Airworthiness Directive

AD 2002-23-06 67 FR 68932 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-29003
Amendment
39-12950
Published
2002-11-14
Effective
2002-11-19
Models covered
1
Last live check
2026-10-02
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AD

2002-23-06

FR doc 02-29003 · 67 FR 68932

AD 2002-23-06Published 2002-11-14Effective 2002-11-19

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 replacing certain zinc-plated crankshaft gear retaining bolts.

Full official abstract

This amendment supersedes an emergency airworthiness directive (AD) that was sent previously to all known U.S. owners and operators of Textron Lycoming (T/L) AEIO-540, IO-540, LTIO-540, O-540, and TIO-540 series reciprocating engines. That action requires replacing certain zinc-plated crankshaft gear retaining bolts. This action still requires replacing certain zinc-plated crankshaft gear retaining bolts, but expands the population of affected engines. This amendment is prompted by two recent failures of zinc-plated crankshaft gear retaining bolts, and a reassessment of the extent to which the suspect bolts may still be present in the field. The actions specified by this AD are intended to prevent loss of all engine power and possible forced landing.

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All Lycoming O-540 directives

Applies to 1 model in our index