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Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; and Model DC-9-81 (MD-81) and DC-9-82 (MD-82) Airplanes

airworthiness · Rule · Final rule. · Published 2005-03-30 · Effective 2005-05-04 · 70 FR 16098

Document

Document number
05-6109
Federal Register citation
70 FR 16098
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-03-30
Effective date
2005-05-04
FAA docket
Docket No. FAA-2004-18774

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 series airplanes; and Model DC-9-81 (MD-81) and DC-9-82 (MD-82) airplanes. This AD requires repetitive detailed inspections of the upper and lower caps of the rear spar of the left and right wings, and corrective action if necessary. This AD also provides an optional modification that would end the repetitive inspections. This AD is prompted by reports of fatigue cracks in the upper and lower caps of the wing spar. We are issuing this AD to detect and correct fatigue cracking in the upper and lower caps of the rear spar of the left and right wings, which could result in structural failure of the wings.

Source

Authoritative
Federal Register document
Machine
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