The Model 525 fea… One-piece nosecone tilts forward and down for access to avionics and equipment bay. Capacity on the 222UT increased by 74 gallons to 310, giving the model an unrefueled range of 486 nautical miles. 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. Fuselage-mounted flotation system optional. View all new & used Bell 222 / 230 / 430 Turbine Helicopter aircraft for sale at ASO.com. Fixed vertical fin in sweptback upper and lower sections. Fuel contained in five crash-resistant internal bladders, in fuselage and sponsons, with total capacity of 710 litres in Model 222B. Bell . A large storage compartment. ZS-HDF. Its cabin holds a maximum of ten persons with one-two pilots and eight to nine passengers. Buy and sell planes and helicopters online at GlobalPlaneSearch.com. On 15 May, 1980, the Model 222 received FAA approval for single-pilot IFR operation. Completely dry titanium main rotor hub has conical elastomeric bearings. External antenna for troop radios, so commanders never lose touch. Thickness chord ratio 8 per cent. Bell 206 Series – 205/212/412 – 222/230, 407 Series, 429 Model 222UT has skid-type landing gear and lock-on ground handling wheels, with fuselage-mounted flotation system optional. (adsbygoogle = window.adsbygoogle || []).push({}); The web portal flugzeuginfo.net includes a comprehensive civil and military aircraft encyclopedia. Free-fall extension in emergency. Total of 80 built up to 1989. 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. Baggage capacity, 43 cu ft (1,22 cu.m) in aft cabin and fuselage baggage compartment. Disc loading: 6.3 lbs/sq.ft. Model 222UT has maximum fuel capacity of 931 litres. ADF, marker beacon receiver, transponder, DME and area navigation. 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. The basic variant Bell 222 and Bell 222B are equipped with retractable wheel landing gear. The Bell 230 is a development of the 222 with two Allison 250 turboshafts instead of the 222's LTS 101s plus other refinements. 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. This proved popular with offshore and medevac operators in particular. The website has also a photo gallery and gives you an overview of all aviation museums worldwide. The powerplant consists of two 684shp Textron Lycoming LTS 101-750C-1 turboshafts. To 1992, one hundred and fifty-six Model 222Bs and seventy-two 222UTs have been delivered, mainly on the civil market. Get seating for 24 combat troops, provisions for FAST rope and rappel, heightened cabin situational awareness, and a GPS repeater. A rotor brake is standard. Max landing weight: 7850 lbs. The Bell 222 can be configured in 5 or 6-seat executive layouts , or can accommodate up to 8 passengers in a utility configuration, with a bench seat at the back for three, … 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. ten-seat light utility helicopter produced by the US-American manufacturer Bell Helicopter Textron. The lack of retractable landing gear allowed larger fuel capacity . Columbus Jack. Total 82 built. So you can get everyone there and back. We use our 212HP helicopters in firefighting, seismic studies, freight hauling, heavy lift operations, construction support, charter services, and emergency disaster relief. Heliflight Systems (Houston), Aerogulf Sales Co (Dubai), Bemor Agencies (Bermudas), CSE Aviation Ltd (UK) and Astra Helicopters (South Africa) were among the main customers. * 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). First flight 1 August 1981; FAA certification 30 June 1982. As Canada’s electric vehicle market continues to expand, MobileSyrup had the opportunity to chat with GM Canada CEO Scott Bell about the company’s electric vision for the future, the recently launched EV Hummer and what role Canada plays in GM’s future. Mainwheel tyres size 6.00-6, pressure 5.18 bars. However, engine problems continued to dog all flavors of the 222, and it developed a reputation as … 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. 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. //-->. The basic Model 222B feature include: ROTOR SYSTEM: Two-blade main rotor. The blades are held to the rotor hub by standard Bell elastomeric bearings. MAX SPEED. Close. You can view all the available GSE for the 222 aircraft below. 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. The executive Bell 222 is sold with full IFR capability. Optional stereo system and refreshment cabinet. 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. 222BStandard production model from late 1982. TAIL UNIT: Cantilever structure of light alloy. 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. Single-point refuelling on starboard side of fuselage. The first model flew in 1976, but it took until 1979 for the 222 to be certified. This variant received VFR and single-pilot IFR certification during the spring of 1983. CAPACITY. 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. The powerplant is the same as for the Model 222B but fuel capacity has been increased to 930 litres. Bell Helicopters for Sale Get email notifications when a new aircraft for sale is listed on AvBuyer. It can accommodate up to eight passengers and could have a fuselage mounted flotation system. SPONSONS: Short-span cantilever sponson set low on each side of fuselage, serving as main landing gear housings, fuel tanks and work platforms. Contribute / share information, experience and/or images, The fields marked with * are required to be entered. Max sling load: 2100 lbs. Two additional passengers can be accommodated in a high-density 2-2-3-3 arrangement. Each blade is attached to the rotor head by two chordwise bolts. And an airframe you can rely on, even in extreme conditions. Single wheel and tyre on each unit. Compare price and specifications of all Bell 222 / 230 / 430 models in our listings. Nosewheel tyre size 5.00-5, pressure 4.14 bars. First deliveries of the Model 222UT were in September 1983. You dont need to know much about 135, but 91. 