EASA Regulations for Piper PA-31

4 airworthiness directives and regulations affecting Piper PA-31.

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New ADs and bulletins for Piper PA-31, summarized like the ones below, every Monday.

EASA SIB CE-14-07

Jan 24, 2014

[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.

Safety Information Bulletin
  • Piper PA-31300325350

EASA SIB 2010-09R1

Oct 20, 2010

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.

Safety Information Bulletin
  • Piper PA-31300325350

EASA SIB 2008-55R1

Jul 24, 2008

WITHDRAWN - REPLACED BY FAA AD 2009-13-06

EASA Safety Information Bulletin 2008-55R1 is a safety information bulletin addressing the forward baggage door locking mechanism components on Piper PA-23, PA-31, and PA-42 series aircraft. It provides recommendations for inspection, lubrication, and replacement of the nose baggage door locking mechanism to prevent the forward baggage door from opening in flight. The bulletin supports FAA Safety Alert for Operators SAFO 08013 and Piper Aircraft Inc. Service Bulletin 1194.

Safety Information Bulletin
  • Piper PA-23
  • Piper PA-31
  • Piper PA-42

EASA SIB 2008-02

Jan 11, 2008

FAA SAIB CE-08-11 - Piper PA-23, PA-31 and PA-42 Aeroplanes - Hydraulic Hose P/N 17766-02 (465-138) Potential Failure

FAA Special Airworthiness Information Bulletin CE-08-11 is an informational bulletin addressing a potential failure of hydraulic hose part number 17766-02 (465-138) on New Piper Aircraft models PA-23, PA-31, and PA-42. The hydraulic hose failure may cause loss of pressure needed to extend the landing gear, affecting all serial numbers of the listed Piper aircraft. This bulletin alerts operators and maintenance personnel to inspect and monitor this specific hydraulic hose for deterioration.

Safety Information Bulletin
  • Piper PA-23
  • Piper PA-31
  • Piper PA-42