Max usable fuel: 1287 lbs. The reactions were so promising that, on 20 April, 1974, Bell announced its decision to go ahead with the Model 222, five prototypes of which were to be built and which were quite similar to the D-306 (the windscreen was improved and the fuselage lengthened by a few inches). 222UT (Utility Twin)Utility version, incorporating the improvements and power plant detailed for the Model 222B. Two-blade tail rotor of stainless steel construction, with preconing, underslung feathering axis and skewed flapping axis. The two Avco Lycoming turboshafts drove a two-blade main rotor through a gearbox with two spiral bevel reductions and one planetary reduction. All Rights Reserved. Bell 222 Ground Support Equipment. The Bell 222 is a twin engine light utility helicopter designed and manufactured by Bell Helicopter Textron, Inc of the USA. Optional layout for a pilot and eight passengers. 222BStandard production model from late 1982. Heliflight Systems (Houston), Aerogulf Sales Co (Dubai), Bemor Agencies (Bermudas), CSE Aviation Ltd (UK) and Astra Helicopters (South Africa) were among the main customers. The Bell 222U Utility Twin is equipped with a skid landing gear. To start with flight of a 230, a changed over 222, occurred on August 12 1991, and Transport Canada confirmation was granted in March 1992. 7848 lb, 3560 kg . The first for Petroleum Helicopters were delivered in January 1980.Production was launched with a backlog of orders for some 140 aircraft and Bell had to boost its planned production from 125 machines the first year to 137. So you can get everyone there and back. In all configurations, there is a bench seat at the back for three, which fits into the L-shape of the fuel tank behind it. Hydraulic disc brakes. Smooth pickups and set downs, basic navigation, holding altitude, etc. External antenna for troop radios, so commanders never lose touch. bfRegisterSummarize("ff_elem13", "", "", "not available", false) The Bell 222 has a light alloy structure, and a fuselage built around a large cabin which can seat two pilots and five or six passengers in the executive trim. And an airframe you can rely on, even in extreme conditions. Incidence 5deg. No movable surfaces. Total 82 built. (adsbygoogle = window.adsbygoogle || []).push({}); The web portal flugzeuginfo.net includes a comprehensive civil and military aircraft encyclopedia. Free-fall extension in emergency. Service ceiling: 12,800 ft.FAA empty weight, 4,250 lb (1930 kg)Standard empty weight: 4860 lbUseful load, 2,950 lb (1 340 kg)Take-off gross weight, 7,200 lb (3270 kg)Fuel flow @ normal cruise: 482 pph. Seating 13 Passengers Emergency EMS Cargo Operations Special Operations Cargo Hook with Capacity of 4500 lbs at … However, engine problems continued to dog all flavors of the 222, and it developed a reputation as … Anti-Corrosion Products. It is employed for corporate, emergency medical or utility transport missions, with seating for up to 10, including the pilot. The designation for Bell 47 is US Army duties was H-13 Sioux. 1258-8000. VFR and single-pilot IFR certification received in Spring 1983; customer deliveries began in September 1983. SPONSONS: Short-span cantilever sponson set low on each side of fuselage, serving as main landing gear housings, fuel tanks and work platforms. In fourteen months, the five prototypes logged more than 600 flying hours and by December, 1977, the figure of 700 hours was reached. The engines were to be either the 500shp Allison 250-C28, the 590shp Lycoming LTS-101 or the 650shp Pratt & Whitney Canada PT7B driving the Bell classic two-blade main rotor. The Bell 222 and 230 are usually flown single-pilot (optional dual controls are available), and can be configured for corporate/… It is a stretched and more powerful development of the Bell 230 , which, in turn, was based on the earlier Bell 222 . Fuel contained in five crash-resistant internal bladders, in fuselage and sponsons, with total capacity of 710 litres in Model 222B. Bell 222 < Back to Fleet < > MANUFACTURER. New-type water-activated emergency pop-out floats optional. Seating configurations include standard seating for a pilot and seven passengers; or executive seating with one to two pilots and seating for five to six. Bell 222 Power Plant: Two Lycoming LTS 101-650C2 turboshafts each with a contingency rating of 675 shp, take-off rating of 615 shp and continuous rating of 590 shp. As a result, Bell decided to proceed with the development and production of the design, which had now been renamed as the Model 222. List of Operators of Bell 222UT: From: Organisation with model 222UT: 1984: Lloyd Helicopters 1984/89 : 1986: Jamaica Defence Force 222 1 1986/88 : 1987: Marine Luchtvaartdienst 222 1 1987/90 : This was the first time that Bell had introduced an all-new civilian helicopter line since the Jetranger. Each blade has a stainless steel spar with bonded glass fibre safety straps to retard crack propagation and offer secondary load path; replaceable stainless steel leading-edge; and afterbody of Nomex honeycomb covered with glass fibre skin. Weather radar, wire-strike technology and an intense searchlight keep you in control of your environment—and out of harm’s way. In March 1974 Bell decided to commit its own resources to the development of a new twin-turbine, ten-seat helicopter. Ventilation standard; air conditioning and heating optional. Strakes added to sponsons. The Bell 222 has two Lycoming turboshaft engines, a streamlined shape, and is available with either retractable undercarriage or fixed skids.It is usually flown single-pilot (optional dual cont… . Fail-safe structure in critical areas. RANGE. The fifth prototype (c/n 47005, N2228X), representative of the production aircraft, was presented at the Paris Air Show in June 1978. Bell 206 Series – 205/212/412 – 222/230, 407 Series, 429 ROTOR DRIVE: Rotors shaft driven through gearbox with two spiral bevel reductions and one planetary reduction. Single wheel and tyre on each unit. Space for 1.05cu.m of baggage aft of cabin, with external door on starboard side. The Bell 222B produced by Bell. You dont need to know much about 135, but 91. Dihedral 3deg 12min. During flight tests several improvements were introduced on the prototypes, the most obvious being a completely new tail configuration. Single-engine rating 548kW. Contribute / share information, experience and/or images, The fields marked with * are required to be entered. You can view all the available GSE for the 222 aircraft below. First flight of a 230, a converted 222, took place on August 12 1991, and Transport Canada certification was awarded in March 1992. ... Jack Load Tester - 35 Ton - 70,000 lbs Capacity. Compare price and specifications of all Bell 222 / 230 / 430 models in our listings. We sell and inventory used and new 222 GSE. Retractable tricycle landing gear replaced by tubular skid gear with lock-on ground handling wheels. Crew door at forward end of cabin on each side; cabin door on each side immediately forward of wing. The Bell 230 is a development of the 222 with two Allison 250 turboshafts instead of the 222's LTS 101s plus other refinements. On 16 January 1980, Petroleum Helicopters Inc (New Orleans) received the first of its sixteen machines soon followed by Schiavone Construction which received an aircraft in executive configuration. Currently, we specialize in the following helicopters for maintenance, repair, and component overhauls. First deliveries of the Model 222UT were in September 1983. The Model 222B Executive is the luxury variant for five or six people with complete systems and avionics such as IFR, Sperry coupled automatic flight control system and VOR/LOC. Powered by Joomla!. 3 Bell 222 Twin Turbine Helicopters for Sale Worldwide. The Model 222 was the first completely new Bell design to reach production status since the JetRanger and the Model 222 was described then as 'the first American made light twin-turbine helicopter'. The twin Lycoming LTS-101-650 engines are mounted side-by-side above the fuselage and have integral particle separators. 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