EASA AD US-2017-26-07
Fuselage - Frame Web at STA 1681 - Inspection
Federal Aviation Administration Airworthiness Directive 2017-26-07 is a final rule addressing certain Boeing 757-200, -200CB, and -300 series airplanes. It mandates inspections of the fuselage frame web at station 1681 for fatigue cracking, including checks for existing repairs and repetitive inspections, to ensure structural integrity. This directive responds to reports of fatigue cracks that could compromise airplane safety.