Specifications (USMC UH-1N, As Modified)
Data from USMC UH-1N Fact Sheet, The International Directiory of Military Aircraft, 2002-2003
General characteristics
- Crew: 4 (Pilot, copilot, crew chief, gunner)
- Capacity: 6-8 combat-equipped troops, or equivalent cargo
- Length: 41 ft 8 in (12.69 m)
- Rotor diameter: 48 ft 0 in (14.6 m)
- Height: 14 ft 5 in (4.4 m)
- Disc area: 1,808 ft² (168.0 m²)
- Empty weight: 6,000 lb (2,721.5 kg)
- Loaded weight: 10,500 lb (4,762.7 kg)
- Useful load: 4500 lb (2038.0 kg)
- Max. takeoff weight: 10,500 lb (4,762.7 kg)
- Powerplant: 2 × Pratt & Whitney Canada T400-CP-400 turboshaft, 900 shp (671 kW), (total 1,250 shp) each
Performance
- Maximum speed: 130 knots (135 mph, 220 km/h)
- Cruise speed: 110 knots (126 mph, 207.3 km/h)
- Range: 248 nmi (286 mi, 460 km)
- Service ceiling: 17,300 ft (5,273 m)
- Rate of climb: 1,755 ft/min (8.9 m/s)
- Power/mass: hp/lb (W/kg)
Armament
- 2.75-inch (70 mm) rocket pods,
- GAU-16 .50 Cal. machine gun,
- GAU-17 7.62mm minigun or M240 7.62mm lightweight machine gun
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