UH-1N Twin Huey
Summary
| Category | Military Helicopters |
| Origin country | 🇺🇸 United States |
| Manufacturer | Bell |
| First flight | 1 April 1969 |
| Year introduced | 1970 |
Technical specifications
| Version: USMC UH-1N, as modified | |
|---|---|
| Crew | 4 (pilot, co-pilot, crew chief, gunner) |
| Operational range | 459 km (285 mi) |
| Maximum speed | 240 km/h (149 mph) |
| Wing area | 168 m² (1808.3 sqft) |
| Wingspan | 14.6 m (48.0 ft) |
| Height | 4.4 m (14.4 ft) |
| Length | 17.6 m (57.7 ft) |
| Service ceiling | 5,300 m (17,388 ft) |
| Max. takeoff weight | 4,763 kg (10,501 lbs) |
| Climb rate | 8.92 m/s (29.3 ft/s) |
| Powerplant | 2 x Pratt & Whitney Canada T400-CP-400 delivering 465 kW each |
Current operating countries
All operators
Armament
Description
The Bell UH-1N Twin Huey is a twin-engine medium military helicopter developed from the stretched-fuselage Bell 205. Designed by Bell Helicopter following 1968 negotiations with the Canadian Forces, the aircraft performed its maiden flight in April 1969. The US military subsequently ordered 294 aircraft under the UH-1N designation, with deliveries starting in 1970, while Canada procured 50 under the CUH-1N (later CH-135) designation starting in 1971. Agusta also produced the helicopter under license in Italy as the AB-212.
Power is provided by a PT6T-3/T400 Turbo Twin Pac, producing up to 1,342 kW (1,800 shp). If one engine section fails, the remaining section can deliver 671 kW (900 shp) for 30 minutes to maintain cruise performance. The UH-1N is IFR and night-flight capable, featuring duplicate hydraulic, electrical, and fuel systems alongside fire suppression systems. The helicopter has a maximum takeoff weight of 10,500 lb (4,763 kg), an internal cargo capacity of 4,400 lb (1,996 kg), and an external load capacity of up to 5,000 lb (2,268 kg). The cabin can be configured for up to 14 passengers or six medical evacuation litters. USMC variants integrated a stability control augmentation system that replaced the mechanical rotor stabilization bar.
Standard armament consists of a .50 caliber GAU-16 machine gun mounted on the left side and a 7.62 mm GAU-17 minigun or M240 lightweight machine gun on the right side. The helicopter can also carry 2.75-inch (70 mm) rocket pods.
The USAF deployed the UH-1N to Vietnam in October 1970 to support Special Forces reconnaissance missions. USMC and USN operations began in 1971. USMC UH-1Ns provided close air support, reconnaissance, and communications during the 2003 invasion of Iraq and deployed to Afghanistan before their retirement in August 2014. The USAF utilizes the UH-1N to support ICBM launch sites. Internationally, Canada operated the CH-135 in UN peacekeeping missions in Central America, Somalia, and Haiti. Argentina deployed two Bell 212s during the 1982 Falklands War, and Colombia operated the type during its internal armed conflict. Export and licensed operators include Italy, Greece, Iran, Peru, Spain, Turkey, and Venezuela.
Main Variants
- CH-135 Twin Huey: The Canadian Forces version of the UH-1N, of which 50 were procured starting in 1971.
- UH-1N Iroquois: The initial production model utilized by the United States Air Force, Navy, and Marine Corps.
- VH-1N: A specialized VIP transport variant configured for carrying high-ranking officials and the US president.
- HH-1N: A dedicated search and rescue variant.
- Agusta-Bell AB 212ASW: An Italian license-built maritime variant configured for anti-submarine warfare and anti-shipping operations.