EASA Regulations for Piper PA-23-250

2 airworthiness directives and regulations affecting Piper PA-23-250.

EASA AD US-2021-25-11

Stabilizers - Horizontal Stabilator Tip Tube and Weight Assemblies - Inspection

Airworthiness Directive 2021-25-11 is a final rule issued by the Federal Aviation Administration (FAA) addressing Piper Aircraft, Inc. Model PA-23-250 airplanes. It mandates inspections and modifications of the horizontal stabilator tip tube and weight assemblies to detect and correct cracks and prevent structural weakening. This directive applies to specific serial-numbered Piper PA-23-250 airplanes and updates previous inspection requirements.

Jan 3, 2022

Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-23 (Aztec)Piper PA-23-250

EASA SIB CE-12-44

Piper PA-23-250 Aeroplanes with Lycoming IO-540-C4B5 Engines (Exhaust systems)

The Special Airworthiness Information Bulletin SAIB: CE-12-44 is an FAA informational bulletin concerning the exhaust systems of Piper PA-23-250 (Aztec) aircraft equipped with Lycoming IO-540-C4B5 engines. It addresses airworthiness concerns related to the engines' crossover exhaust assemblies, highlighting potential durability and functional issues without mandating regulatory action. The bulletin provides guidance for inspection and maintenance to prevent exhaust system failures.

Jan 14, 2013

Safety Information BulletinMaintenanceSafety MgmtPiper PA-23-250