Lycoming O-235-L2C: Cessna 152 Power and Installation Limits

The Lycoming O-235-L2C is recorded at 110 hp and 2,550 RPM in the Cessna 152 installation. Its engine certification/manufacturer rating is separately recorded as 118 hp at 2,800 RPM. Those are different operating contexts, not competing descriptions from which to choose the larger number. The aircraft limit governs the aircraft installation; the engine reference explains the underlying engine.

Left side of a Cessna 152 engine exposed in a maintenance hangar
A Cessna 152 engine photographed from the pilot’s side during overhaul work. This is an installation view, not a statement of serviceability. Photo: Brian Burger from Victoria, Canada · Wikimedia Commons · CC BY 2.0. Resized, WebP.

Engine identity and aircraft rating

The L2C is a 233.3-cubic-inch, four-cylinder, horizontally opposed, carbureted engine in the O-235 family. It is air-cooled, normally aspirated and direct-drive. Its recorded compression ratio is 8.5:1, with engine certificate E-223. These characteristics distinguish it from the O-200-A used in the principal 150 installations, but they do not establish an approved L2C conversion for a 150.

The table deliberately places the aircraft and engine ratings beside one another. Increasing the aircraft's permitted RPM cannot be inferred from an engine-family specification. Likewise, an engine advertisement using 118 hp does not establish the performance of a 152 with its aircraft installation limit. For practical comparisons, use the 150 versus 152 guide and the applicable aircraft handbook conditions.

Engine characteristics and aircraft rating
EngineCharacteristicValueSourceSpecification Source
O-235-L2CManufacturerLycoming Engines[1][2]
O-235-L2CTCE-223[1][2]
O-235-L2CAircraft installed hp110[1][2]
O-235-L2CAircraft max rpm2550[1][2]
O-235-L2CEngine TC / manufacturer rated hp118[1][2]
O-235-L2CEngine rated rpm2800[1][2]
O-235-L2CDisplacement cu in233.3[1][2]
O-235-L2CCompression8.5:1[1][2]
O-235-L2CConfiguration4-cylinder horizontally opposed, overhead-valve, spark ignition, four-stroke[1][2]
O-235-L2CInductionCarbureted[1][2]
O-235-L2CDriveDirect[1][2]
O-235-L2CFuel100/100LL aviation gasoline[1][2]
Lower engine installation and nosewheel strut of a Cessna 152
The lower engine area of a Cessna 152 with the cowling removed, including the nosewheel strut assembly. Photo: Brian Burger from Victoria, Canada · Wikimedia Commons · CC BY 2.0. Resized, WebP.

Early production, standard models and Aerobats

The recorded L2C installation groups include U.S. 152 and A152 aircraft and Reims F152 and FA152 aircraft. The model and origin columns preserve those branches. Aerobat identity does not require inventing a different engine rating, but the same engine does not make the aircraft's category, loading envelope or manoeuvre limits interchangeable. The A152 reference and FA152 reference describe their own evidence boundaries.

Special serial assignments also matter. A1500433 appears in the 152-family research as an A152 exception; its prefix is not authority to treat it as an ordinary A150 engine application. The 681/A15200681 notation likewise needs the identity explanation rather than two physical-aircraft assumptions. Resolve those cases in the Cessna 152 serial guide before interpreting the installation table.

