Airworthiness Directives; Boeing Model 727 Airplanes
airworthiness · Rule · Final rule. · Published 2005-10-05 · Effective 2005-11-09 · 70 FR 58002
Document
Document number
05-19842
Federal Register citation
70 FR 58002
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 727
Publication date
2005-10-05
Effective date
2005-11-09
FAA docket
Docket No. FAA-2005-21085
Abstract
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 727 airplanes. This AD requires a one-time inspection of the lower lobe frames of body section 43 to find open holes between stringers 17L and 17R and to record their location; repetitive high frequency eddy current (HFEC) inspections for cracks of all open holes; and related investigative and corrective actions if necessary. This AD also includes an optional terminating action of installing rivets in all open tooling holes and all unused lining holes, which would terminate the repetitive open-hole HFEC inspections once a hole is plugged with a rivet. This AD results from reports of cracks at open tooling holes in the lower lobe frames of body section 43. We are issuing this AD to detect and correct cracks in the frames, which could result in cracks in the skin panels and rapid decompression of the airplane.