← FAA Federal Register actions

Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes, Model MD-88 Airplanes, and Model MD-90-30 Airplanes

airworthiness · Rule · Final rule. · Published 1999-06-23 · Effective 1999-07-28 · 64 FR 33392

Document

Document number
99-15777
Federal Register citation
64 FR 33392
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model DC-9-80 Series
Publication date
1999-06-23
Effective date
1999-07-28
FAA docket
Docket No. 98-NM-109-AD

Abstract

This amendment adopts a new airworthiness directive (AD); applicable to certain McDonnell Douglas Model DC-9-80 series airplanes, Model MD-88 airplanes, and Model MD-90-30 airplanes; that 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 is prompted by reports indicating that, while an airplane was positioned on the taxiway, the right MLG shock strut piston failed due to fatigue cracking. The actions specified by this AD are intended to detect and correct such fatigue cracking, which could result in failure of the piston, and consequent damage to the airplane structure or injury to the passengers and flightcrew.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown