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Airworthiness Directive

AD 95-03-10 61 FR 625 Active

Federal Aviation Administration · 14 CFR part 39

Requires a one- time inspection within the next 5 hours time in service to determine the part number (P/N) and revision letter of the push rod installed on the engine.

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FR document
96-272
Amendment
39-9458
Published
1996-01-09
Effective
1996-01-24
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/95-03-10 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

95-03-10

FR doc 96-272 · 61 FR 625

AD 95-03-10Published 1996-01-09Effective 1996-01-24

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires a one- time inspection within the next 5 hours time in service to determine the part number (P/N) and revision letter of the push rod installed on the engine.

Full official abstract

This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 95-03-10 that was sent previously to all known U.S. owners and operators of Textron Lycoming O-235 series reciprocating engines by individual letters. This AD requires a one- time inspection within the next 5 hours time in service to determine the part number (P/N) and revision letter of the push rod installed on the engine. All push rods with P/N 73806 and revision letters ``V'' or ``W'' must be replaced with serviceable parts. This amendment is prompted by reports of several failures of push rods. The actions specified by this AD are intended to prevent engine roughness and power loss, which could result in loss of the aircraft.

More directives for Lycoming O-235

  1. AD 2026-17-10 Airworthiness Directives; Lycoming Engines Effective 2026-09-14

All Lycoming O-235 directives

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Applies to 1 model in our index