EASA Regulations for Piper PA-34-220T

EASA AD US-2024-10-04

Wings - Rear Wing Spar Attachment Fitting - Inspection

The Federal Aviation Administration's Airworthiness Directive 2024-10-04 addresses certain Piper Aircraft, Inc. models PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes. This directive mandates inspection of the rear wing spar attachment fitting due to a manufacturing defect involving a double-drilled bolt hole, which compromises structural integrity. The AD aims to prevent potential wing separation and loss of control by requiring inspections and corrective actions as necessary.