeller Diameter 13.5 ft / 4.11 m
Wing Area (gross) 1,745 sq. ft / 162.12 sq. m
Internal Dimensions
Cabin Length (excluding ramp) 40 ft / 12.19 m
Cabin Length (including ramp) 50.7 ft / 15.44 m
Max. Width 10.25 ft / 3.12 m
Max. Height 9 ft / 2.74 m
Total useable volume 4,551 cubic ft / 128.9 cubic m
Weights and loadings
Operating Empty Weight 75,562 lbs / 34,274 kg
Max. Fuel Weight (internal) 45,900 lbs / 20,519 kg
Max. Payload, 2.5 g 41,790 lbs / 18,955 kg
Max. Normal Takeoff Weight 155,000 lbs / 70,305 kg
Max. Overload Takeoff Weight 175,000 lbs / 79,380 kg
Max. Normal Landing Weight 130,000 lbs / 58,965 kg
Max. Overload Landing Weight 155,000 lbs / 70,305 kg
Max Zero-Fuel Weight, 2.5 g 117,350 lbs / 53,230 kg
Max. Wing Loading (normal) 88.83 lb/sq ft / 433.7 kg/sq m
Max. Power Loading (normal) 8.44 lbs/shp / 5.14 kg/kW
Performance (at max normal takeoff weight, unless indicated otherwise)
Max. Cruising Speed 348 kts / 645 km/h
Economy Cruising Speed 339 kts / 628 km/h
Stalling Speed 100 kts / 185 km/h
Max. Rate of Climb at Sea Level 2,100 ft/min / 640 m/min
Time to 6,100 m 12 min
Cruising Altitude 28,000 ft / 8,535 m
Service Ceiling at 66,680 kg AUW 30,560 ft / 9,315 m
Service Ceiling, OEI, at 66,680 kg AUW 22,820 ft / 6,955 m
Takeoff Run 3,290 ft / 1,003 m
Takeoff Run to 15 m 4,700 ft / 1,433 m
Takeoff Run using max. effort procedures 1,800 ft / 549 m
Landing from 15 m at 58,967 kg AUW 2,550 ft / 777 m
Landing Run at 58,967 kg AUW 1,400 ft / 427 m
Runway LCN: asphalt 37
Runway LCN: concrete 42
Range with 18,144 kg payload and MIL-C-5011A reserves 2,835 nm / 5,250 km



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