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RED A03 – 000 Series Base Configuration (500 HP) – RED Aircraft GmbH
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RED A03 – 000 Series Base Configuration (500 HP)

  • RED A03 Design View Base Side View
  • RED A03 Design View Base

Base Configuration (500 HP)

RED A03– 000

The RED A03 engine is purpose-designed for aviation, to deliver the highest safety level combined with a compact and weight-optimized design.

The RED A03 type engine is a lightweight, all-aluminium, compression-ignition, internal combustion 12-cylinder engine, with two six-cylinder banks capable of independent operation.

Application Fields

All types of General Aviation (GA) aircraft, as

  • Commuter
  • Utility
  • Agricultural & more

Key Design Features

  • Operates with Jet Fuel
  • High safety level with independent circuits for each engine bank:
    • air induction system
    • fuel system
    • cooling system
  • FADEC single lever engine control
  • Turbocharged
  • Self-carrying structure for cantilever installation
  • Dry-sump oil system
  • Integrated engine oil and gearbox oil tank.
  • Integrated engine oil and gearbox oil heat exchanger
  • Designed for lean maintenance

Certification

Certified in compliance to EASA CS-E / TYPE-CERTIFICATE-DATA-SHEET No.: E.150.

Included Equipment

  • FADEC & electric looms
  • Engine starter
  • Engine and gearbox oil subsystem, incl. oil tank and heat exchanger
  • Exhaust system and turbochargers
  • Optional: propeller governor, engine display, fuel supply system,
    alternators & more

 
 
ENGINE DESCRIPTION
NUMBER OF CYL. +
ARRANGEMENT		 V-12
FUEL TYPE JET FUEL
DISPLACEMENT 4
BORE X STROKE 3.38” X 3.46”
VALVES PER CYLINDER 4
TURBOCHARGER SINGLE STAGE
FUEL SYSTEM COMMON RAIL
ELECTRICAL SYSTEM 2 X 28V 3.5KW ALTERNATOR
REDUCTION GEAR 1:1.88
DRY MASS* 800 LBS
FADEC DESIGN ASSURANCE LEVEL B
CERTIFIED IN COMPLIANCE TO RTCA
DO-254, DO-178B & DO-160G
DIMENSIONS 33.46 x 29.53 x 43.86 inch ( Width x Height x Length )

*According to type design configuration.

PERFORMANCE & RATINGS

TAKEOFF POWER 500 SHP(2)
TAKEOFF PROPELLER SPEED 2127 RPM
MAXIMUM CONTINUOUS
POWER		 460 SHP
MAXIMUM CONTINUOUS SPEED 1995 RPM
CRITICAL ALTITUDE 6562 FT
BSFC (BEST) 0.349 LBS/H/SHP
FUEL FLOW:  
AT TAKEOFF
AT MCP
AT 400 HP
AT 300 HP		 187 LBS/H
169 LBS/H
143 LBS/H
103 LBS/H