TYPE: RED A03 MODEL: RED A03–100 Series Key Operational Features Certified For

TYPE: RED A03 MODEL: RED A03–100 Series Key Operational Features Certified for . +9g positive load factor . -7g negative load factor . Inverted flight operation . Aerobatic maneuvers

Application Fields . Advanced Trainer Aircraft

. Aerobatic

Key Design Features . Operates with Jet Fuel

. High safety level with independent The 100 series engine model is designed for advanced trainer and circuits for each engine bank: aerobatic aircrafts. The engine is approved for high positive-&  air induction system negative g-load factors, high angular rotation velocities and

inverted flight.  fuel system  cooling system The RED A03 engine is purpose-designed for aviation, to deliver the . FADEC single lever engine control highest safety level combined with a compact and weight-optimized . Turbocharged design. . Self-carrying structure for cantilever The RED A03 type engine is a lightweight, all-aluminium, installation compression-ignition, internal combustion 12-cylinder engine, with . Dry-sump oil system two six-cylinder banks capable of independent operation. . Integrated gearbox oil tank. ENGINE DESCRIPTION . Integrated engine oil and gearbox oil NUMBER OF CYL. + V-12 heat exchanger ARRANGEMENT . Designed for lean maintenance FUEL TYPE JET FUEL DISPLACEMENT 6.1 L BORE X STROKE 86MM X 88MM Certification

VALVES PER CYLINDER . 4 Certified in compliance to EASA CS-E / TURBOCHARGER . SINGLE STAGE TYPE-CERTIFICATE-DATA-SHEET No.: FUEL SYSTEM . COMMON RAIL E.150.

ELECTRICAL SYSTEM . 28V 3.5KW ALTERNATOR Included Equipment REDUCTION GEAR . 1:1.88 DRY MASS* . 357 KG . FADEC & electric looms DESIGN ASSURANCE LEVEL B . Engine starter FADEC CERTIFIED IN COMPLIANCE TO RTCA . Exhaust system and turbochargers DO-254, DO-178B & DO-160G . Optional: aerobatic oil tank, propeller * According to type design configuration. governor, engine display, fuel boost pumps and regulators & alternators

TYPE: RED A03 MODEL: RED A03– 100 Series

DIMENSIONS WIDTH 850 MM HEIGHT 712 MM LENGTH 1114 MM

*All dimension in mm

PERFORMANCE & RATINGS 600 TAKEOFF POWER 500 SHP(2)

500 TAKEOFF PROPELLER SPEED 2127 RPM

(1) MAXIMUM CONTINUOUS POWER 460 SHP 400 MAXIMUM CONTINUOUS SPEED 1995 RPM

300 CRITICAL ALTITUDE 2000 M

BSFC (BEST) 215 G/KWH 200

. FUEL FLOW: Shaft Power [SHP] Power Shaft AT TAKEOFF 85 KG/H 100 AT MCP 77 KG/H 0 AT 400 HP 65 KG/H AT 300 HP 47 KG/H 0 2000 4000 6000 8000 MAX POSITIVE G LOAD FACTOR +9G Altitude [m] MAX NEGATIVE G LOAD FACTOR -7G

ROLL = NO LIMIT (1) Enhanced altitude performance available on request (dotted line). MAX ANGULAR SPEEDS YAW = 3.5 RAD/S (2) 550 SHP Takeoff available on request. PITCH = 2.0 RAD/S

RED aircraft GmbH Am alten Wehr 23 D-53518 Adenau +49 2691/93776-10

[email protected] www.red-aircraft.com