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Blue DA50 RG with orange and silver highlights.

DA50 RG
Technical Specifications

Power Plant

Engine

Continental CD-300 turbocharged, FADEC controlled jet fuel engine with 300 hp TOP / 272 hp MCP

Propeller

MT propeller MTV-12-D/210-56

Fuel grades

JET-A1

Performance

Max. speed (ISA, 16,000 ft, 1,700 kg, MCP)335 km/h TAS181 kts TAS
Cruise speed at 82% (14,000 ft)319 km/h TAS172 kts TAS
Stall speed, landing configuration107 km/h CAS58 kts CAS
Best rate of climb3.96 m/s780 ft/min
Max. range (FL180, 45% PWR) no climb, no reserves1,520 km820 nm
Max. range incl. 30 min. reserve no climb, no reserves1,396 km754 nm
Consumption at max. range (FL180, 45% PWR)30.2 lt/hr8 US gal/hr
Consumption (12,000 ft, 60% PWR)38.9 lt/hr10.3 US gal/hr
Take-off performance (MSL, ground roll / take-off obstacle)407 m / 734 m1,335 ft / 2,408 ft
Landing performance (MSL, ground roll / landing distance)344 m / 678 m1,129 ft / 2,224 ft
Max. operating altitude6,096 m20,000 ft

Dimensions

DA50 RG technical drawing with dimensions. Wingspan 13.41 m/44 ft. Height 2.95 m/9 ft 8 in, length 9.24/30 ft 4 in.

Mass and Loading

Seats

55
Empty weight without options1,450 kg3,197 lbs
Maximum useful load549 kg1,210 lbs

Max. take off mass

1,999 kg4,407 lbs
Fuel capacity total (usable fuel)185 lt / 148 kg49 US gal / 326 lbs

Specifications apply to standard equipped aircraft, typical configuration, average occupation, short trip loading, well serviced aircraft condition, if not otherwise stated. The above data are approximately specifications and may change without notice.