DAR-23 AKTSENT

English name: Accent

TYPE: Side-by-side ultralight.

PROGRAMME: Prototype (LZ-DAS) flying by 2002; joined by second aircraft (LZ-DAF) early 2003.

DESIGN FEATURES: Cabin pod underslung from boom carrying uncowled engine, wings and empennage. Wings braced to cabin; cabin braced to boom ahead of windscreen.

FLYING CONTROLS: Conventional and manual. Plain flaps. Flight-adjustable elevator tab. No aerodynamic balances. Ailerons, elevator and flaps actuated by pushrods; rudder by cables.

STRUCTURE: Metal boom and composites cabin. Metal wings fabric-covered.

LANDING GEAR: Tricycle type; fixed. Tubular steel legs. Mainwheels Azusa 6.00. Cable mainwheel brakes.

POWER PLANT: One 34.0 kW (45.6 hp) Rotax 503 UL two-stroke driving a Powerfin two-blade, composites propeller via 2.58:1 reduction gear. Fuel capacity 30 litres (7.9 US gallons; 6.6 Imp gallons).

ACCOMMODATION: Optional cover for cockpit.

 

Index Facebook Search Index Facebook Search