Airworthiness Directives; McDonnell Douglas Model DC-8-33, -42, -55, and -61 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2001-03-23 · Effective 2001-04-09 · 66 FR 16105
Document
Document number
01-6643
Federal Register citation
66 FR 16105
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2001-03-23
Effective date
2001-04-09
FAA docket
Docket No. 2000-NM-254-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to McDonnell Douglas Model DC-8-33, -42, -55, and -61 series airplanes. This action requires detailed visual and eddy current inspections of the lower wing skin at the 3 outboard fasteners of stringer 64 end fitting to detect cracks; and corrective actions, if necessary. This action is necessary to prevent fatigue cracking of the lower wing skin, which could reduce structural integrity and loss of fail-safe capability of the airplane. This action is intended to address the identified unsafe condition.