The Model 525 fea… The website is currently in the process of optimizing and will have further functions added in order to improve the usability. The Bell 222 and 222A are the first production variants and are to be followed by the more powerful Bell 222B. On 15 May, 1980, the Model 222 received FAA approval for single-pilot IFR operation. Powered by Joomla!. On 10 November, 1987, this Model 222 flew with a digital control system developed by Bell and Lucas Aerospace which gave the engine the ability to adapt its characteristics in flight. Bell 212 HP Aero Tech’s Bell 212HP aircraft are high-performance tanked helicopters. The powerplant consists of two 684shp Textron Lycoming LTS 101-750C-1 turboshafts. Each blade is attached to the rotor head by two chordwise bolts. Valid XHTML and CSS. Production ceased in 1989.Versions: 222AInitial production model powered by twin 462kW Lycoming LTS 101 650C-3 turboshaft engines. The Bell 230 is a development of the 222 with two Allison 250 turboshafts instead of the 222's LTS 101s plus other refinements. More powerful, 510kW Lycoming LTS 101 750C-1 engines; fuselage increased by 0.43m and main rotor diameter 0.69m larger. Disc loading: 6.3 lbs/sq.ft. 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. bfRegisterSummarize("ff_elem13", "", "", "not available", false) FUEL CAPACITY. First deliveries of the Model 222UT were in September 1983. Free-fall extension in emergency. TBO: 2400 hrMax continuous speed, 173 mph (278 km/h) at sea levelNormal cruise @ 3000 ft: 135 kts. The Bell 222B produced by Bell. A large storage compartment. This proved popular with offshore and medevac operators in particular. However, engine problems continued to dog all flavors of the 222, and it developed a reputation as … VFR and single-pilot IFR certification received in Spring 1983; customer deliveries began in September 1983. It is employed for corporate, emergency medical or utility transport missions, with seating for up to 10, including the pilot. 222B ExecutiveFully equipped for both single- and dual-pilot IFR flight. Takeoff (lbs): 7,850 Empty Operating Weight (EOW): 4,904 Speed Knots ; Normal Cruise TAS: 134 Vmo (Max Op) IAS: 150 The fuel is contained in five crash resistant tanks located in the fuselage as well as in the sponsons, with a total capacity of 710 litres. 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). 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. The twin Lycoming LTS-101-650 engines are mounted side-by-side above the fuselage and have integral particle separators. Retractable tricycle landing gear replaced by tubular skid gear with lock-on ground handling wheels. The Bell 47 was also produced under license by Agusta (Italy), Kawasaki Heavy Industries (Japan) and Westland (UK). Oleo-pneumatic shock-absorbers, with scissored yoke. Capacity on the 222UT increased by 74 gallons to 310, giving the model an unrefueled range of 486 nautical miles. Crew. All-metal structure of light-alloy sheet and honeycomb. Max usable fuel: 1287 lbs. Completely dry titanium main rotor hub has conical elastomeric bearings. The D-306 could accommodate two pilots and eight passengers (four passengers in executive configuration). Oil capacity 6.5 litres per engine. Compare price and specifications of all Bell 222 / 230 / 430 models in our listings. 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. Honeywell coupled automatic flight control system to provide stability augmentation and automatic hold for attitude, altitude, heading and airspeed, plus VOR/LOC course and glide slope hold during approach. One alternative is the offshore configuration for ferrying eight passengers to offshore oil platforms. Replaced from late 1982 by the Model 222B. This was the first time that Bell had introduced an all-new civilian helicopter line since the Jetranger. 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. The tail rotor is also metal with two blades. To 1992, one hundred and fifty-six Model 222Bs and seventy-two 222UTs have been delivered, mainly on the civil market. Model 222UT has maximum fuel capacity of 931 litres. © 2001 - 2019, Karsten Palt, Leipzig / Germany - All rights reserved. 3 Bell 222 Twin Turbine Helicopters for Sale Worldwide. BELL 222A; Length (ft): 41.0 Height (ft): 11.0 Width (ft): 11.3 Typical Configuration ; Crew: 1 Passengers: 7 Fuel Capacity ; Standard (lbs): 1,260 Standard (gal): 188 Optional (lbs): 0 Optional (gal): 0 Weight ; Max. The fuel is contained in three tanks, one in the fuselage and two in the sponsons into which the main landing gear members retract. 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. Model 222UT has maximum fuel capacity of 931 litres. And an airframe you can rely on, even in extreme conditions. So you can get everyone there and back. 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. A rotor brake is standard. Total of 80 built up to 1989. Sweepback at quarter-chord 3deg 30min. The Model 222B was the second main production variant with accommodation for seven to nine passengers. 236 US Gal . The first model flew in 1976, but it took until 1979 for the 222 to be certified. First flight 7 September 1982. From 1982, the fourth prototype (N680L) served as test bed for the Model 680 four-blade composite bearingless rotor system, designed to improve performance and reduce noise. 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. SPONSONS: Short-span cantilever sponson set low on each side of fuselage, serving as main landing gear housings, fuel tanks and work platforms. ROTOR DRIVE: Rotors shaft driven through gearbox with two spiral bevel reductions and one planetary reduction. RANGE. Get seating for 24 combat troops, provisions for FAST rope and rappel, heightened cabin situational awareness, and a GPS repeater. 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. Close. If you were a flight instructor at any point, its a breeze. 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. We use our 212HP helicopters in firefighting, seismic studies, freight hauling, heavy lift operations, construction support, charter services, and emergency disaster relief. ten-seat light utility helicopter produced by the US-American manufacturer Bell Helicopter Textron. All information is given in good faith and for information purposes only. The executive Bell 222 is sold with full IFR capability. Specs, range, speed, operating weights and performance for the Bell 222B here The main rotor diameter has been increased by 12 in (30,5 cm) and a slightly more powerful version of the Lycoming turboshaft engine has been adopted, to off-set some weight growth attributable to the new tailplane and larger rotor. (adsbygoogle = window.adsbygoogle || []).push({}); The web portal includes a comprehensive civil and military aircraft encyclopedia. Rotor blades do not fold. 9 Passengers + 1 Crew. The website has also a photo gallery and gives you an overview of all aviation museums worldwide. 7848 lb, 3560 kg . Anti-Corrosion Products. Single wheel and tyre on each unit. 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. FUSELAGE: Semi-monocoque structure of light alloy, with limited use of light-alloy honeycomb panels. It is a stretched and more powerful development of the Bell 230 , which, in turn, was based on the earlier Bell 222 . View all new & used Bell 222 / 230 / 430 Turbine Helicopter aircraft for sale at It is anew design and not a member of the Model 222 family, but it most closelyresembles the Model 222 among Bell's product line. In March 1974 Bell decided to commit its own resources to the development of a new twin-turbine, ten-seat helicopter.