2009 Atec 122 Zephyr

Specifications

Crew: one
Capacity: one passenger
Wingspan: 9.6 m (31 ft 6 in)
Wing area: 10.07 m2 (108.4 sq ft)
Airfoil: UA-2
Empty weight: 275 kg (606 lb)
Gross weight: 472.5 kg (1,042 lb)
Fuel capacity: 60 litres (13 imp gal; 16 US gal)
Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke, 80 hp
Maximum speed: 265 km/h (165 mph, 143 kn)
Cruise speed: 215 km/h (134 mph, 116 kn)
Stall speed: 65 km/h (40 mph, 35 kn)
Rate of climb: 6.5 m/s (1,280 ft/min)
Wing loading: 46.92 kg/m2 (9.61 lb/sq ft)

The Zephyr was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear, a T-tail and a single engine in tractor configuration
The aircraft's fuselage is made from carbon composites with wooden bulkheads. The semi-tapered 9.6 m (31.5 ft) span wing is made from plywood with composite spars and leading edges and employs a UA-2 airfoil. The wing is covered with doped aircraft fabric.
General characteristics
Performance
Airplane time state
First owner
TTAF 1470 h
ARC valid till 19.05.2026
MTOM 450 kg

Atec 2004 Atec 122 Zephyr €37,500 ≈ $41,974 2004 · 2,344 h · Sweden Private seller

Atec 2002 Atec 122 Zephyr €45,000 ≈ $50,368 2002 · 730 h · Germany Private seller

Atec 2008 Atec 122 Zephyr €49,650 ≈ $55,573 2008 · 5,101 h Private seller