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The RW-133 was developed in 1979 as an all-new piston engine for amateur-built aircraft, including a new crankcase oil system. The helicopter version features a dry sump oil system and a turbocharger option increasing power to 160 hp (119 kW). [ 1 ]
Five-engined piston helicopters (1 P) This page was last edited on 22 May 2017, at 13:00 (UTC). Text is available under the Creative Commons Attribution ...
Pages in category "Single-engined piston helicopters" The following 171 pages are in this category, out of 171 total. This list may not reflect recent changes .
Data from Brassey's World Aircraft & Systems Directory General characteristics Crew: one Capacity: two passengers Length: 29 ft 3 in (8.92 m) Height: 9 ft 0 in (2.74 m) Empty weight: 1,570 lb (712 kg) Max takeoff weight: 2,600 lb (1,179 kg) Powerplant: 1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine, 225 hp (168 kW) Main rotor ...
Aircraft modified by Aviation Specialties and produced and marketed by Helitec with a 650 hp (480 kW) Garrett AiResearch TPE-331-3U-303 turboshaft and updated equipment. S-55/Mi-24 Orlando Helicopter Airways (OHA) conversion for U.S. Army to simulate the Mil Mi-24. Used newly-designed five-bladed rotor assembly with piston engine. Fifteen ...
A U.S. Coast Guard HUS-1G in 1960. Row of Westland Wessex HU.5, 1978. The Sikorsky H-34 (company designation S-58) is an American piston-engined military utility helicopter originally designed by Sikorsky as an anti-submarine warfare (ASW) aircraft for the United States Navy.
This page was last edited on 15 November 2024, at 06:23 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.
Data from Jane's All The World's Aircraft 1982–83 General characteristics Crew: 1 (optionally 2) Capacity: 6 or 7 pax when passenger module fitted / 2 stretcher patients, 2 seated patients and medical attendant / 900 kg (1,984 lb) pax or liquid chemical / 1,065 kg (2,348 lb) dusting or with platform / 1,100 kg (2,425 lb) with slung load Length: 7.75 m (25 ft 5 in) fuselage Width: 3.64 m (11 ...