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Aviadesign A-16 Sport Falcon

From Wikipedia, the free encyclopedia
American light-sport aircraft

A-16 Sport Falcon
General information
TypeLight-sport aircraft
National originUnited States
ManufacturerAviadesign
StatusProduction completed
Number built2
History
Introduction date2007
First flight2006

TheAviadesign A-16 Sport Falcon is an Americanlight-sport aircraft that was designed byAviadesign, acertified aircraft modification company based inCamarillo, California. The A-16 was announced atSun 'n Fun April 2006 and introduced at the LSA Expo held inSebring, Florida in 2007. The aircraft was to be supplied as a complete ready-to-fly-aircraft.[1][2][3][4][5]

Jane's Information Group reports that two prototypes were completed by 2006, but it is not clear if any other examples ever flew before the company went out of business.[3]

Design and development

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The aircraft was designed to comply with the US light-sport aircraft rules. It features astrut-bracedhigh-wing, a two-seats-in-tandem enclosed cockpit under abubble canopy, fixedtricycle landing gear and a single engine inpusher configuration.[1][2]

The aircraft is made with a welded steel tubing airframe. Its 29 ft (8.8 m) span wing employs a single strut per side. The standard engine for production examples was intended to be the 100 hp (75 kW)Rotax 912ULSfour-stroke powerplant. Entry to the cockpit is via anairstair door.[1][2]

The design is listed on theFederal Aviation Administration's list of accepted SLSAs, but as no longer in production.[6]

Operational history

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In March 2010 reviewer Dan Johnson reported on a test flight in the prototype:

the interior is spacious and comfortable, more so than many other LSAs; handling is predictable with no bad traits I could uncover; the airplane is well equipped and expects to have a price somewhere in the $110,000 range, though this decision is still being reviewed; visibility is enormous, with the pilot sitting about 4 feet in front of the wing; even the aft seat has good room, very good visibility, and full controls — it turns out my smoothest landings were from the rear.[5]

Specifications (A-16)

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Data from Bayerl[1][7]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 27 ft (8.2 m)
  • Wingspan: 28 ft 10 in (8.8 m)
  • Wing area: 130 sq ft (12 m2)
  • Empty weight: 739 lb (335 kg)
  • Gross weight: 1,232 lb (559 kg)
  • Fuel capacity: 80 litres (18 imp gal; 21 US gal)
  • Powerplant: 1 ×Rotax 912ULS four cylinder, liquid and air-cooled,four strokeaircraft engine, 101 hp (75 kW)
  • Propellers: 3-bladedPrince Aircraft composite

Performance

  • Maximum speed: 140 mph (220 km/h, 120 kn)
  • Cruise speed: 121 mph (195 km/h, 105 kn)
  • Stall speed: 45 mph (72 km/h, 39 kn)
  • Range: 450 mi (720 km, 390 nmi)
  • g limits: +4/-2
  • Rate of climb: 980 ft/min (5 m/s)
  • Wing loading: 9.55 lb/sq ft (46.6 kg/m2)

References

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  1. ^abcdBayerl, Robby; Martin Berkemeier; et al:World Directory of Leisure Aviation 2011-12, page 30. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^abcTacke, Willi; Marino Boric; et al:World Directory of Light Aviation 2015-16, page 32. Flying Pages Europe SARL, 2015.ISSN 1368-485X
  3. ^abJane's Information Group (2009)."Aviadesign A-16 Sport Falcon (United States), Aircraft - Fixed-wing - Civil". RetrievedMay 9, 2012.
  4. ^Experimental Aircraft Association (January 15, 2007)."Bigger and better: Sebring's third LSA expo a rousing success". RetrievedMay 9, 2012.
  5. ^abJohnson, Dan (March 18, 2010)."New tandem LSA headed to market".General Aviation News. RetrievedMay 9, 2012.
  6. ^Federal Aviation Administration (March 3, 2015)."SLSA Make/Model Directory". Archived fromthe original on May 16, 2013. RetrievedApril 22, 2015.
  7. ^Skytamer (2011)."Aviadesign A-16 Sport Falcon two-seat light sport aircraft". RetrievedMay 9, 2012.

External links

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Retrieved from "https://en.wikipedia.org/w/index.php?title=Aviadesign_A-16_Sport_Falcon&oldid=1321151691"
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