Specifications (C-130H)

Data from USAF C-130 Hercules fact sheet,^[40] International Directory of Military Aircraft,^[41] Complete Encyclopedia of World Aircraft,^[42] Encyclopedia of Modern Military Aircraft^[43]

General characteristics

• Crew: 5 (two pilots, navigator, flight engineer and loadmaster)
• Capacity:
  
  • 92 passengers or
  • 64 airborne troops or
  • 74 litter patients with 2 medical personnel or
  • 6 pallets or
  • 2–3 HMMWVs or
  • 2 M113 armored personnel carrier
• Payload: 45,000 lb (20,000 kg)
• Length: 97 ft 9 in (29.8 m)
• Wingspan: 132 ft 7 in (40.4 m)
• Height: 38 ft 3 in (11.6 m)
• Wing area: 1,745 ft² (162.1 m²)
• Empty weight: 75,800 lb (34,400 kg)
• Useful load: 72,000 lb (33,000 kg)
• Max takeoff weight: 155,000 lb (70,300 kg)
• Powerplant: 4× Allison T56-A-15 turboprops, 4,590 shp (3,430 kW) each

Performance

• Maximum speed: 320 knots (366 mph, 592 km/h) at 20,000 ft (6,060 m)
• Cruise speed: 292 kn (336 mph, 540 km/h)
• Range: 2,050 nmi (2,360 mi, 3,800 km)
• Service ceiling: 33,000 ft (10,060 m) empty;^[44] 23,000 ft (7,077 m) with 42,000 pounds (19,090 kilograms) payload ()
• Rate of climb: 1,830 ft/min (9.3 m/s)
• Takeoff distance: 3,586 ft (1,093 m) at 155,000 lb (70,300 kg) max gross weight;^[43] 1,400 ft (427 m) at 80,000 lb (36,300 kg) gross weight^[45]