You dont need to know much about 135, but 91. The blades are held to the rotor hub by standard Bell elastomeric bearings. 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 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. 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 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. View all new & used Bell 222 / 230 / 430 Turbine Helicopter aircraft for sale at ASO.com. Tailplane, with slotted leading-edge and endplate fins, mounted midway along rear fuselage. ten-seat light utility helicopter produced by the US-American manufacturer Bell Helicopter Textron. Power loading: 6.4 lbs/hp. 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. bfRegisterSummarize("ff_elem13", "", "", "not available", false) A stereo system and refreshment cabinet are optional. Main rotor diameter, 40 ft 0 in (12,19 m)Overall length, 47 ft 9 in (14,55 m)Overall height, 11 ft l .5 in (3,39 m)Fuselage length: 10.98mUndercarriage -track, 9ft (2,74 m)Wheelbase, 11 ft 9 12 in (3,59 in)Span over sponsons, 14 ft (4,27 m). Airwolf is the title aircraft from a 1980s television series.The aircraft itself was a modified Bell 222 twin-engined light helicopter owned by JetCopters Inc. and built by Bell Helicopter.Bell 222The flying Airwolf helicopter was actually a Bell 222. Replaced from late 1982 by the Model 222B. The Bell 230 is a development of the 222 with two Allison 250 turboshafts instead of the 222's LTS 101s plus other refinements. Small trim tab on each blade. The Bell 222U Utility Twin is equipped with a skid landing gear. Capacity: 9 passengers; Empty weight: 4,577 lbs; Length: 42 ft 2 in; Height: 11 ft 8 in; Rotor diameter: 42 ft; References [edit | edit source] Notes [edit | edit source] ↑ However, engine problems continued to dog all flavors of the 222, and it developed a reputation as … First flight 1 August 1981; FAA certification 30 June 1982. Price: USD $695,000. The tail rotor is also metal with two blades. A rotor brake is standard. Crew. All to transport your team where they’re needed most. Bell 222/230 The Bell 430 is an American twin-engine light-medium helicopter built by Bell Helicopter . MAX SPEED. Bell 206 Series – 205/212/412 – 222/230, 407 Series, 429 130 kt, 240 km/h . SPONSONS: Short-span cantilever sponson set low on each side of fuselage, serving as main landing gear housings, fuel tanks and work platforms. The Bell 222 is a twin-engined max. ROTOR DRIVE: Rotors shaft driven through gearbox with two spiral bevel reductions and one planetary reduction. This proved popular with offshore and medevac operators in particular. We sell and inventory used and new 222 GSE. The Bell 222 is a twin engine light utility helicopter designed and manufactured by Bell Helicopter Textron, Inc of the USA. 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. Five prototypes were built. It is employed for corporate, emergency medical or utility transport missions, with seating for up to 10, including the pilot. ADF, marker beacon receiver, transponder, DME and area navigation. Energy attenuating seats, all with shoulder harness in Model 222B. The website has also a photo gallery and gives you an overview of all aviation museums worldwide. Fuselage Dimensions BELL 212; Length (ft): 42.4 Height (ft): 11.5 Width (ft): 9.3 Typical Configuration ; Crew: 1 Passengers: 14 Fuel Capacity ; Standard (lbs): Close. One-piece nosecone tilts forward and down for access to avionics and equipment bay. Fail-safe structure in critical areas. 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. LANDING GEAR: Hydraulically retractable tricycle type. The Bell 222 was the first light commercial twin turbine engine helicopter developed in the United States. 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. 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. Some special variants with enclosed cabin and fuselage are the Bell 47H (three seats) and the Bell 47J Ranger (four seats). 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. 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. It can accommodate up to eight passengers and could have a fuselage mounted flotation system. Max landing weight: 7850 lbs. Comprehensive data about the Bell 222, including performance and engines, with listings of relevant maintenance, charter, training and completions companies, and news about the aircraft. Transmission rating (two engines) 690kW. ... Jack Load Tester - 35 Ton - 70,000 lbs Capacity. 