EASA AD US-2024-10-04
Wings - Rear Wing Spar Attachment Fitting - Inspection
Summary
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.
What Changed
This new airworthiness directive introduces mandatory inspections of the rear wing spar attachment fitting on specified Piper aircraft models. If discrepancies are found, it requires inspection of the forward wing spar attachment fitting and corrective actions. Additionally, operators must report inspection results to the FAA when repairs are needed.
Why It Matters
This AD is critical for aviation professionals because the identified defect can lead to structural failure of the wing, posing a significant safety risk. Operators and maintenance organizations must promptly identify and rectify any issues to ensure continued airworthiness and prevent accidents. Compliance helps maintain safety standards and avoid operational disruptions.
What To Do
Operators of affected Piper PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes must inspect the rear wing spar attachment fitting by June 6, 2024. If any discrepancies are found, they must inspect the forward wing spar attachment fitting, perform necessary repairs, and report the findings to the FAA. Comments on the AD are accepted until July 8, 2024.