Airworthiness Directives; McDonnell Douglas Model DC-9-15, DC-9-31, and DC-9-32 Airplanes
airworthiness · Rule · Final rule. · Published 2004-04-06 · Effective 2004-05-11 · 69 FR 17909
Document
Document number
04-7297
Federal Register citation
69 FR 17909
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-04-06
Effective date
2004-05-11
FAA docket
Docket No. 2003-NM-60-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-9-15, DC-9-31, and DC- 9-32 airplanes, that requires repetitive visual and x-ray inspections to detect cracks of the upper and lower corners and upper center of the door cutout of the aft pressure bulkhead; corrective actions, if necessary; and follow-on actions. For certain airplanes, this AD also requires modification of the ventral aft pressure bulkhead. This action is necessary to detect and correct fatigue cracks in the corners and upper center of the door cutout of the aft pressure bulkhead, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane. This action is intended to address the identified unsafe condition.