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Textron Lycoming O-235-C User Manual

Textron Lycoming O-235-C
91 pages
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OPERATOR’SMANUAL
REVISION
REVISIONNO. PUBLICATION PUBLICATIONNO. PUBLICATIONDATE
6029791 O235,O290SERIES 602979 January2007
Thepage(s)inthisrevisionreplace,addto,ordeletecurrentpagesintheoperator’smanual.
PREVIOUS REVISION CURRENTREVIS ION
None
September 2008
35,36, Addspage36A/B
©2008byLycoming“AllRightsReserved”
LycomingEngines,adivisionofAVCOCorporation,awhollyownedsubsidiaryofTextronInc.

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Textron Lycoming O-235-C Specifications

General IconGeneral
Bore4.375 in (111.1 mm)
Stroke3.875 in (98.4 mm)
Compression Ratio8.5:1
Fuel TypeAvgas 100LL
Fuel systemCarburetor
Cooling systemAir-cooled
TypeFour-cylinder, horizontally opposed
Displacement3.85 L (235 cu in)

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