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

airworthiness · Rule · Final rule. · Published 2001-05-10 · Effective 2001-06-14 · 66 FR 23840

Document

Document number
01-11674
Federal Register citation
66 FR 23840
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model DC-9-80 Series
Publication date
2001-05-10
Effective date
2001-06-14
FAA docket
Docket No. 99-NM-164-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-9-80 series airplanes and Model MD-88 airplanes, that currently requires a one-time inspection to detect cracking of the main landing gear (MLG) pistons, and repair or replacement of the pistons with new or serviceable parts, if necessary. This amendment requires, among other actions, repetitive dye penetrant and magnetic particle inspections to detect cracks of the MLG pistons; repair and replacement of discrepant parts; and installation of a preventative modification; as applicable. This amendment also provides for an optional terminating action for certain MLG pistons. This amendment is prompted by additional reports of failure of the MLG pistons during towing of the airplanes. The actions specified by this AD are intended to prevent fatigue cracking of the MLG pistons, which could result in failure of the pistons and subsequent damage to the airplane structure or injury to airplane occupants.

Source

Authoritative
Federal Register document
Machine
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