This article is about the 1940 carbureted aircraft engine. For the 2008 fuel-injected aircraft engine, see Lycoming IO-233.
The Lycoming O-233 is a four-cylinder, air-cooled, horizontally opposed piston aircraft engine that was built by Lycoming Engines between 1940 and 1944.[1]
Lycoming applied for certification of the O-233 on 13 June 1940, with certification to CAR 13 (amended to 31 May 1938) granted on 16 August 1940. The O-233 had its type certificate cancelled on 25 February 1944 at serial number 106.[1]
The FAA type certificate notes:
No engines of these models manufactured after the date or with serial numbers above those listed below are eligible for use in certificated aircraft. (The early production engines may still be used in certificated aircraft or installed under a supplemental type certificate). Detail specifications for these engines have been deleted from this data sheet.[1]
Variantsedit
O-233-A1
Sole variant, type certification cancelled 25 February 1944[1]
Wikimedia Commons has media related to Lycoming O-233.
Textron Lycoming - Manufacturer's home page
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February 14, 2024
lycoming, this, article, about, 1940, carbureted, aircraft, engine, 2008, fuel, injected, aircraft, engine, lycoming, four, cylinder, cooled, horizontally, opposed, piston, aircraft, engine, that, built, lycoming, engines, between, 1940, 1944, 233type, piston,. This article is about the 1940 carbureted aircraft engine For the 2008 fuel injected aircraft engine see Lycoming IO 233 The Lycoming O 233 is a four cylinder air cooled horizontally opposed piston aircraft engine that was built by Lycoming Engines between 1940 and 1944 1 O 233Type Piston aero engineNational origin United StatesManufacturer Lycoming EnginesFirst run 1940Produced 1940 1944Number built 106Developed from Lycoming O 145Developed into Lycoming O 235 Contents 1 Development 2 Variants 3 Specifications O 233 A1 3 1 General characteristics 3 2 Components 4 See also 5 References 6 External linksDevelopment editLycoming applied for certification of the O 233 on 13 June 1940 with certification to CAR 13 amended to 31 May 1938 granted on 16 August 1940 The O 233 had its type certificate cancelled on 25 February 1944 at serial number 106 1 The FAA type certificate notes No engines of these models manufactured after the date or with serial numbers above those listed below are eligible for use in certificated aircraft The early production engines may still be used in certificated aircraft or installed under a supplemental type certificate Detail specifications for these engines have been deleted from this data sheet 1 Variants editO 233 A1 Sole variant type certification cancelled 25 February 1944 1 Specifications O 233 A1 editData from TCDS 1 General characteristics Type Four cylinder horizontally opposed piston engineComponents Cooling system Air cooledSee also editRelated lists List of aircraft enginesReferences edit a b c d e Federal Aviation Administration December 2003 TYPE CERTIFICATE DATA SHEET NO E 223 PDF Retrieved 2008 11 30 External links edit nbsp Wikimedia Commons has media related to Lycoming O 233 Textron Lycoming Manufacturer s home page 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 Lycoming O 233 amp oldid 1056214761, wikipedia, wiki, book, books, library,
