C130 Captain Sim

[JBI]

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Specifications External Dimensions Value

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 ft2/ 162.12 m2



Internal Dimensions Value

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 ft3 / 128.9 m3



Weights and Loadings Value

Operating weight empty 75,562 lb / 34,274 kg

Max. fuel weight (internal) 45,900 lb / 20,819 kg

Max. payload (2.5 g) 41,790 lb / 18,955 kg

Max. normal takeoff weight 155,000 lb / 70,305 kg

Max. overload takeoff weight 175,000 lb / 79,380 kg

Max. normal landing weight 130,000 lb / 58,965 kg

Max. overload landing weight 155,000 lb / 70,305 kg

Max. zero-fuel weight (2.5 g) 117,350 lb / 53,230 kg

Max. wing loading (normal) 88.83 lb/ft.2/ / 433.7 kg/m2

Max. power loading (normal) 8.44 lb/SHP / 5.14 kg/kW



Performance Value

Max. cruising speed 348 kt / 645 km/h

Econ. cruising speed 339 kt / 628 km/h

Stalling speed 100 kt /185 km/h

Max. rate of climb at sea level 640 m/min / 2100 ft/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 1800 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

Range with 18,144 kg payload and Mil-C-5011A reserves
2,835 n miles / 5,250 km