RED A03
| A03 | |
|---|---|
 | |
| RED A03 V-12 engine | |
| Type | Diesel aero-engine |
| National origin | Germany |
| Manufacturer | RED Aircraft GmbH |
| First run | 2009 |
|
| |
The RED A03 is a V12 four-stroke diesel aircraft engine designed and built by RED Aircraft GmbH of Adenau, Germany. The engine received type approval from the European Aviation Safety Agency in December 2014 for use in any CS/Part 23 aircraft in both normal and utility categories.[1]
Specifications
Data from EASA Type-Certificate Data Sheet[1]
General characteristics
- Type: four-stroke compression-ignition piston engine
- Displacement: 6134 cc
- Length: 1100 mm
- Width: 850 mm
- Height: 750 mm
- Dry weight: 363 kg fully-dressed, including Gearbox
Components
- Valvetrain: Gear-driven DOHC
- Turbocharger: 2 intercooled
- Fuel system: Common-rail
- Fuel type: jet-fuel, kerosene-type/diesel
- Oil system: Dry-sump, dual-circuit
- Cooling system: Liquid, dual circuit
Performance
- Power output: 368KW (500 HP)Take-off power ; 338KW (460 HP)MCP @ 1995 Propeller RPM
References
- 1 2 "E.150 - Type-Certificate Data Sheet - RED A03 series engines" (PDF). European Aviation Safety Agency. 19 December 2014.
External links
This article is issued from Wikipedia - version of the Thursday, February 04, 2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.