EASA Regulations for Piper PA-34-220T

3 airworthiness directives and regulations affecting 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.

May 23, 2024

Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-28 (Archer)Piper Aircraft PA-28R (Arrow)Piper Aircraft PA-34 (Seneca)Piper Aircraft PA-44 (Seminole)Piper PA-28-181Piper PA-28R-201Piper PA-34-220TPiper PA-44-180

EASA AD US-2020-24-09

Flight Controls - Rudder Flight Control Cables and the Emergency Power Supply Wiring - Inspection / Replacement

Federal Register Volume 85, Number 231 (December 1, 2020) is a final rule airworthiness directive issued by the FAA addressing certain Piper Aircraft, Inc. Model PA-34-220T airplanes. The directive focuses on inspecting and replacing rudder flight control cables and emergency power supply wiring, and re-routing the wiring harness to prevent damage caused by inadequate clearance. This AD aims to ensure the continued airworthiness and safety of the affected Piper PA-34-220T aircraft.

Dec 2, 2020

Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-34 (Seneca)Piper PA-34-220T

EASA SIB CE-09-15

Piper PA-34 Nose Gear Centering Attach Bolt

The Special Airworthiness Information Bulletin SAIB CE-09-15 is an FAA informational bulletin addressing a nose gear centering attach bolt issue on Piper Aircraft Models PA-34-200, PA-34-200T, and PA-34-220T. It highlights a potential failure of the nose landing gear to extend due to the hex-head bolt on the nose gear centering spring rod-end jamming against the nose gear door actuation aft tube assembly. This bulletin provides awareness but does not mandate corrective action under 14 CFR part 39.

Mar 3, 2009

Safety Information BulletinMaintenanceSafety MgmtPiper PA-34-200Piper PA-34-200TPiper PA-34-220T