Airworthiness Directives; McDonnell Douglas Model DC-9 and DC-9- 80 Series Airplanes, Model MD-88 Airplanes, and C-9 (Military) Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-12-03 · Effective 1999-01-07 · 63 FR 66739
Document
Document number
98-31698
Federal Register citation
63 FR 66739
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model DC-9 and DC-9- 80 Series
Publication date
1998-12-03
Effective date
1999-01-07
FAA docket
Docket No. 97-NM-21-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-9 and DC-9-80 series airplanes, Model MD-88 airplanes, and C-9 (military) series airplanes, that requires a one-time visual inspection to detect fatigue cracking of the lower left nose of certain longerons and the attaching frames; repair, if necessary; and installation of a preventive modification. This amendment is prompted by several reports of fatigue cracking of certain longerons and the attaching frames. The actions specified by this AD are intended to prevent such fatigue cracking, which could result in reduced structural integrity of the fuselage, and consequent loss of pressurization of the airplane.