UH-1Y Venom

Summary

Category Military Helicopters
Origin country 🇺🇸 United States
ManufacturerBell
First flight20 December 2001
Year introduced2008
Number produced160 units

Technical specifications

Version: UH-1Y Venom
Crew2 (pilot and co-pilot)
Operational range240 km (149 mi)
Endurance3 hours
Maximum speed 304 km/h (189 mph)
Wing area168 m² (1808.3 sqft)
Wingspan14.9 m (48.8 ft)
Height4.5 m (14.6 ft)
Length17.8 m (58.3 ft)
Service ceiling6,100 m (20,013 ft)
Empty weight5,371 kg (11,841 lbs)
Max. takeoff weight8,391 kg (18,499 lbs)
Climb rate12.8 m/s (42.0 ft/s)
Powerplant2 x General Electric T700-GE-401C delivering 682 kW each

Current operating countries

Country Units
United States United States 160
Czechia Czechia 6 (+4)
Romania Romania 0 (+21)

All operators

🇨🇿 Czechia • 🇷🇴 Romania • 🇺🇸 United States

Armament

Missiles payload:

  • Air-to-Ground APKWS II

Bombs payload:

  • Rocket Pod Hydra 70
  • Rocket Pod LAU-68
  • Rocket Pod LAU-61
  • Rocket Pod M260
  • Rocket Pod M261

Bell UH-1Y Venom military helicopters in flight
Bell UH-1Y Venom military helicopters side profile drawing

Description

The Bell UH-1Y Venom, also designated "Yankee" or "Super Huey," is a twin-engine, four-blade, medium-sized utility helicopter manufactured by Bell Textron. Developed under the United States Marine Corps (USMC) H-1 upgrade program initiated in 1996, the UH-1Y was designed alongside the AH-1Z Viper to achieve 84% component commonality, sharing the tail boom, engines, rotor system, drivetrain, and avionics. While initially planned as a remanufacturing program for the UH-1N, the USMC approved all-new production airframes in April 2005. The helicopter completed its first flight on 20 December 2001. Developmental testing concluded in early 2006, followed by operational evaluation at NAS Patuxent River. The USMC certified the UH-1Y as operationally capable in August 2008, and full-rate production began in September 2009. Bell delivered 160 UH-1Y helicopters to the USMC, completing deliveries in January 2019. Production restarted in 2021 to fulfill an export order.

Design

The UH-1Y features a 21-inch (530 mm) fuselage extension forward of the main door, a longer cabin, and larger twin engine exhausts than the UH-1N. Its propulsion system consists of two General Electric T700-GE-401C turboshaft engines, each providing 1,828 shp for 2.5 minutes and 1,546 hp continuous power. This drives a four-blade, all-composite main rotor system designed to withstand ballistic impacts up to 23 mm. The digital glass cockpit features flat-panel multifunctional displays. Mission equipment includes a forward-looking infrared system and the AN/ALQ-231(V)3 Intrepid Tiger II electronic warfare pod, which provides communications jamming and signals intelligence capabilities. The helicopter has an empty weight of 11,840 lb (5,371 kg) and a maximum takeoff weight of 18,500 lb (8,391 kg), with a payload capacity of 6,660 lb (3,021 kg). It has a cruise speed of 158 knots and a combat range of 130 nmi with a 2,182 lb payload.

Armament

Armament is carried on two external stations and two pintle mounts. The external hardpoints support 70 mm Hydra 70 or APKWS II rockets, utilizing LAU-68, LAU-61, M260, or M261 launchers with Mk 66 rockets. The pintle mounts accommodate 7.62 mm M240D machine guns, GAU-17A Gatling guns, GAU-16, or 12.7 mm GAU-21 machine guns.

Operational History

The USMC first deployed the UH-1Y in January 2009 with the 13th Marine Expeditionary Unit. UH-1Y helicopters deployed to Afghanistan starting in 2009, providing close air support during the September 2012 Taliban raid on Camp Bastion. In August 2014, the UH-1Y became the USMC's standard utility helicopter following the retirement of the UH-1N. In August 2016, the 22nd Marine Expeditionary Unit operated the UH-1Y in strikes against ISIL during the Battle of Sirte in Libya. The Czech Republic is the sole export customer, ordering eight UH-1Ys in December 2019, with the first delivery in 2023; two additional airframes are scheduled for transfer under the Excess Defense Articles program. One Czech UH-1Y crashed on 23 July 2026.

Frequently Asked Questions

What type of aircraft is the UH-1Y Venom?
The Bell UH-1Y Venom is a military helicopters aircraft developed by Bell and entered service in 2008.
What is the maximum speed of the UH-1Y Venom?
The Bell UH-1Y Venom has a maximum speed of 304 km/h (188 mph).
What is the range of the UH-1Y Venom?
The Bell UH-1Y Venom has an operational range of 240 km (149 miles). This range can vary based on payload, altitude, and mission profile.
When did the UH-1Y Venom first fly?
The Bell UH-1Y Venom made its first flight on December 20, 2001. It entered operational service in 2008.
How many UH-1Y Venom have been built?
Approximately 160 units of the Bell UH-1Y Venom have been produced since it entered service in 2008.
Which countries operate the UH-1Y Venom?
The Bell UH-1Y Venom is operated by 3 countries with approximately 166 aircraft in active service. The largest operators include United States, Czechia, and Romania.
What is the service ceiling of the UH-1Y Venom?
The Bell UH-1Y Venom has a service ceiling of 6,100 meters (20,013 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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