C-130 Hercules -5

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* C-130J Specifications and Performance *

1.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

2.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

3.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

4.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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