222B ExecutiveFully equipped for both single- and dual-pilot IFR flight. Incidence 5deg. Blade section Wortmann 090. Fuel contained in five crash-resistant internal bladders, in fuselage and sponsons, with total capacity of 710 litres in Model 222B. ZS-HDF. Accommodation: Up to 10 including pilot. Specs, range, speed, operating weights and performance for the Bell 222B here 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 : A large storage compartment. Oil capacity 6.5 litres per engine. 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. Free-fall extension in emergency. All information is given in good faith and for information purposes only. flugzeuginfo.net is a non-commercial webproject. Single wheel and tyre on each unit. 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). Endurance @ normal cruise: 2.5 hr.Max ramp weight: 7850 lbMax useful load: 2990 lbs. 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. TAIL UNIT: Cantilever structure of light alloy. 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. All Rights Reserved. Valid XHTML and CSS. Smooth pickups and set downs, basic navigation, holding altitude, etc. Each blade is attached to the rotor head by two chordwise bolts. 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. The website is currently in the process of optimizing and will have further functions added in order to improve the usability. RANGE. 324 nm, 600 km . Bell . And an airframe you can rely on, even in extreme conditions. 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. 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. Takeoff (lbs): 7,850 Empty Operating Weight (EOW): 4,904 Speed Knots ; Normal Cruise TAS: 134 Vmo (Max Op) IAS: 150 Luxury equipment includes automatic temperature control, fluorescent and reading lights and window curtains. Optional layout for a pilot and eight passengers. In fourteen months, the five prototypes logged more than 600 flying hours and by December, 1977, the figure of 700 hours was reached. Powered by Joomla!. Long-range cruising speed, 150 mph (241 km/h) at sea levelHovering ceiling (OGE), 8,200 ft (2500 m) in ISA and 4,000 ft (1 220 m) in ISA plus 20 deg CHovering ceiling (IGE), 13,000 ft (3962 m) in ISA and 10,000 ft (3050 m) in ISA plus 20 deg CSingle-engine ceiling, 9,000 ft (2743 m) in ISA and 5,100 ft (1555 m) in ISA plus 20 deg CRange with 20-mm reserve, 400 mls (644 km) at 8,000 ft (2440 m) Max rate of climb: 1580 fpm. The two Avco Lycoming turboshafts drove a two-blade main rotor through a gearbox with two spiral bevel reductions and one planetary reduction. //-->. TBO: 2400 hrMax continuous speed, 173 mph (278 km/h) at sea levelNormal cruise @ 3000 ft: 135 kts. Two additional passengers can be accommodated in a high-density 2-2-3-3 arrangement. The designation for Bell 47 is US Army duties was H-13 Sioux. 3 Bell 222 Twin Turbine Helicopters for Sale Worldwide. Search aircraft for sale for free! Dihedral 3deg 12min. Main rotor engine rpm ratio 1:27.4; tail rotor engine rpm ratio 1:5.08. Max usable fuel: 1287 lbs. MAUW. External antenna for troop radios, so commanders never lose touch. Oleo-pneumatic shock-absorbers, with scissored yoke. Fuselage-mounted flotation system optional. Bell Helicopters for Sale Get email notifications when a new aircraft for sale is listed on AvBuyer. Aircraft Tooling & Hangar Equipment. Space for 1.05cu.m of baggage aft of cabin, with external door on starboard side. New-type water-activated emergency pop-out floats optional. CAPACITY. Rear seat fuel tank, capacity 246 litres, and parcel shelf fuel tank, capacity 181 litres, optional on both models. The basic variant Bell 222 and Bell 222B are equipped with retractable wheel landing gear. Bell 206B III . Columbus Jack. 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. Production ceased in 1989.Versions: 222AInitial production model powered by twin 462kW Lycoming LTS 101 650C-3 turboshaft engines. 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. Small skid below ventral fin for protection in tail-down landing. Model 222UT has skid-type landing gear and lock-on ground handling wheels, with fuselage-mounted flotation system optional. Fixed vertical fin in sweptback upper and lower sections. If you were a flight instructor at any point, its a breeze. The Bell 222 is fitted with two Lycoming/Honeywell LTS101-650 engines which produce a maximum of 592 shaft horsepower each. 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. Optional stereo system and refreshment cabinet. Contribute / share information, experience and/or images, The fields marked with * are required to be entered. More powerful, 510kW Lycoming LTS 101 750C-1 engines; fuselage increased by 0.43m and main rotor diameter 0.69m larger.