A03 Certificates

Our certificates New Zealand CAA DOA EASA.21J.433 and TCDS E.150 – Updated 2022-07 FAA TC The Russian Federation CAA Produced in an EN9100 certified environment Made in Germany

RED FADEC

Full authority digital engine controlFADEC by RED Aircraft Developed and certified according to DO-254 DAL B. The software   Voll redundanter Aufbau mit zwei identischen Lanes IBIT und CBIT Überwachung mit automatischem Lanewechsel im Fehlerfall Betriebsdaten- und Fehleraufzeichnung CAN-Bus Interface zur Fehleranalyse und Auswertung der Betriebsdaten Serielle Schnittstelle zum Cockpit Optionale bidirektionale Schnittstelle Intelligenter Watch Dog …

RED A03 Technical Data

Core
details

 

No. Of cyl
and arrangement

V12 – 80°

Fuel type

Jet A1, kerosene type fuels acc. To
ASTM D1655, Def Stan 91-91 and GOST 10227 up to a maximum ignition delay time of 8.06 ms/minimum derived cetane number of 27.9 (determined according EN 15195/ASTM D6890)

Power A03-x03

500 hp – 378 kW/4,000 rpm

Power A03-x05

550 hp – 405 kW/4,000 rpm

Power A03-Non aviation use (project
state)

600 HP – 441 kW

Displacement

372 CUI – 6.1 l

Bore & stroke

3.38″x3.46″ – 86×88 mm

Valves per cylinder

4

Camshaft system

gear driven dual overhead camshaft

Turbocharger

Single or 2-stage system

Fuel system

Common rail high preasure system 1,600 bar – 23,206 psi

Electrical system

2x28V 3.5 kW alternator

Reduction gear

1:1.88

Dry mass w/o gearbox

290 kg – 640 lbs

Dry mass with normal/utility
gearbox

363 kg – 800 lbs

Dry mass with aerobatic gearbox

357 kg – 787 lbs

Fuel Flow take-off power

85 KG/H – 187 lbs/h

Fuel Flow MCP

77 KG/H – 169 lbs/h

Fuel Flow 400 hp

65 KG/H – 143 lbs/h

Fuel Flow 300 hp

47 KG/H – 103 lbs/h

Engine control system

FADEC, EECU, EECS, sensors, Design Assurance Level B cert. ompliant RTCA DO-254,
DO-178B, DO-160G