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Airworthiness Directives; McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes

airworthiness · Rule · Final rule. · Published 2006-03-31 · Effective 2006-05-05 · 71 FR 16201

Document

Document number
06-3061
Federal Register citation
71 FR 16201
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2006-03-31
Effective date
2006-05-05
FAA docket
Docket No. FAA-2005-23197

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes. This AD requires repetitive inspections for stress corrosion cracks of the main fuselage frame, and corrective actions if necessary. This AD also provides an optional terminating action for the repetitive inspections. This AD results from several reports of cracking of the main fuselage frame. We are issuing this AD to detect and correct stress corrosion cracking of the main fuselage frame, which could result in extensive damage to adjacent structure and reduced structural integrity of the airplane.

Source

Authoritative
Federal Register document
Machine
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