EASA Regulations for Piper PA-31-300

2 airworthiness directives and regulations affecting Piper PA-31-300.

EASA SIB CE-14-07

[Correction] Piper PA-31 Series — Main Wing Spar Lower Cap Cracks

The FAA Special Airworthiness Information Bulletin SAIB: CE-14-07 addresses cracking found in the main wing spar lower cap of Piper Aircraft Models PA-31, PA-31-300, PA-31-325, and PA-31-350. It provides inspection guidance for the wing main spar lower cap at the centerline spar splice plate to detect fatigue and stress corrosion cracks. This bulletin is informational and does not mandate regulatory action.

Jan 24, 2014

Safety Information BulletinMaintenanceSafety MgmtPiper PA-31Piper PA-31-300Piper PA-31-325Piper PA-31-350

EASA SIB 2010-09R1

Piper PA-31 - Wing Leading Edge Stall Strip Configuration

EASA Safety Information Bulletin 2010-09R1 is an advisory document addressing the wing leading edge stall strip configuration for Piper PA-31 series aircraft, including PA-31, PA-31-300, PA-31-325, and PA-31-350 models. It highlights the importance of correct stall strip installation to maintain conformity with the aircraft's Type Design and improve low-speed handling characteristics. The bulletin supports CASA Australia's Airworthiness Bulletin 57-009 Issue 2 and provides guidance for European operators and maintainers.

Oct 20, 2010

Safety Information BulletinMaintenanceSafety MgmtPiper PA-31Piper PA-31-300Piper PA-31-325Piper PA-31-350