Airworthiness Directives; McDonnell Douglas Model DC-9-10, -15, and -30 Series Airplanes, and C-9 (Military) Airplanes
airworthiness · Rule · Final rule. · Published 1998-09-15 · Effective 1998-10-20 · 63 FR 49267
Document
Document number
98-24246
Federal Register citation
63 FR 49267
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-09-15
Effective date
1998-10-20
FAA docket
Docket No. 96-NM-272-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-9-10, -15, and -30 series airplanes, and C-9 (military) airplanes, that requires a one- time visual inspection to determine if all corners of the upper cargo doorjamb have been previously modified; various follow-on repetitive inspections; and modification, if necessary. This amendment is prompted by reports of fatigue cracks found in the fuselage skin and doubler at the corners of the upper cargo doorjamb. The actions specified by this AD are intended to detect and correct such fatigue cracking, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane.