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DA50 RG
Preliminary Technical Specifications

Power Plant

Engine

Continental CD-300 turbocharged, FADEC controlled jet fuel engine with 300 hp TOP / 270 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
Stall speed, landing configuration106 km/h CAS57 kts CAS
Best rate of climb5.3 m/s1,050 ft/min
Max. range incl. 30 min. reserve1,389 km750 nm
Consumption at max range34.1 lt/hr9 US gal/hr
Take-off distance (ISA SL, MTOM, ground roll / 50 ft obstacle)440 m / 740 m1,444 ft / 2,427 ft
Landing distance (ISA SL, MTOM, ground roll / 50 ft obstacle)340 m / 640 m1,115 ft / 2,100 ft
Max. operating altitude6,096 m20,000 ft

Dimensions

Mass and Loading

Seats

55

Empty mass

1,440 kg3,175 lbs

Useful load

559 kg1,232 lbs

Max. take off mass

1,999 kg4,407 lbs

Fuel capacity

189 lt50 US gal

Specifications apply to standard equipped aircraft (DA50 RG 5-seat 300 hp prototype version June 2020, average occupation, short trip loading, well serviced aircraft condition), if not otherwise stated. The above data are approximately specifications and may change without notice.