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Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o. Models PZL M18, PZL M18A, and PZL M18B Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2000-09-15 · Effective 2000-09-27 · 65 FR 55891

Document

Document number
00-23322
Federal Register citation
65 FR 55891
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2000-09-15
Effective date
2000-09-27
FAA docket
Docket No. 99-CE-84-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Polskie Zaklady Lotnicze Spolka zo.o. (PZL-Mielac) Models PZL M18, PZL M18A, and PZL M18B airplanes. This AD requires you to repetitively inspect the centerwing-to-outboard wing attach joints for cracks in the lugs, corrosion in the main holes, and ovalization of the main holes; repair corrosion and apply anti-corrosion protection; replace the wing attach joints, as necessary; and eliminate any ovalization of the wing main joint holes. This AD is the result two instances of in-flight wing separation on Model PZL M18A airplanes where severe corrosion and pitting led to high stress concentrations on the wing attachment joints. The actions specified by this AD are intended to detect and correct cracks in the lugs, corrosion in the main holes, and ovalization of the main holes, in the centerwing-to- outboard wing attach joints. Such damage could result in failure of the joints with consequent in-flight wing separation.

Source

Authoritative
Federal Register document
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