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Airworthiness Directives; Textron Lycoming AEIO-540, IO-540, LTIO-540, O-540, and TIO-540 Series Reciprocating Engines

airworthiness · Rule · Final rule, request for comments. · Published 2002-11-14 · Effective 2002-11-19 · 67 FR 68932

Document

Document number
02-29003
Federal Register citation
67 FR 68932
Type
Rule
Action
Final rule, request for comments.
Category
airworthiness
Publication date
2002-11-14
Effective date
2002-11-19
FAA docket
Docket No. 2002-NE-31-AD

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.

Source

Authoritative
Federal Register document
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