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'. It had a semi-monocoque light alloy fuselage with a hydraulically retractable tricycle undercarriage. Bell AH-1, UH-1, 204-205, 212, 222, 230 & 412 Hydraulic Ground Handling Wheels AERO Product ID: 2001398 Helicopter ground handling wheels are used to lift a helicopter off the ground for easy movement in the hangar or on the ramp. A stereo system and refreshment cabinet are optional. Baggage capacity, 43 cu ft (1,22 cu.m) in aft cabin and fuselage baggage compartment. Two-blade tail rotor of stainless steel construction, with preconing, underslung feathering axis and skewed flapping axis. Dihedral 3deg 12min. No movable surfaces. 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. The maiden flight of the prototype was expected by the end of 1975 but, in fact, the first prototype (c/n 47001, N9988K) got into the air on Friday 13 August, 1976, with Donald Bloom at the controls. The blades are held to the rotor hub by standard Bell elastomeric bearings. The executive Bell 222 is sold with full IFR capability. The Bell 222 is fitted with two Lycoming/Honeywell LTS101-650 engines which produce a maximum of 592 shaft horsepower each. POWER PLANT: Two Textron Lycoming LTS 101-750C-1 turboshafts, each rated at 510kW for take-off, mounted in a streamline housing above the cabin and aft of the rotor pylon. 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. Specs, range, speed, operating weights and performance for the Bell 222B here Currently, we specialize in the following helicopters for maintenance, repair, and component overhauls. The basic Model 222B feature include: ROTOR SYSTEM: Two-blade main rotor. The twin Lycoming LTS-101-650 engines are mounted side-by-side above the fuselage and have integral particle separators. Disc loading: 6.3 lbs/sq.ft. Heliflight Systems (Houston), Aerogulf Sales Co (Dubai), Bemor Agencies (Bermudas), CSE Aviation Ltd (UK) and Astra Helicopters (South Africa) were among the main customers. Fail-safe structure in critical areas. The two Avco Lycoming turboshafts drove a two-blade main rotor through a gearbox with two spiral bevel reductions and one planetary reduction. Fuel contained in five crash-resistant internal bladders, in fuselage and sponsons, with total capacity of 710 litres in Model 222B. All to transport your team where they’re needed most. The fuel is contained in three tanks, one in the fuselage and two in the sponsons into which the main landing gear members retract. Rear seat fuel tank, capacity 246 litres, and parcel shelf fuel tank, capacity 181 litres, optional on both models. The Bell 230 features more powerful engines, plus other refinements, to improve speed and range. Single wheel and tyre on each unit. Powered by Joomla!. Ventilation standard; air conditioning and heating optional. Optional layout for a pilot and eight passengers. First flight 7 September 1982. Its cabin holds a maximum of ten persons with one-two pilots and eight to nine passengers. Price: USD $695,000. MAUW. Search aircraft for sale for free! Compare price and specifications of all Bell 222 / 230 / 430 models in our listings. ACCOMMODATION: Pilot and seven passengers in standard 2-3-3 layout, alternatively pilot, co-pilot and six passengers. 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. It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. Fixed vertical fin in sweptback upper and lower sections. 130 kt, 240 km/h . 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. Transmission rating (two engines) 690kW. Seating 13 Passengers Emergency EMS Cargo Operations Special Operations Cargo Hook with Capacity of 4500 lbs at … The first model flew in 1976, but it took until 1979 for the 222 to be certified. Bell focused pylon with nodalisation. Capacity on the 222UT increased by 74 gallons to 310, giving the model an unrefueled range of 486 nautical miles. Section NACA 0035. Max usable fuel: 1287 lbs. FUEL CAPACITY. TBO: 2400 hrMax continuous speed, 173 mph (278 km/h) at sea levelNormal cruise @ 3000 ft: 135 kts. Retractable tricycle landing gear replaced by tubular skid gear with lock-on ground handling wheels. Optional stereo system and refreshment cabinet. Crew door at forward end of cabin on each side; cabin door on each side immediately forward of wing. View all new & used Bell 222 / 230 / 430 Turbine Helicopter aircraft for sale at ASO.com. Completely dry titanium main rotor hub has conical elastomeric bearings. All information is given in good faith and for information purposes only. ten-seat light utility helicopter produced by the US-American manufacturer Bell Helicopter Textron. The Bell 47 was also produced under license by Agusta (Italy), Kawasaki Heavy Industries (Japan) and Westland (UK). flugzeuginfo.net is a non-commercial webproject. Standard seating for a pilot and six or seven passengers. Collins Pro Line avionics include dual VHF com, dual VOR nav with glide slope. First flight of a 230, a converted 222, took place on August 12 1991, and Transport Canada certification was awarded in March 1992. 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. 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. Side-By-Side above the fuselage and sponsons, with automatic temperature control, fluorescent and reading lights window... / 230 / 430 models in our listings the lack of retractable landing.... 101-750C-1 turboshafts sea levelNormal cruise @ 3000 ft: 135 kts, Karsten,. Control of your environment—and out of harm ’ s way and reading lights, window curtains extreme conditions for and... It provides code tables for aerodromes, air operators including the pilot September 1983 currently we. 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