Energetics Phd ANNUAL REPORT 2016
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Type-Certificate Data Sheet
TCDS No.: E.150 Raikhlin aircraft Engine Developments GmbH Issue: 02 RED A03 Series Engines Date: 27 August 2018 TYPE-CERTIFICATE DATA SHEET E.150 for RED A03 series engines Type Certificate Holder Raikhlin aircraft Engine Developments GmbH Am alten Wehr 23 D-53518 Adenau Germany For Models: RED A03-003 RED A03-102 TE.CERT.00050-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 1 of 10 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: E.150 Raikhlin aircraft Engine Developments GmbH Issue: 02 RED A03 Series Engines Date: 27 August 2018 Intentionally left blank TE.CERT.00050-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 2 of 10 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: E.150 Raikhlin aircraft Engine Developments GmbH Issue: 02 RED A03 Series Engines Date: 27 August 2018 TABLE OFCONTENTS I. General ..................................................................................................................................... 4 1. Type/ Model ..................................................................................................................... 4 2. Type Certificate Holder ...................................................................................................... 4 3. Manufacturer ................................................................................................................... -
RED A03– 200 Series Key Operational Features
TYPE: RED A03 MODEL: RED A03– 200 Series Key Operational Features . Developed for very high altitude operation up to 15 km - FL500 . MCP rating - 460 SHP at FL250 . High altitude restart capability . Digital FADEC for unmanned operation Design Features . Operates with Jet Fuel . High safety level with independent circuits for each engine bank: air induction system fuel system cooling system The RED A03-200 series is a derivative of the proven RED A03-003 . FADEC single lever engine control engine model, developed for very high-altitude operation. Twin Stage turbocharged The RED A03 engine type is purpose-designed for aviation, to . Self-carrying structure for cantilever deliver the highest safety level combined with a compact and installation weight-optimized design. Dry-sump oil system The RED A03 type engine is a lightweight, all-aluminium, . Integrated engine oil and gearbox oil compression-ignition, internal combustion 12-cylinder engine, with tank. two six-cylinder banks capable of independent operation. Integrated engine oil and gearbox oil heat exchanger . Designed for lean maintenance ENGINE DESCRIPTION NUMBER OF CYL. + V-12 ARRANGEMENT Included Equipment FUEL TYPE JET FUEL DISPLACEMENT 6.1 L . FADEC & electric looms BORE X STROKE 86MM X 88MM . Engine starter VALVES PER CYLINDER . 4 . Engine and gearbox oil subsystem, TURBOCHARGER . 2 X TWIN STAGE incl. oil tank and heat exchanger FUEL SYSTEM . COMMON RAIL . Exhaust system and turbochargers ELECTRICAL SYSTEM . 2 X 28V 3.5KW ALTERNATOR . Optional: propeller governor, engine REDUCTION GEAR . 1:1.88 display, fuel boost pumps and . DRY MASS* 390 KG regulators & alternators DESIGN ASSURANCE LEVEL B FADEC CERTIFIED IN COMPLIANCE TO RTCA DO-254, DO-178B & DO-160G * Dependant on final configuration. -
Final Report - 18TTD009 Group Design Project
Final Report - 18TTD009 Group Design Project Department of Aeronautical and Automotive Engineering, Loughborough University, Leicestershire LE11 3T U, UK Project SkyRide – S270 DESIGN TEAM Harry Hay Group Leader and Propulsion Design Darshan Balasingam Ryan Beecroft Georgia Gregory Batteries and Systems Design Design and Modelling Risk and Reliability Ewa Mikinka Erandika Mohanathasan Simran Panesar Structural Design Business and Sales Stability and Systems Vandan Patel George Smith Edmund Tong Parachute and Landing Gear Aerodynamics Design Aircraft Performance Design i Executive Summary In this report, Project SkyRide design a 5 seat general aviation aircraft named the S270 (the SkyRide 270kW engine aircraft). The aim of the S270 is to increase regional mobility and reduce congestion of roads in the US by providing a low cost, fast alternative for commuters that frequently travel by car or public transport. This aircraft will make use of the existing infrastructure of small airports in the US, the majority of which are currently underutilised. This S270 follows the thin haul transport model (THT), serving as a scheduled service or on-demand “Air-Taxi”. The aircraft will carry out a standard 135 nmi mission in 45 minutes, with the capability of performing an extended sizing mission of 250 nmi in 2 hours. This is a significant time saving when compared to the equivalent car, train or bus journey. The cost of this standard 45-minute flight will be approximately $45 per person, which gives a total profit of 15%. In order to outperform and outsell competitors, the S270 aircraft will incorporate a number of advanced technologies to reduce operating costs and environmental impact. -
EASA-European Aviation Safety Agency
Standards Manager Web Standards List EASA-European Aviation Safety Agency Id Number Title Year Organization Page 1 AD 2018-0161 ATA 53 - Fuselage - Trimmable Horizontal Stabilizer Support Struts - Inspection 2018 EASA 2 PART-SPO AMC/GM to Part-SPO Amendment 10 - Annex V to Decision 2018/003/R 2018 EASA AMC & GM AMD 10 3 AD 2018- ATA 38 - Water/Waste - Forward Fuselage Shrouded Pipe T-Boxes And Clamps - Replacement 2018 EASA 0111R1 4 CS-25 AMD 22 CS-25 Amendment 22 - Change Information 2018 EASA CI 5 EC 2018/401 Commission Regulation (EU) 2018/401 Amending Regulation (EU) No 139/2014 As Regards The Classification Of 2018 EASA Runways 6 AD 2018-0247 ATA 34 Navigation Transponders Inspection / Modification 2018 EASA 7 AD 2018-0228 ATA 71 - Power Plant - Engine Air Inlet Cowl Inner Barrel Lower Panels - Inspection / Replacement 2018 EASA 8 AD 2018-0236- Emergency AD - ATA 32 Landing Gear Emergency Flotation Unit Inspection / Replacement Rotorcraft Flight Manual / 2018 EASA E Master Minimum Equipment List Temporary Revision 9 TOR Terms of Reference for rulemaking task - RAMP Deregulation - Issue 1 2018 EASA RMT.0721 10 TCDS BA.013 Type-Certificate Data Sheet - Cameron Balloons Ltd. - Manned Free Hot Air Balloons - Issue 18 2018 EASA 11 TCD SN Type-Certificate Data Sheet For Noise - Textron Aviation Inc. - Cessna 525 Series (Citation) - Issue 12 2018 EASA IM.A.078 12 TCDS Type-Certificate Data Sheet - Textron Aviation Inc. - Beechcraft 33, 35, 36 (Bonanza) - Issue 03 2018 EASA IM.A.279 13 TCDS Type-Certificate Data sheet - Lycoming Engines -
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. -
Red A03red A03
[Geben Sie Text ein] RED A03RED A03 MODEL:MODEL: RED A03RED– 003A03 –/ 003500 / SH 500P SHP RED aircraft GmbH MODEL:MODEL: RED A03RED– 00A035 –/ 005550 / SH 550P SHP RED aircraft GmbH RED aircraft is committed to deliver high span performance piston engines for special applications. Located in Adenau – Germany, RED offers a full range of engineering services required for engine and Annual Direct Engine Operation Costs powertrain development. All products are designed, tested and produced in-house, starting from a assuming average of 500 Hours per Year clean sheet of paper, by highly skilled and experienced specialists. RED A03 MRO COST FUEL COST Design RED A03 Utility & Agricultural Our products are carefully designed, starting from clean-sheet-of-paper, to meet all the demanding requirements and simultaneously deliver best-in-class value in terms of fuel economy, durability and PT6A Total Operating Cost. Our highly-experienced team of engineers and designers has acquired a vast wealth of know-how and lessons-learned which are now part of our built-in Intellectual Property. This allows us to approach R-1340 design challenges with creativity and innovation as well as fast turn-around, to provide a competitive edge to our customers. $- $20.000 $40.000 $60.000 $80.000 $100.000 $120.000 $140.000 Development and Testing Our state-of-the-art test cells provide the perfect test environment for the complete engine-, powertrains and engine sub module testing. Our engineers are skilled to perform the development and test activities, tailored to advanced engine requirements, optimization and durability of an engine throughout its development.