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SA 315B Lama, 2003. The Lama was developed specifically to provide a rotorcraft with exceptional high-altitude performance. In practice, the type found considerable use within regions that possessed extensive mountain ranges, such as South America and India, being capable of lifting loads and deploying personnel in areas that had been previously impossible to have otherwise achieved.
The Bell 400 TwinRanger featured a reprofiled fuselage, two Allison 250 turboshafts, the OH-58D Kiowa's four-bladed main rotor, and a new shrouded tail rotor. [1] Bell also planned the single-engine 400A, and the 440 twin with a larger fuselage made possible by a high degree of composites. [2] The Bell 400 first flew on April 4, 1984.
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The TwinRanger name dates from the mid-1980s when Bell developed the Bell 400 TwinRanger, but it never entered production. [16] In 1989, Tridair Helicopters began developing a twin-engine conversion of the LongRanger, the Gemini ST. The prototype's first flight was on January 16, 1991, while full FAA certification was awarded in November.
The RotorWay Helicopter Manufacturing Company, formerly called RotorWay International, was a manufacturer of kit helicopters located in Chandler, Arizona, United States. The company was founded by B.J. Schramm in 1961 as RotorWay Aircraft.
Today, on most modern aircraft the swashplate is above the transmission and the pushrods are visible outside the fuselage, but a few early designs, notably light helicopters built by Enstrom Helicopter, placed it underneath the transmission and enclosed the rotating pushrods inside the mainshaft. This reduces rotor hub drag since there are no ...
After Schweizer acquired the FAA Type Certificate, the helicopter was known for a short time as the Schweizer-Hughes 300C and then simply, the Schweizer 300C. The basic design remained unchanged over the years. Between Hughes and Schweizer, nearly 3,000 copies of the Model 269/300 have been built and flown over the last 50 years.
Data from Bell Helicopter, International Directory of Civil Aircraft, Aerospace-Technology [unreliable source?] General characteristics Crew: 2 Capacity: 7 passengers / 2,960 lb (1,343 kg) internal load Length: 37 ft 6 in (11.43 m) Height: 10 ft 6 in (3.20 m) with standard skids Empty weight: 3,881 lb (1,760 kg) Max takeoff weight: 6,550 lb (2,971 kg) Powerplant: 2 × Pratt & Whitney Canada ...