Shark 600 UL/EXP

Artikkelnr.: SHRK600

A high-performance European UL with retractable gear, smaller wing and variable-pitch propeller. Shark UL is designed, tested and certified for a maximum take-off weight of 600 kg. Available with 100-154HP engines. Contact for pricing.

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FAI declares 4 ratified world speed records of Shark

Design features

Designed according to European UL and US Light Sport Aircraft criteria. Composite low-wing design with classic tail and tandem seating. Now also available as Experimental under our factory builder assist program.


Glass-fibre and carbonfibre/epoxy airframe, with PVC foam and aramid honeycomb core in sandwich panels. Monocoque fuselage with integral fin has integrated arm rests, seat backs, floors and instrument panels. Composite wing with carbon-fibre main spar and an auxiliary spar carrying flap levers and aileron hinges has 60 % of the trailing edge occupied by powerful single-slotted flaps. Wings and horizontal tail can be quickly detached for transportation or storage.

Flying controls

Mechanically actuated control surfaces with electric trim tab on the elevator and electrically actuated flaps. HOTAS - Hand On Throttle AND Side-stick


Shark UL has tricycle type retractable undercarriage with steerable 13x4" nose wheel and 14x4” main wheels with hydraulic disc brakes. Beringer wheel and brakes as stadard.


The Shark can be delivered with either the Rotax 912ULS (100HP) or the EP)!¤Ti (126HP Turbo, Fuel Injection and Intercooler).

Fixed or Variable-pitch composite propeller.

Fuel tanks - Wet Wings, capacity 100-150 litres.


A completely upholstered two-seat tandem cockpit with adjustable seats has full dual controls – with sidesticks on the right and throttles and flap levers on the left panels. Elevator trim tab is controlled by electric switch on the sidestick. Instrument panels with standard EFIS/EMS displays for both pilots are complete with the classic fuel gauges, transceiver, transponder and GPS and secondary airspeed indicators and altimeters. The single-piece cockpit canopy opens to starboard and is supported by gas struts. Baggage space aft of seats.


Available with Garmin and Dynon EFIS systems, or analogue gauges with FlyBox PFD.


Technical specifications
 Wing span  7,9 m
 Length  6,85 m
 Height  2,5 m
 Wing area  9,5 m²
 Engine  Rotax 912 S - 75 kW (100 HP)
 Empty weight  295 kg, (325 kg full options)
 Max. take-off weight  480 / 600 kg
 Max. permissible speed VNE  333 km/h
 Max. cruising speed VH  300 km/h
 Optimum cruising speed  250-270 km/h
 Stall speed, clean  80 km/h
 Stall speed, full flaps  64 km/h
 Max. climb rate at the MTOW  7,2 m/s
 Fuel capacity  100l
 Fuel consumption (economy flight)  15 l/h
 Maximum load factor  +4/-2
 Maximum ultimate  +6/-3