← FAA Federal Register actions

Airworthiness Directives; McDonnell Douglas Model DC-9-14, DC-9-15, and DC-9-15F Airplanes; DC-9-20, DC-9-30, DC-9-40, DC-9-50 Series Airplanes; DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes; and Model MD-88 Airplanes

airworthiness · Rule · Final rule. · Published 2004-12-16 · Effective 2005-01-20 · 69 FR 75231

Document

Document number
04-27332
Federal Register citation
69 FR 75231
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-12-16
Effective date
2005-01-20
FAA docket
Docket No. 2002-NM-333-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas airplane models, that requires an inspection of the retract cylinder support fitting and the cylinder bore of the support fitting of both main landing gear (MLG) for corrosion, and corrective action if necessary. This action also requires replacing cadmium-plated retract cylinder support bushings and bearings of both MLG. This action is necessary to detect and correct corrosion to the retract cylinder support fitting of the MLG and the cylinder bore in the support fitting, which could result in compromised integrity of the retract cylinder support fitting of the MLG and possible damage to the hydraulic system. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown