EASA Regulations for Piper PA-46-310P

2 airworthiness directives and regulations affecting Piper PA-46-310P.

EASA SIB CE-15-18

Piper PA-46 Aeroplanes — Wing Main Spar Lower Cap Cracks

The Special Airworthiness Information Bulletin SAIB: CE-15-18 is an FAA informational bulletin addressing fatigue cracking in the wing main spar lower cap near wing station 79 on Piper Aircraft Models PA-46-310P, PA-46-350P, PA-46R-350T, and PA-46-500TP airplanes. It highlights the discovery of a fatigue crack during routine inspection and provides guidance on recommended inspections and repairs. This bulletin is advisory and does not mandate regulatory action under 14 CFR part 39.

Jul 15, 2015

Safety Information BulletinMaintenanceSafety MgmtPiper PA-46-310PPiper PA-46-350PPiper PA-46R-350TPiper PA-46-500TP

EASA SIB CE-09-13R1

Piper PA-46 Aeroplanes - Engine Mount - Cracking at Nose Landing Gear

The Special Airworthiness Information Bulletin (SAIB) CE-09-13R1 issued by the FAA addresses potential cracking in the engine mounts of certain Piper PA-46 series airplanes, specifically the PA-46-310P, PA-46-350P, PA-46R-350T, and PA-46-500TP models. The cracks occur at the nose landing gear trunnion and actuator attachment points, which could affect the structural integrity of the engine mount. This bulletin provides updated service information and recommendations for inspections and replacements to mitigate the issue.

Aug 27, 2014

Safety Information BulletinMaintenanceSafety MgmtPiper PA-46-310PPiper PA-46-350PPiper PA-46R-350TPiper PA-46-500TP