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Airworthiness Directives; McDonnell Douglas Model DC-9-81 (MD-81) and DC-9-82 (MD-82) Airplanes

airworthiness · Rule · Final rule. · Published 2007-12-10 · Effective 2008-01-14 · 72 FR 69591

Document

Document number
E7-23687
Federal Register citation
72 FR 69591
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model DC-9-81 (MD-81) and DC-9-82 (MD-82)
Publication date
2007-12-10
Effective date
2008-01-14
FAA docket
Docket No. FAA-2007-29226

Abstract

We are adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-9-81 (MD-81) and DC-9-82 (MD-82) airplanes. This AD requires, for certain airplanes, inspecting for cracking of the fuselage skin at the upper corners of the forward passenger doorjamb, installing or replacing doublers as applicable, and doing applicable repairs. This AD results from reports of fatigue cracking in the fuselage skin at the upper corners of the forward passenger doorjamb. We are issuing this AD to prevent cracking of the fuselage skin at the upper corners of the forward passenger doorjamb, which could lead to loss of overall structural integrity of the airplane.

Source

Authoritative
Federal Register document
Machine
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