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General Info

Bell UH-1Y Venom
Super Huey

Role Utility helicopter
National origin United States
Manufacturer Bell Helicopter
First flight 20 December 2001
Introduction 8 August 2008
Status In service Primary user United States Marine CorpsProduced 2001–present Number built 160
Developed from Bell UH-1N Twin Huey

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History Bell Textron Inc. 
Bell UH-1Y Venom Super Huey



he Bell UH-1Y Venom (also called Super Huey) is a twin-engine, medium-sized utility helicopter built by Bell Helicopter under the H-1 upgrade program of the United States Marine Corps. One of the latest members of the numerous Huey family,
the UH-1Y is also called "Yankee", based on the NATO phonetic alphabet pronunciation of its variant letter

Over the years, new avionics and radios, modern door guns, and safety upgrades have greatly increased the UH-1N's empty weight. With a maximum speed around 100 knots (190 km/h) and an inability to lift much more than its own crew, fuel, and ammunition, the UH-1N had limited capabilities as a transport

The UH-1Y variant modernizes the UH-1 design. The Y-model upgrades pilot avionics to a glass cockpit, adds further safety modifications, and provides the UH-1 with a modern forward-looking infrared system. Engine power was increased. Its most noticeable upgrade over previous variants is a four-blade, all-composite rotor system designed to withstand up to 23 mm rounds. By replacing the engines and the two-bladed rotor system with four composite blades, the Y-model returns the Huey to the utility role for which it was designed.

A 21-inch (530 mm) fuselage extension just forward of the main door was added for more capacity. The UH-1Y features upgraded transmissions and a digital cockpit with flat-panel multifunctional displays. Compared to the UH-1N, the Y-model has an increased payload, almost 50% greater range, a reduction in vibration, and higher cruising speed 

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Bell UH-1Y Venom Super Huey

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Howard Bell Textron Inc.

Bell Textron Inc.
Bell UH-1Y Venom Super Huey

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General Info

  • Crew: 2 (pilot and co-pilot)
  • Capacity: 6,660 lb (3,021 kg) / up to ten crashworthy passenger seats / six litters / equivalent cargo
  • Length: 58 ft 4 in (17.78 m)
  • Height: 14 ft 7 in (4.45 m)
  • Empty weight: 11,840 lb (5,371 kg)
  • Max takeoff weight: (8,391 kg)
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Powerplant

  • Powerplant: 2 × General Electric T700-GE-401C turboshaft, 1,828 shp (1,363 kW) each for 2 minutes 30 seconds
    • 1,546 hp (1,153 kW) continuous
    • Main rotor diameter:  (14.88 m)
    • Main rotor area: 1,808 sq ft (168.0 m2)
    • Blade section: Narramore[
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Specifications

  • Maximum speed: 164 kn (189 mph, 304 km/h)
  • Cruise speed: 158 kn (182 mph, 293 km/h)
  • Never exceed speed:  367 km/h)
  • Combat range: 130 nmi (150 mi, 240 km) with 2,182 lb (990 kg) payload
  • Endurance: 3 hours 18 minutes
  • Service ceiling: 20,000 ft (6,100 m) +
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The UH-60 entered service with the U.S. Army's 101st Combat Aviation Brigade of the 101st Airborne Division in June 1979.[92] The U.S. military first used the UH-60 in combat during the invasion of Grenada in 1983.

Bell UH-1Y Venom
Super Huey

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