Airworthiness Directives; McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes
airworthiness · Rule · Final rule. · Published 2005-04-28 · Effective 2005-06-02 · 70 FR 21924
Document
Document number
05-8404
Federal Register citation
70 FR 21924
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-04-28
Effective date
2005-06-02
FAA docket
Docket No. 2001-NM-293-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 airplanes. The existing AD currently requires repetitive inspections to detect cracking of the main landing gear (MLG) shock strut pistons, and replacement of a cracked piston with a new or serviceable part. This amendment removes certain airplanes but requires that the existing inspections, and corrective actions if necessary, be accomplished on additional MLG shock strut pistons. This amendment also requires replacing the MLG shock strut pistons with new improved parts, which would terminate the repetitive inspections. 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 consequent damage to the airplane structure or injury to airplane occupants. This action is intended to address the identified unsafe condition.