Airworthiness Directives; Boeing Model 727 and 727C Series Airplanes
airworthiness · Rule · Final rule. · Published 2000-05-01 · Effective 2000-06-05 · 65 FR 25278
Document
Document number
00-10287
Federal Register citation
65 FR 25278
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 727 and 727C Series
Publication date
2000-05-01
Effective date
2000-06-05
FAA docket
Docket No. 98-NM-293-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 727 and 727C series airplanes, that requires one-time inspections of the exterior body skin located at the forward corners of the mid-galley door hinge cutouts to detect cracking, and corrective actions, if necessary. This AD also requires modification of the body skin of the mid-galley door hinge cutouts. This amendment is prompted by a report indicating that, during fatigue testing on a Boeing Model 727 series airplane, a crack was found in the body skin at the lower forward corners of the mid-galley door hinge cutouts due to cabin pressurization cycles. The actions specified by this AD are intended to prevent such fatigue cracking of the body skin, which could result in reduced structural integrity of the fuselage and consequent loss of cabin pressurization.