Experience a Virtual Demo Flight
The DA50 RG has a sleek carbon composite airframe paired with a geared, liquid-cooled, turbo-charged and jet-A1-fueled engine. These factors combined offer the ultimate experience in handling, stability, and control.
Overview
Tech Specs
12 gal/h
Consumption at max range (34.1 l/h)
Continental CD-300 turbocharged, FADEC controlled jet fuel engine with 300 hp TOP / 270 hp MCP
181 kts
Max. speed (ISA, 16,000 ft, 1,700 kg, MCP)
57 kts stall speed, landing configuration
20,000 ft
Max. operating altitude (6,096 m)
1,050 ft/min max. rate of climb (MSL)
750 nm
Max. range (incl. auxiliary tank)
9 US gal/hr fuel consumption at max range
5 Seats
Comfortable access for all on board is assured through the two forward gull wing doors and the huge rear door that provides access to all rear seats.
1,232 lbs
Useful load (559 kg)
Your baggage is safely stowed in the rear of the cabin, offering you maximum loading capability for any kind of mission.
Design
The DA50 RG spoils pilots and passengers alike: You will love the sound the landing gear makes as the wheels retract, you will utterly enjoy the moment the aircraft accelerates and appreciate the aerodynamic efficiency.
And yes, you and your plane will look really cool while you and your passengers enjoy everything the extra-large cabin is offering you – just like the cabin of our marvelous twin-engine DA62: generous front seats with adjustable backrests, a 60/40 split folding three seat second row bench, easy access through the large gull wing doors and cargo door and exceptional leg, shoulder and head room. And your baggage is safely stowed in the rear of the cabin, offering you maximum loading capability for any kind of mission.
Safety
Diamond‘s industry-leading safety record is the result of our commitment to protecting you and your passengers with a long list of active and passive safety features. Active safety features help to avoid accidents in the first place, the first and most important line of defense. Passive safety features are designed to minimize the probability and degree of injury, just in case the unexpected happens.
The DA50 RG offers the ultimate in handling, stability and control, ease of operation as well as structural and system redundancies, all coupled with a high degree of crashworthiness. The sleek all carbon composite airframe incorporates advanced aerodynamics with the latest in passive safety technology for high performance, great efficiency and superior occupant protection.
Propulsion and Avionics
The DA50 RG is powered by the 300 hp Continental Aerospace Technologies CD-300. The CD-300 is a geared, liquid-cooled, turbo-charged and jet-A1-fueled engine controlled by two redundant full FADEC. Pilot workload is lightened using a single lever power control that adjusts thrust and propeller RPM’s automatically. The extra benefits of operating a jet fuel powered aircraft are low emissions, low fuel consumption and global availability.
The 3 blade MT hydraulic variable pitch propeller features advanced blade geometry with state of the art aerodynamic airfoils for efficient performance, smoothness and low noise. The blades are built in natural composite design which leads to an exceptional vibration damping behavior and reduced weight.
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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 TAS | 181 kts TAS |
|---|---|---|
| Stall speed, landing configuration | 106 km/h CAS | 57 kts CAS |
| Best rate of climb | 5.3 m/s | 1,050 ft/min |
| Max. range incl. 30 min. reserve | 1,389 km | 750 nm |
| Consumption at max range | 34.1 lt/hr | 9 US gal/hr |
| Take-off distance (ISA SL, MTOM, ground roll / 50 ft obstacle) | 381 m / 740 m | 1,250 ft / 2,427 ft |
| Landing distance (ISA SL, MTOM, ground roll / 50 ft obstacle) | 344 m / 678 m | 1,129 ft / 2,224 ft |
| Max. operating altitude | 6,096 m | 20,000 ft |
Dimensions
Mass and Loading
|
Seats |
5 | 5 |
|---|---|---|
|
Empty weight |
1,440 kg | 3,175 lbs |
|
Useful load |
559 kg | 1,232 lbs |
|
Max. take off mass |
1,999 kg | 4,407 lbs |
|
Fuel capacity |
195 lt | 51,5 US gal |
Interested in the DA50 RG?
Reach out to us to see if this plane is a good fit for your mission.