EASA Regulations for Piper PA-34-220T

3 airworthiness directives and regulations affecting Piper PA-34-220T.

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New ADs and bulletins for Piper PA-34-220T, summarized like the ones below, every Monday.

EASA AD US-2024-10-04

May 23, 2024

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.

Airworthiness Directive
  • Piper Aircraft PA-28 (Archer)
  • Piper Aircraft PA-28R (Arrow)
  • Piper Aircraft PA-34 (Seneca)
  • Piper Aircraft PA-44 (Seminole)
  • Piper PA-28-181
  • Piper PA-28R-201
  • Piper PA-34-220T
  • Piper PA-44-180

EASA AD US-2020-24-09

Dec 2, 2020

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.

Airworthiness Directive
  • Piper Aircraft PA-34 (Seneca)
  • Piper PA-34-220T

EASA SIB CE-09-15

Mar 3, 2009

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.

Safety Information Bulletin
  • Piper PA-34-200
  • Piper PA-34-200T
  • Piper PA-34-220T