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Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes and Model MD-88 Airplanes

airworthiness · Rule · Final rule. · Published 1999-11-19 · Effective 1999-12-27 · 64 FR 63187

Document

Document number
99-30056
Federal Register citation
64 FR 63187
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model DC-9-80 Series
Publication date
1999-11-19
Effective date
1999-12-27
FAA docket
Docket No. 99-NM-05-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-9-80 series airplanes and Model MD-88 airplanes, that requires a one-time visual inspection to determine whether self-aligning nuts are installed at certain locations of the aft pressure bulkhead tee; and corrective actions, if necessary. This amendment is prompted by reports of failures of certain Hi-Lok pin fasteners of the aft pressure bulkhead tee due to installation of non-self-aligning nuts. The actions specified by this AD are intended to prevent failure of certain Hi-Lok pin fasteners and subsequent gouging of the aft pressure bulkhead tee, which could result in fatigue cracking and reduced structural integrity of the airplane.

Source

Authoritative
Federal Register document
Machine
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