DAR-21

VS (stall speed): 32 kts | 37 mph | 60 kph

VC (cruise speed): 86 kts | 99 mph | 160 kph

VNE (never exceed speed) : 113 kts | 130 mph | 210 kph

Climb ratio: 800 ft/min | 4 m/s
Glide ratio: 10

Takeoff distance over 50ft (15m) obstacle: 660 ft | 200 m
Landing distance over 50ft (15m) obstacle: 490 ft | 150 m

MEW (manufacturers empty weight): 230 kg | 507 lbs
MTOW (maximum takeoff weight): 450 kg | 992 lbs

Engine: Rotax 912 or Jabiru 2200
Fuel consumption: 10 / 12 l per hour

The DAR-21 by Aeroplanes DAR, is a two-seat aircraft, engine ranging from 60 to 120 HP. It has a fully enclosed cabin with tandem seats. The aircraft is flown from the front or back seat. There is only one door on the right side giving access both to seats and cargo sector.

All necessary instrumentation is mounted on the front panel, from where the aircraft is flown when flying solo.

The building materials of the DAR-21 airplane are aluminum alloys 1050, 2024, 3105 and 6061. The wing is rectangular with a single spar construction. The fuselage is made of rectangular tubing and steel struts with stressed aluminum skin. Cowling is made of composites. It has a steerable tail wheel. The fuselage holds a 30 liter fuel tank, but wings can be equipped with wing tanks.

Pricing:
 EXW SOF (Ex-work Sofia, Bulgaria)

Complete airplane:
 DAR-21 with ROTAX 912 31500EUR
 DAR-21 with Jabiru 2200 31450EUR

Kit Pricing EWR SOF:
 DAR-21 kit without engine, prop and instruments 20700EUR

For more information regarding the DAR-21, please visit Aeroplanes DAR Ltd. For dealers in your country, see related links below.