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. 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. It is employed for corporate, emergency medical or utility transport missions, with seating for up to 10, including the pilot. FUSELAGE: Semi-monocoque structure of light alloy, with limited use of light-alloy honeycomb panels. 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. Tailplane, with slotted leading-edge and endplate fins, mounted midway along rear fuselage. 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. It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. 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. Incidence 5deg. Crew. It was used in the 1980s TV Show Airwolf Production ended in … 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. 130 kt, 240 km/h . Search aircraft for sale for free! This was the first time that Bell had introduced an all-new civilian helicopter line since the Jetranger. During flight tests several improvements were introduced on the prototypes, the most obvious being a completely new tail configuration. Replaced from late 1982 by the Model 222B. 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. 236 US Gal . 222UT (Utility Twin)Utility version, incorporating the improvements and power plant detailed for the Model 222B. Weather radar, wire-strike technology and an intense searchlight keep you in control of your environment—and out of harm’s way. The design includes two main rotor blades of stainless-steel-fiberglass construction and rotor hub with elastomeric bearings, which are lubricant free. flugzeuginfo.net is a non-commercial webproject. Section NACA 0035. Luxury accommodation for five or six passengers, with automatic temperature control, fluorescent and reading lights, window curtains and ceiling speakers. In fourteen months, the five prototypes logged more than 600 flying hours and by December, 1977, the figure of 700 hours was reached. Fail-safe structure in critical areas. 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 : In March 1974 Bell decided to commit its own resources to the development of a new twin-turbine, ten-seat helicopter. 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'. 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): Space for 1.05cu.m of baggage aft of cabin, with external door on starboard side. Dihedral 3deg 12min. Aircraft Tooling & Hangar Equipment. RANGE. The Model 222B incorporates numerous improvements such as a taller main rotor mast, increased diameter narrow-chord blades, larger tail rotor and lengthened tail boom. Rear seat fuel tank, capacity 246 litres, and parcel shelf fuel tank, capacity 181 litres, optional on both models. 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. Standard seating for a pilot and six or seven passengers. 1 / 2. © 2001 - 2019, Karsten Palt, Leipzig / Germany - All rights reserved. Self-centring nosewheel, swivelling through 360degrees. All units retract forward, mainwheels into sponsons. 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. On 18 January 1981, Bell Helicopters delivered its 25,000th helicopter, a Model 222, to Omniflight Helicopters. The Bell 222 is fitted with two Lycoming/Honeywell LTS101-650 engines which produce a maximum of 592 shaft horsepower each. The Bell 222 and 222A are the first production variants and are to be followed by the more powerful Bell 222B. Specs, range, speed, operating weights and performance for the Bell 222B here 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. TBO: 2400 hrMax continuous speed, 173 mph (278 km/h) at sea levelNormal cruise @ 3000 ft: 135 kts. It is a stretched and more powerful development of the Bell 230 , which, in turn, was based on the earlier Bell 222 . Currently, we specialize in the following helicopters for maintenance, repair, and component overhauls. 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). The two Avco Lycoming turboshafts drove a two-blade main rotor through a gearbox with two spiral bevel reductions and one planetary reduction. The D-306 could accommodate two pilots and eight passengers (four passengers in executive configuration). ROTOR DRIVE: Rotors shaft driven through gearbox with two spiral bevel reductions and one planetary reduction. New-type water-activated emergency pop-out floats optional. Smooth pickups and set downs, basic navigation, holding altitude, etc. Small trim tab on each blade. The fifth prototype (c/n 47005, N2228X), representative of the production aircraft, was presented at the Paris Air Show in June 1978. Rear seat fuel tank, capacity 246 litres, and parcel shelf fuel tank, capacity 181 litres, optional on both models. Thanks for contributing, sharing and contacting us. 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. Two-blade tail rotor of stainless steel construction, with preconing, underslung feathering axis and skewed flapping axis. All Rights Reserved. 222B ExecutiveFully equipped for both single- and dual-pilot IFR flight. 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 Bell 222 and 230 are usually flown single-pilot (optional dual controls are available), and can be configured for corporate/… The Bell 222 was the first light commercial twin turbine engine helicopter developed in the United States. Transmission rating (two engines) 690kW. Takeoff (lbs): 7,850 Empty Operating Weight (EOW): 4,904 Speed Knots ; Normal Cruise TAS: 134 Vmo (Max Op) IAS: 150 Price: USD $695,000. 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. As a result, Bell decided to proceed with the development and production of the design, which had now been renamed as the Model 222. Anti-Corrosion Products. Strakes added to sponsons. Powered by Joomla!. Small skid below ventral fin for protection in tail-down landing. 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. 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. I did not work in AirMed, but PHI is pretty standardized. Luxury equipment includes automatic temperature control, fluorescent and reading lights and window curtains.