Technical

General Characteristics:

TYPE - Class one microlight

CREW - Single pilot

AIRCRAFT EMPTY WEIGHT - 200kg

MAX AIRCRAFT TAKE-OFF WEIGHT - 320kg

PAYLOAD AT FULL FUEL (PILOT + EQUIP WEIGHT) - 120kg

ENGINE - 200hp, 100hr TBO, low vibration

FUEL CAPACITY - 45 litre

Performance:

Range - 30km-50km

Endurance (flight time) - 30 minutes + Reserves

Maximum airspeed - 40kts (74km/h)

Cruise speed - 30kts (56km/h)

Ceiling - 3,000 ft AMSL

Recommended cruise height - 500ft and above per aviation authority regulations

Take-off wind limit - 15kts gusting +/- 5kts (28km/h +/- 9km/h)

Composite Airframe Specifications:

DUCTS - Carbon fibre, aramid fibre, honeycomb core, epoxy resin

FANS - Epoxy prepreg carbon fibre, aramid fibre, foam core

MAIN BEAM - High modulus carbon fibre, foam core

SPINE - Epoxy prepreg carbon fibre

FUEL TANK - Carbon fibre, Kevlar, fuel resistant epoxy resin

UNDERCARRIAGE - Carbon fibre, epoxy resin, aluminium alloy

ENGINE HEADS - Carbon fibre, high temp flame resistant vinylester resin

AIRBOXES - Carbon fibre, epoxy resin