VFR and single-pilot IFR certification received in Spring 1983; customer deliveries began in September 1983. 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. Five prototypes were built. Optional layout for a pilot and eight passengers. Max sling load: 2100 lbs. © 2001 - 2019, Karsten Palt, Leipzig / Germany - All rights reserved. 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 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. Two-blade tail rotor of stainless steel construction, with preconing, underslung feathering axis and skewed flapping axis. Each blade is attached to the rotor head by two chordwise bolts. Baggage capacity, 43 cu ft (1,22 cu.m) in aft cabin and fuselage baggage compartment. The Bell 222 is a twin engine light utility helicopter designed and manufactured by Bell Helicopter Textron, Inc of the USA. 9 Passengers + 1 Crew. Bell Helicopters for Sale Get email notifications when a new aircraft for sale is listed on AvBuyer. Compare price and specifications of all Bell 222 / 230 / 430 models in our listings. ... Jack Load Tester - 35 Ton - 70,000 lbs Capacity. 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. Bell . Luxury accommodation for five or six passengers, with automatic temperature control, fluorescent and reading lights, window curtains and ceiling speakers. Max usable fuel: 1287 lbs. Valid XHTML and CSS. Hydraulic disc brakes. 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. FUEL CAPACITY. RANGE. To 1992, one hundred and fifty-six Model 222Bs and seventy-two 222UTs have been delivered, mainly on the civil market. It is a stretched and more powerful development of the Bell 230 , which, in turn, was based on the earlier Bell 222 . The Bell 230 is a development of the 222 with two Allison 250 turboshafts instead of the 222's LTS 101s plus other refinements. Bell 222/230 The Bell 430 is an American twin-engine light-medium helicopter built by Bell Helicopter . 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. 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. Seating for 14 troops. On 18 January 1981, Bell Helicopters delivered its 25,000th helicopter, a Model 222, to Omniflight Helicopters. 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. Single-engine rating 548kW. The Model 525 fea… Seating 13 Passengers Emergency EMS Cargo Operations Special Operations Cargo Hook with Capacity of 4500 lbs at … All information is given in good faith and for information purposes only. The Bell 222U Utility Twin is equipped with a skid landing gear. 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). Energy attenuating seats, all with shoulder harness in Model 222B. 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. It is a turboshaft engine with a 1-stage low-pressure axial compressor and a 1-stage high-pressure centrifugal compressor, annular combustors, and 1-stage high-pressure turbine and 1-stage low-pressure turbine. bfRegisterSummarize("ff_elem13", "", "", "not available", false) Single wheel and tyre on each unit. TBO: 2400 hrMax continuous speed, 173 mph (278 km/h) at sea levelNormal cruise @ 3000 ft: 135 kts. Accommodation: Up to 10 including pilot. Self-centring nosewheel, swivelling through 360degrees. 222UT (Utility Twin)Utility version, incorporating the improvements and power plant detailed for the Model 222B. Crew. FUSELAGE: Semi-monocoque structure of light alloy, with limited use of light-alloy honeycomb panels. 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, … Powered by Joomla!. ADF, marker beacon receiver, transponder, DME and area navigation. Bell focused pylon with nodalisation. 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. Takeoff (lbs): 7,850 Empty Operating Weight (EOW): 4,904 Speed Knots ; Normal Cruise TAS: 134 Vmo (Max Op) IAS: 150 You dont need to know much about 135, but 91. First deliveries of the Model 222UT were in September 1983. 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. The lack of retractable landing gear allowed larger fuel capacity . Mainwheel tyres size 6.00-6, pressure 5.18 bars. New-type water-activated emergency pop-out floats optional. The Bell 222 is a twin-engined max. Space for 1.05cu.m of baggage aft of cabin, with external door on starboard side. Max landing weight: 7850 lbs. This proved popular with offshore and medevac operators in particular. All to transport your team where they’re needed most. flugzeuginfo.net is a non-commercial webproject. 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. The Bell 222 and 230 are usually flown single-pilot (optional dual controls are available), and can be configured for corporate/… 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. Specs, range, speed, operating weights and performance for the Bell 222B here On 15 May, 1980, the Model 222 received FAA approval for single-pilot IFR operation. 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. Free-fall extension in emergency. So you can get everyone there and back. 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 tail rotor is also metal with two blades. 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 D-306 could accommodate two pilots and eight passengers (four passengers in executive configuration). Bell 222 Ground Support Equipment. Blade section Wortmann 090. Main rotor engine rpm ratio 1:27.4; tail rotor engine rpm ratio 1:5.08. Crew door at forward end of cabin on each side; cabin door on each side immediately forward of wing. 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. 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. Total of 26 produced between 1982 and 1987. 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'. Transmission rating (two engines) 690kW. Thickness chord ratio 8 per cent. This variant received VFR and single-pilot IFR certification during the spring of 1983. Nosewheel tyre size 5.00-5, pressure 4.14 bars. The two Avco Lycoming turboshafts drove a two-blade main rotor through a gearbox with two spiral bevel reductions and one planetary reduction. The powerplant is the same as for the Model 222B but fuel capacity has been increased to 930 litres. The Bell 222 and 222A are the first production variants and are to be followed by the more powerful Bell 222B. Production ceased in 1989.Versions: 222AInitial production model powered by twin 462kW Lycoming LTS 101 650C-3 turboshaft engines. 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. The basic variant Bell 222 and Bell 222B are equipped with retractable wheel landing gear. (adsbygoogle = window.adsbygoogle || []).push({}); The web portal flugzeuginfo.net includes a comprehensive civil and military aircraft encyclopedia. Bell focused pylon with nodalisation. If you were a flight instructor at any point, its a breeze. Some special variants with enclosed cabin and fuselage are the Bell 47H (three seats) and the Bell 47J Ranger (four seats). 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 skid-type landing gear and lock-on ground handling wheels, with fuselage-mounted flotation system optional. Model 222UT has maximum fuel capacity of 931 litres. A large storage compartment. As a result, Bell decided to proceed with the development and production of the design, which had now been renamed as the Model 222. Tailplane, with slotted leading-edge and endplate fins, mounted midway along rear fuselage. Disc loading: 6.3 lbs/sq.ft. 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. TAIL UNIT: Cantilever structure of light alloy.