The Zephyr was designed to comply with the F d ration A ronautique 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

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

Performance
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)

Airplane time state:
First owner
TTAF 1470 h
Motor Rotax 912 UL, 80 HP, TTE: 1730 h
ARC valid till 19.05.2026
MTOM 450 kg

Equipment:
GPS Garmin Map 296
Radio KRT 2 8,33 kHz plus Intercom
Transponder Trig mode S

Analog:
Altimeter
Variometer
Airspeed indicator
Compass
MGL FMS with digital:
Tachometer
Flight hour meter
Outside temperature gauge
Exhaust gas temperature gauge
Cylinder head temperature gauge
Oil temperature gauge
Oil pressure gauge
Fuel pressure gauge
Fuel tank quantity gauge
Stopwatch