Airworthiness Directives; McDonnell Douglas Model DC-9, Model MD-90-30, Model 717-200, and Model MD-88 Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2000-02-28 · Effective 2000-03-06 · 65 FR 10379
Document
Document number
00-4337
Federal Register citation
65 FR 10379
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2000-02-28
Effective date
2000-03-06
FAA docket
Docket No. 2000-NM-58-AD
Abstract
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2000-NM-58-AD that was sent previously to all known U.S. owners and operators of McDonnell Douglas Model DC-9, Model MD-90-30, Model 717-200, and Model MD-88 airplanes by individual telegrams. This AD requires inspecting the general condition of the jackscrew assembly and the area around the jackscrew assembly to detect the presence of metal shavings and flakes. This action is prompted by a report from an operator that indicated two instances of metallic shavings in the vicinity of the jackscrew assembly and gimbal nut of the horizontal stabilizer. The actions specified by this AD are intended to prevent loss of pitch trim capability due to excessive wear of the jackscrew assembly of the horizontal stabilizer, which could result in loss of vertical control of the airplane.