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ECi O-320

January 01, 1970

The ECi O-320 is part of a family of normally aspirated, air-cooled, four-cylinder, direct-drive engines developed for certified and experimental aircraft. Its cylinders are arranged in horizontally opposed configuration and a displacement of 320 cubic inches (5.24 L). It is based on the Lycoming O-320 engine with ECi cylinder assemblies.[1][2]

O-320
Type Piston aero-engine
Manufacturer Engine Components Inc.
Major applications Vans RV-6

Design and development edit

ECi developed engine kits starting in 1995.[3]

Variants edit

O-320 series edit

ECi O-320
154 hp (115 kW) at 2700 rpm, Minimum fuel grade 100/100LL avgas, compression ratio 7.0:1. Certified Applications
ECi OX-320
154 hp (115 kW) at 2700 rpm, Minimum fuel grade 100/100LL avgas, compression ratio 7.0:1. Experimental Variant
ECi IOX-320
156 hp (116 kW) at 2700 rpm, Minimum fuel grade 100/100LL avgas, compression ratio 7.0:1. Fuel Injected Experimental

Applications edit

Specifications (ECi O-320) edit

Data from ECi

General characteristics

Components

  • Valvetrain: Two overhead valves per cylinder
  • Fuel system: MA4-5 Carb
  • Fuel type: minimum grade of 100/100LLavgas
  • Oil system: Wet sump
  • Cooling system: Air-cooled

Performance

See also edit

References edit

  1. ^ . Archived from the original on 16 April 2014. Retrieved 15 April 2014.
  2. ^ "ECi AD affects 13,000 Titan cylinders". Retrieved 15 April 2014.
  3. ^ "ECi launches engine assembly program". General Aviition News. 22 January 2013.

External links edit

  This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.

January 01, 1970
part, family, normally, aspirated, cooled, four, cylinder, direct, drive, engines, developed, certified, experimental, aircraft, cylinders, arranged, horizontally, opposed, configuration, displacement, cubic, inches, based, lycoming, engine, with, cylinder, as. The ECi O 320 is part of a family of normally aspirated air cooled four cylinder direct drive engines developed for certified and experimental aircraft Its cylinders are arranged in horizontally opposed configuration and a displacement of 320 cubic inches 5 24 L It is based on the Lycoming O 320 engine with ECi cylinder assemblies 1 2 O 320 Type Piston aero engine Manufacturer Engine Components Inc Major applications Vans RV 6 Contents 1 Design and development 2 Variants 2 1 O 320 series 3 Applications 4 Specifications ECi O 320 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 7 External linksDesign and development editECi developed engine kits starting in 1995 3 Variants editO 320 series edit ECi O 320 154 hp 115 kW at 2700 rpm Minimum fuel grade 100 100LL avgas compression ratio 7 0 1 Certified Applications ECi OX 320 154 hp 115 kW at 2700 rpm Minimum fuel grade 100 100LL avgas compression ratio 7 0 1 Experimental Variant ECi IOX 320 156 hp 116 kW at 2700 rpm Minimum fuel grade 100 100LL avgas compression ratio 7 0 1 Fuel Injected ExperimentalApplications editAviat Husky A 1B 160 Avid Flyer Aero Commander 100 Alpha 160A American Champion Citabria Australian Aircraft Kits Hornet STOL Australian Lightwing SP 4000 Speed Aviation Industries of Iran AVA 202 Beechcraft Musketeer Bellanca Decathlon Bushcaddy L 160 Canadian Home Rotors Safari Cessna 172 Custom Flight North Star Christavia Mk IV Dakota Cub Super 18 EM 11 Orka Eaves Cougar 1 Explorer Ellipse Falconar F12A Cruiser Fly Fan Shark Glasair GlaStar Grumman American AA 5 Gulfstream American GA 7 Cougar Hatz CB 1 Hatz Classic Lambert Mission 212 MBB Bo 209 Mooney M20 Murphy Elite Mustang Aeronautics Mustang II Osprey Osprey 2 Partenavia P66B Oscar 150 Pena Dahu PIK 19 Piper Aztec Piper Apache Piper PA 40 Arapaho Piper Twin Comanche Piper Cherokee Piper Tripacer Preceptor STOL King PZL 110 Koliber Quikkit Glass Goose Rihn DR 107 One Design Robin DR400 Robinson R22 Rutan Long EZ Sands Fokker Dr 1 Triplane SGP M 222 Flamingo Socata TB9 Tampico Symphony SA 160 Tapanee Levitation 2 Thorp T 18 Piper PA 18 150 Super Cub Van s Aircraft RV 3 Van s Aircraft RV 4 Van s Aircraft RV 6 Van s Aircraft RV 8 Van s Aircraft RV 9 Varga Kachina Velocity V Twin Vulcanair P 68C Wassmer WA 52 Wickham B Wittman TailwindSpecifications ECi O 320 editData from ECi General characteristics Type Four cylinder air cooled horizontally opposed engine Bore 5 125 in 130 18 mm Stroke 3 875 in 98 43 mm Displacement 319 7 cu in 5 24 L Length 29 07 Width 32 27 Height 24 8 Dry weight 244 lb 111 kg Components Valvetrain Two overhead valves per cylinder Fuel system MA4 5 Carb Fuel type minimum grade of 100 100LLavgas Oil system Wet sump Cooling system Air cooled Performance Power output 154 hp 115 kW Compression ratio 7 1See also editList of aircraft enginesReferences edit Proposed AD Demands Removal of Thousands of ECI Titan Cylinders Archived from the original on 16 April 2014 Retrieved 15 April 2014 ECi AD affects 13 000 Titan cylinders Retrieved 15 April 2014 ECi launches engine assembly program General Aviition News 22 January 2013 External links edit nbsp This aircraft engine article is missing some or all of its specifications If you have a source you can help Wikipedia by adding them Retrieved from https en wikipedia org w index php title ECi O 320 amp oldid 1174498948, wikipedia, wiki, book, books, library,

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