The HC-130P is a variant of the C-130 Hercules transport aircraft operated by the U.S. Air Force as a combat
search and rescue platform and to extend the range of combat search and rescue helicopters by the provision
of in-air refuelling. Lockheed HC-130P Specifications: - Crew: 5 to 7 personnel
- 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: 76,780 lb (34,826)
- Max takeoff weight: 175,000 lb (79,379 kg)
- Engines: Four 4,300 shp (3,210 kW) Allison T56-A-15 turboprops
- Maximum speed: 330 knots (380 mph, 611 km/h)
- Cruise speed: 290 knots (333 mph, 537 km/h)
- Range: 4,500 nm (5,178 mi, 8,334 km)
- Service ceiling 33,000 ft (10,000 m)
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