Brantly 305

From Wikipedia, the free encyclopedia
Jump to: navigation, search
Brantly 305
Brantly 305 G-ASXF Kidlington 29.10.66 edited-2.jpg
Brantly 305 at Oxford Airport UK in 1966
Role Light helicopter
National origin United States of America
Manufacturer Brantly Helicopter Corporation
First flight January 1964

The Brantly 305 is an American five-seat light helicopter of the 1960s. It is an enlarged version of the Brantly B-2 which was produced by the Brantly Helicopter Corporation.

Design and development[edit]

The five-seater Model 305 helicopter is based on the smaller two-seat Brantly B-2 that was designed by Newby O. Brantly. The helicopter is powered by a Lycoming IVO-540 flat six piston engine.[1] The enlarged cabin has room for five passengers, two side-by-side forward-facing seats and a bench seat at the rear for three passengers.[1] The Model 305 first flew during January 1964 and FAA type approval was received 29 July 1965.[2] 45 were built during the mid 60's by Brantly and Brantly-Hynes produced an improved version in 1985 of which 4 were built. The Brantly 305 suffered from a ground resonance problems.[citation needed] Hynes developed a more powerful and streamline version in 1993, none were produced.[citation needed]

Specifications[edit]

Data from Jane's All The World's Aircraft 1976-77 [3]

General characteristics

Performance

See also[edit]

Related development

References[edit]

  1. ^ a b Orbis 1985, p. 839
  2. ^ "Type Certificate Date Sheet H3SW - Brantly 305". Federal Aviation Authority. 17 October 1990. Retrieved 2009-12-30. 
  3. ^ Taylor 1976, pp. 252–253.
  4. ^ Fuselage length
  • Taylor, John W.R.. Jane's All The World's Aircraft 1976-77. London:Jane's Yearbooks, 1976. ISBN 0-354-00538-3.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing.