Aviadesign A-16 Sport Falcon
# Aviadesign A-16 Sport Falcon

The Aviadesign A-16 Sport Falcon is an American light-sport aircraft that was designed by Aviadesign, a certified aircraft modification company based in Camarillo, California. The A-16 was announced at Sun 'n Fun April 2006 and introduced at the LSA Expo held in Sebring, Florida in 2007. The aircraft was to be supplied as a complete ready-to-fly-aircraft.

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.

## Design and development

The aircraft was designed to comply with the US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-tandem enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in pusher configuration.

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 912ULS four-stroke powerplant. Entry to the cockpit is via an airstair door.

The design is listed on the Federal Aviation Administration's list of accepted SLSAs, but as no longer in production.

## Operational history

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.

## Specifications (A-16)

Data from Bayerl

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 $m^2)$
* 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 stroke aircraft engine, 101 hp (75 kW)
* Propellers: 3-bladed Prince 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 $kg/m^2)$
