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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; request for comments. · Published 2007-05-08 · Effective 2007-05-23 · 72 FR 25960

Document

Document number
E7-8768
Federal Register citation
72 FR 25960
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2007-05-08
Effective date
2007-05-23
FAA docket
Docket No. FAA-2007-28100

Abstract

The FAA is adopting a new airworthiness directive (AD) for all 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. This AD requires repetitive inspections to detect cracks in the horizontal stabilizer, and related investigative/corrective actions if necessary. This AD results from reports of cracks found in the horizontal stabilizer--in the upper and lower aft skin panels at the aft inboard corner at station XH = 8.2, and in the rear spar upper caps adjacent to the aft skin panel at station XH = 10.0. We are issuing this AD to detect and correct cracks in the upper and lower aft skin panels and rear spar upper caps, which, if not corrected, could lead to the loss of overall structural integrity of the horizontal stabilizer.

Source

Authoritative
Federal Register document
Machine
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