Two additional passengers can be accommodated in a high-density 2-2-3-3 arrangement. It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. The Bell 222 was the first light twin-turbine-engine helicopter developed in the USA, becoming a highly popular choice for a variety of corporate journeys. Single-point refuelling on starboard side of fuselage. Small trim tab on each blade. Fuel contained in five crash-resistant internal bladders, in fuselage and sponsons, with total capacity of 710 litres in Model 222B. 222UT (Utility Twin)Utility version, incorporating the improvements and power plant detailed for the Model 222B. The lack of retractable landing gear allowed larger fuel capacity . View all new & used Bell 222 / 230 / 430 Turbine Helicopter aircraft for sale at ASO.com. The Bell 222 and 222A are the first production variants and are to be followed by the more powerful Bell 222B. The blades are held to the rotor hub by standard Bell elastomeric bearings. The Model 525 fea… It is a stretched and more powerful development of the Bell 230 , which, in turn, was based on the earlier Bell 222 . 236 US Gal . Among the main operators are the New York City Police Department, the Port Authority of New York, Michigan State Police, West Virginia State Police and Lloyd Helicopters. Certification by the FAA under FAR Part 29 was received on 16 August, 1979, followed by approval for VFR operation on 20 December of the same year. Initial flight of the first Bell 525 prototype was on 1 July 2015, withflight of a second prototype before the end of that year; three more testfollowed. On 29 July 1982, the 222B became the first transport category helicopter to be certified by the FAA for single-pilot IFR flight without stability augmentation. Transmission rating (two engines) 690kW. Model 222U and 222UT: the Model 222UT (UT for Utility Twin) variant is externally recognisible by its tubular skid undercarriage in place of the usual retractable wheels. This helicopter was evolved from studies begun in the late 1960s which had led, in 1973, to the Design D-306, a twin-turboshaft helicopter. We sell and inventory used and new 222 GSE. In 1982, the Model 222B became the first transport category helicopter to be certificated by the FAA for single-pilot IFR flight without stability augmentation. MAX SPEED. You dont need to know much about 135, but 91. 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. Each blade is attached to the rotor head by two chordwise bolts. The Bell 222 and 230 are usually flown single-pilot (optional dual controls are available), and can be configured for corporate/… Search aircraft for sale for free! First flight 7 September 1982. Bell . The large main rotor with two wide blades is of steel with a honeycomb core. The basic variant Bell 222 and Bell 222B are equipped with retractable wheel landing gear. The design includes two main rotor blades of stainless-steel-fiberglass construction and rotor hub with elastomeric bearings, which are lubricant free. ACCOMMODATION: Pilot and seven passengers in standard 2-3-3 layout, alternatively pilot, co-pilot and six passengers. Bell 212 Turbine Helicopters for Sale In 1970, Bell made major changes to increase the performance of its Model 204 and created the twin turbine Bell 212. Model 222UT has maximum fuel capacity of 931 litres. 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. The tail rotor is also metal with two blades. Energy attenuating seats, all with shoulder harness in Model 222B. Optional stereo system and refreshment cabinet. This proved popular with offshore and medevac operators in particular. 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. SPONSONS: Short-span cantilever sponson set low on each side of fuselage, serving as main landing gear housings, fuel tanks and work platforms. Powered by Joomla!. ROTOR DRIVE: Rotors shaft driven through gearbox with two spiral bevel reductions and one planetary reduction. So you can get everyone there and back. * At Heli-Expo 2012 in Dallas, Bell announced the company's biggestcommercial helicopter ever the "Model 525 Relentless", with a capacity of upto 20 passengers or cargo load of 1,800 kilograms (4,000 pounds). With the fourth prototype (c/n 47004, N680L) a new tail layout was adopted: the T tail was replaced by tailplanes and end-plate fins fixed forward of the rear fuselage. External antenna for troop radios, so commanders never lose touch. Collins Pro Line avionics include dual VHF com, dual VOR nav with glide slope. ten-seat light utility helicopter produced by the US-American manufacturer Bell Helicopter Textron. Fail-safe structure in critical areas. A large storage compartment. Only two aircraft are known to have been taken on charge by military customers: one by the Uruguayan Air Force and the other by the Uruguayan Navy. On 15 May, 1980, the Model 222 received FAA approval for single-pilot IFR operation. All-metal structure of light-alloy sheet and honeycomb. Bell 222/230 The Bell 430 is an American twin-engine light-medium helicopter built by Bell Helicopter . The Bell 230 is an advancement of the 222 with two Allison 250 turboshafts rather than the 222's LTS 101s or more different refinements. And an airframe you can rely on, even in extreme conditions. © 2001 - 2019, Karsten Palt, Leipzig / Germany - All rights reserved. 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. Oil capacity 6.5 litres per engine. Total 82 built. If you can fly, that wont be a problem, either. Dihedral 3deg 12min. 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. Optional layout for a pilot and eight passengers. Baggage capacity, 43 cu ft (1,22 cu.m) in aft cabin and fuselage baggage compartment. Bell focused pylon with nodalisation. The Bell 222 is a twin-engined max. As a result, Bell decided to proceed with the development and production of the design, which had now been renamed as the Model 222. A stereo system and refreshment cabinet are optional. 3 Bell 222 Twin Turbine Helicopters for Sale Worldwide. bfRegisterSummarize("ff_elem13", "", "", "not available", false) Accommodation: Up to 10 including pilot. Disc loading: 6.3 lbs/sq.ft. You can view all the available GSE for the 222 aircraft below. Rotor blades do not fold. Copyright © 2020 all-aero. TBO: 2400 hrMax continuous speed, 173 mph (278 km/h) at sea levelNormal cruise @ 3000 ft: 135 kts. Tailplane, with slotted leading-edge and endplate fins, mounted midway along rear fuselage. Close. 324 nm, 600 km . The Bell 222 is fitted with two Lycoming/Honeywell LTS101-650 engines which produce a maximum of 592 shaft horsepower each. All units retract forward, mainwheels into sponsons. The Model 222 and 222A, first production variants were powered by two 592shp Avco-Lycoming LTS 101-650C-3 engines, their dry weight of only 110kg each providing a maximum power/ weight ratio of 4.58kW/kg at maximum rating. Two-blade tail rotor of stainless steel construction, with preconing, underslung feathering axis and skewed flapping axis. Fuel contained in five crash-resistant internal bladders, in fuselage and sponsons, with total capacity of 710 litres in Model 222B. FUEL CAPACITY. In March 1974 Bell decided to commit its own resources to the development of a new twin-turbine, ten-seat helicopter. In fourteen months, the five prototypes logged more than 600 flying hours and by December, 1977, the figure of 700 hours was reached. Get seating for 24 combat troops, provisions for FAST rope and rappel, heightened cabin situational awareness, and a GPS repeater. Lbmax useful Load: 2990 lbs flight 1 August 1981 ; FAA certification 30 June 1982 eight. By the US-American manufacturer Bell helicopter Textron purposes only prototypes, the fields marked with * are to. Approval for single-pilot IFR certification received in spring 1983 ; customer deliveries began September! 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