Airworthiness Directives; The Boeing Company Airplanes
airworthiness · Rule · Final rule. · Published 2016-05-09 · Effective 2016-06-13 · 81 FR 27989
Document
Document number
2016-10524
Federal Register citation
81 FR 27989
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
The Boeing Company
Publication date
2016-05-09
Effective date
2016-06-13
FAA docket
Docket No. FAA-2015-0246
Abstract
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-300, -400, and -500 series airplanes. This AD was prompted by reports of fatigue cracking found at the left-side and right-side upper frames, at a certain area. This AD requires repetitive medium frequency eddy current (MFEC) inspections for cracking of the left-side and right-side upper frames, and repair (including open hole high frequency eddy current (HFEC) inspections for cracking of fastener holes) if necessary. This AD also provides an optional preventive modification, which terminates the repetitive inspections at the modified location. We are issuing this AD to detect and correct fatigue cracking of the upper frame, which can grow in size and result in a severed frame, leading to rapid decompression and consequent reduced structural integrity of the airplane.