← FAA Federal Register actions

Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-12-14 · Effective 1999-01-19 · 63 FR 68672

Document

Document number
98-32811
Federal Register citation
63 FR 68672
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model MD-11 Series
Publication date
1998-12-14
Effective date
1999-01-19
FAA docket
Docket No. 96-NM-227-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD-11 series airplanes. This amendment requires inspections to detect attachment failures of the 12 attachments located on the No. 4 banjo fitting/pylon carry- through cap, and to detect cracking of the forward and aft flanges and bolt holes of the No. 4 banjo fitting; repair, if necessary; and replacement of the 12 attachments with new or serviceable parts. Such replacement terminates the repetitive inspections. This amendment is prompted by a report indicating that attachment bolts on the forward and aft flanges of the No. 4 banjo fitting and the pylon carry-through cap failed due to fatigue cracking. The actions specified by this AD are intended to prevent such cracking, which could result in reduced controllability of the airplane during flight and ground operations.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown