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Hirth F-263

The Hirth F-263 is a twin cylinder, in-line, two stroke, carburetted aircraft engine that was designed for use on ultralight aircraft. It was manufactured by Hirth of Germany, but was discontinued about 2001.[1]

Hirth F-263
Type Twin cylinder two-stroke aircraft engine
National origin Germany
Manufacturer Hirth

Development

The F-263 uses fan cooling and piston-ported induction, with a single Bing carburetor and single capacitor discharge ignition. The cylinder walls are electrochemically coated with Nikasil. Standard starting is recoil start. A gearbox reduction drive system and electric start were factory options.[1]

The engine produces 31 hp (23 kW) and runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil. Recommended time between overhauls is 1000 hours.[1]

Applications

Specifications (F-263)

Data from Cliche[1]

General characteristics

  • Type: Twin cylinder, two-stroke, aircraft engine
  • Displacement: 383 cc (23.4 cu in)
  • Dry weight: 70 lb (31.8 kg)

Components

Performance

  • Power output: 30 hp (22 kW)

See also

References

  1. ^ a b c d Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page G-3 Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4
  2. ^ Ultralight Home Page (n.d.). "Ultralight/Microlight aircraft specs USA". Retrieved 16 December 2009. {{cite web}}: |last= has generic name (help)
  3. ^ Fraser, Richard (2009). "Phillipe Balligand and his HM293". Retrieved 16 December 2009.

hirth, twin, cylinder, line, stroke, carburetted, aircraft, engine, that, designed, ultralight, aircraft, manufactured, hirth, germany, discontinued, about, 2001, type, twin, cylinder, stroke, aircraft, enginenational, origin, germanymanufacturer, hirth, conte. The Hirth F 263 is a twin cylinder in line two stroke carburetted aircraft engine that was designed for use on ultralight aircraft It was manufactured by Hirth of Germany but was discontinued about 2001 1 Hirth F 263Type Twin cylinder two stroke aircraft engineNational origin GermanyManufacturer Hirth Contents 1 Development 2 Applications 3 Specifications F 263 3 1 General characteristics 3 2 Components 3 3 Performance 4 See also 5 ReferencesDevelopment EditThe F 263 uses fan cooling and piston ported induction with a single Bing carburetor and single capacitor discharge ignition The cylinder walls are electrochemically coated with Nikasil Standard starting is recoil start A gearbox reduction drive system and electric start were factory options 1 The engine produces 31 hp 23 kW and runs on a 50 1 pre mix of unleaded 93 octane auto fuel and oil Recommended time between overhauls is 1000 hours 1 Applications EditHowland H 3 Pegasus 2 Falconar HM 293 3 Specifications F 263 EditData from Cliche 1 General characteristics Type Twin cylinder two stroke aircraft engine Displacement 383 cc 23 4 cu in Dry weight 70 lb 31 8 kg Components Valvetrain piston ported Fuel system 1 X Bing carburetor Fuel type unleaded 93 octane auto fuel Oil system 50 1 fuel oil premix Cooling system fan forced air Reduction gear optional gearboxPerformance Power output 30 hp 22 kW See also EditArrow 250 Kawasaki 440References Edit a b c d Cliche Andre Ultralight Aircraft Shopper s Guide 8th Edition page G 3 Cybair Limited Publishing 2001 ISBN 0 9680628 1 4 Ultralight Home Page n d Ultralight Microlight aircraft specs USA Retrieved 16 December 2009 a href Template Cite web html title Template Cite web cite web a last has generic name help Fraser Richard 2009 Phillipe Balligand and his HM293 Retrieved 16 December 2009 Retrieved from https en wikipedia org w index php title Hirth F 263 amp oldid 1068083443, wikipedia, wiki, book, books, library,

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