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Air Sylphe 447

The Air Sylphe 447 is a French powered parachute that was designed and produced by Air Sylphe of Villereau, Nord. Now out of production, when it was available, the aircraft was supplied as a complete ready-to-fly-aircraft.[1]

447
Role Powered parachute
National origin France
Manufacturer Air Sylphe
Status Production completed

The company seems to have gone out of business in the end of 2007 and production ended by that date.[2]

Design and development edit

The Air Sylphe 447 was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 115 kg (254 lb). The aircraft has a standard empty weight of 88 kg (194 lb). It features a 35 m2 (380 sq ft) parachute-style wing, single-place accommodation, tricycle landing gear and a single 40 hp (30 kW) Rotax 447 engine in pusher configuration. The 50 hp (37 kW) Rotax 503 engine was a factory option.[1]

The aircraft carriage is built from metal tubing with a ducted fan derived from an industrial air ventilation system. The main landing gear incorporates spring rod suspension.[1]

The aircraft has an empty weight of 88 kg (194 lb) and a gross weight of 210 kg (463 lb), giving a useful load of 122 kg (269 lb). With full fuel of 18 litres (4.0 imp gal; 4.8 US gal) the payload for crew and baggage is 109 kg (240 lb). A version with a gross weight of 310 kg (683 lb) to accommodate heavier pilots was also built.[1]

Specifications (Air Sylphe 447) edit

Data from Bertrand[1]

General characteristics

  • Crew: one
  • Wingspan: 12.20 m (40 ft 0 in)
  • Wing area: 35 m2 (380 sq ft)
  • Aspect ratio: 4.4:1
  • Empty weight: 88 kg (194 lb)
  • Gross weight: 210 kg (463 lb)
  • Fuel capacity: 18 litres (4.0 imp gal; 4.8 US gal)
  • Powerplant: 1 × Rotax 447 twin cylinder, two-stroke, air-cooled aircraft engine, 30 kW (40 hp)

Performance

  • Maximum speed: 45 km/h (28 mph, 24 kn)
  • Stall speed: 20 km/h (12 mph, 11 kn)
  • Rate of climb: 2 m/s (390 ft/min)
  • Wing loading: 6.0 kg/m2 (1.2 lb/sq ft)

References edit

  1. ^ a b c d e Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 79. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
  2. ^ Air Sylphe (2 February 2011). . Archived from the original on 25 June 2007. Retrieved 26 May 2015.

sylphe, french, powered, parachute, that, designed, produced, sylphe, villereau, nord, production, when, available, aircraft, supplied, complete, ready, aircraft, 447role, powered, parachutenational, origin, francemanufacturer, sylphestatus, production, comple. The Air Sylphe 447 is a French powered parachute that was designed and produced by Air Sylphe of Villereau Nord Now out of production when it was available the aircraft was supplied as a complete ready to fly aircraft 1 447Role Powered parachuteNational origin FranceManufacturer Air SylpheStatus Production completedThe company seems to have gone out of business in the end of 2007 and production ended by that date 2 Design and development editThe Air Sylphe 447 was designed to comply with the US FAR 103 Ultralight Vehicles rules including the category s maximum empty weight of 115 kg 254 lb The aircraft has a standard empty weight of 88 kg 194 lb It features a 35 m2 380 sq ft parachute style wing single place accommodation tricycle landing gear and a single 40 hp 30 kW Rotax 447 engine in pusher configuration The 50 hp 37 kW Rotax 503 engine was a factory option 1 The aircraft carriage is built from metal tubing with a ducted fan derived from an industrial air ventilation system The main landing gear incorporates spring rod suspension 1 The aircraft has an empty weight of 88 kg 194 lb and a gross weight of 210 kg 463 lb giving a useful load of 122 kg 269 lb With full fuel of 18 litres 4 0 imp gal 4 8 US gal the payload for crew and baggage is 109 kg 240 lb A version with a gross weight of 310 kg 683 lb to accommodate heavier pilots was also built 1 Specifications Air Sylphe 447 editData from Bertrand 1 General characteristicsCrew one Wingspan 12 20 m 40 ft 0 in Wing area 35 m2 380 sq ft Aspect ratio 4 4 1 Empty weight 88 kg 194 lb Gross weight 210 kg 463 lb Fuel capacity 18 litres 4 0 imp gal 4 8 US gal Powerplant 1 Rotax 447 twin cylinder two stroke air cooled aircraft engine 30 kW 40 hp Performance Maximum speed 45 km h 28 mph 24 kn Stall speed 20 km h 12 mph 11 kn Rate of climb 2 m s 390 ft min Wing loading 6 0 kg m2 1 2 lb sq ft References edit a b c d e Bertrand Noel Rene Coulon et al World Directory of Leisure Aviation 2003 04 page 79 Pagefast Ltd Lancaster UK 2003 ISSN 1368 485X Air Sylphe 2 February 2011 Air Sylphe Archived from the original on 25 June 2007 Retrieved 26 May 2015 Retrieved from https en wikipedia org w index php title Air Sylphe 447 amp oldid 1113330533, wikipedia, wiki, book, books, library,

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