Airworthiness Directives; the Boeing Company Airplanes
airworthiness · Rule · Final rule. · Published 2016-02-04 · Effective 2016-03-10 · 81 FR 5893
Document
Document number
2016-01827
Federal Register citation
81 FR 5893
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
the Boeing Company
Publication date
2016-02-04
Effective date
2016-03-10
FAA docket
Docket No. FAA-2015-1983
Abstract
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD was prompted by a report of a crack of the forward leg of the left front spar lower chord and cracks on the lower wing skin at three fastener holes common to the nacelle outboard side load fitting. This AD requires repetitive inspections for cracks on the front spar lower chord, inspar skin, and wing skin, and corrective action if necessary. We are issuing this AD to detect and correct fatigue cracking of the forward leg of the front spar lower chord, inspar skin, and wing skin common to the nacelle outboard side load fitting, which could adversely affect the structural integrity of the wing.