Recorded installation groups: eligibility is not installed-equipment proof (22 records)
Recorded installation groups: eligibility is not installed-equipment proof
OriginModel YearAircraft ModelFactory EngineInstalled hpRPM LimitFirst Serial in GroupLast Serial in GroupApplicability BasisAircraft Source
France1978F152O-235-L2C1102550F15201429F15201528A13EU 1978-1982 model production[1]
France1978FA152O-235-L2C1102550FA1520337FA1520347A13EU 1978-1982 model production[1]
France1979F152O-235-L2C1102550F15201529F15201673A13EU 1978-1982 model production[1]
France1979FA152O-235-L2C1102550FA1520348FA1520357A13EU 1978-1982 model production[1]
France1980F152O-235-L2C1102550F15201674F15201808A13EU 1978-1982 model production[1]
France1980FA152O-235-L2C1102550FA1520358FA1520372A13EU 1978-1982 model production[1]
France1981F152O-235-L2C1102550F15201809F15201893A13EU 1978-1982 model production[1]
France1981FA152O-235-L2C1102550FA1520373FA1520377A13EU 1978-1982 model production[1]
France1982F152O-235-L2C1102550F15201894F15201928A13EU 1978-1982 model production[1]
France1982FA152O-235-L2C1102550FA1520378FA1520382A13EU 1978-1982 model production[1]
USA1978152O-235-L2C11025501527940615282031Factory / type-design[2]
USA1978A152O-235-L2C1102550A1520735A1520808Factory / type-design[2]
USA1978A152O-235-L2C1102550A1500433A1500433Factory / type-design special serial[2]
USA1979152O-235-L2C11025501528203215283591Factory / type-design[2]
USA1979A152O-235-L2C1102550A1520809A1520878Factory / type-design[2]
USA1979A152O-235-L2C1102550681A15200681Factory / type-design special serial[2]
USA1980152O-235-L2C11025501528359215284541Factory / type-design[2]
USA1980A152O-235-L2C1102550A1520879A1520943Factory / type-design[2]
USA1981152O-235-L2C11025501528454215285161Factory / type-design[2]
USA1981A152O-235-L2C1102550A1520944A1520983Factory / type-design[2]
USA1982152O-235-L2C11025501528516215285594Factory / type-design[2]
USA1982A152O-235-L2C1102550A1520984A1521014Factory / type-design[2]

Relationship to the later N2C

The later O-235-N2C is recorded at 108 hp in the aircraft installation. That makes “every 152 has a 110 hp engine” an inaccurate generalization for this source set. The N2C also has its own production/rework effectivity, so an early serial number and a present engine suffix must be reconciled through aircraft records rather than forced into a factory-only story.

A replacement engine may share much of the family designation while still requiring a different installation and documentation analysis. Read the whole suffix and the applicable approval basis. This guide supplies the recorded L2C groups; it does not certify which engine is installed today or what work was accomplished during a past overhaul or replacement.

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Right side of a Cessna 152 engine with the battery and wiring visible
The right side of a Cessna 152 engine installation, including equipment behind the engine. Details vary with modifications. Photo: Brian Burger from Victoria, Canada · Wikimedia Commons · CC BY 2.0. Resized, WebP.

Propeller pairing and operating context

the 152/A152 and F152/FA152 applications name McCauley 1A103/TCM6958 with the L2C/N2C pairing. The application table retains U.S. and French entries independently. The TCM propeller guide explains its 69-inch maximum, 67.5-inch minimum diameter and recorded static-RPM window, together with the installed-propeller AD research path.

Propeller applications with original model and configuration scope
OriginAircraft ModelModel Year / ConfigEngineExact Propeller ApplicationMaximum diameter (in)Minimum diameter (in)Static RPM minimumStatic RPM maximumNotesPrimary Authority
USA152/A152AllO-235-L2C/N2C1A103/TCM69586967.522802380Spinner Dwg 0450073 in aircraft TCDS.[1]
FranceF152/FA1521978-1986O-235-L2C/N2C1A103/TCM69586967.522802380-[2]

Maintenance records and source boundaries

An oil-pump or ignition issue may apply through installed parts, modification history or an engine-specific directive. It should not be assigned merely because an aircraft belongs to the 152 family. The 152 AD reference preserves the conditions and historical status, including distinctions between active and superseded records. No aircraft-level compliance determination follows from an engine page.

The recorded engine fuel description is 100/100LL aviation gasoline. It does not authorize another grade or fuel-related modification. Similarly, engine catalogue weights do not replace the aircraft's current empty weight and moment. Follow the 152 loading guide for the separate aircraft limits, then reconcile the actual equipment list and records. A sound prebuy investigation connects these documents to the installed engine rather than using nominal horsepower as a proxy for condition.