EASA Regulations for Piper PA-46R-350T

5 airworthiness directives and regulations affecting Piper PA-46R-350T.

EASA AD US-2021-09-02

Vacuum - Stall Warning Heat Control - Modification

Airworthiness Directive 2021-09-02 is a final rule issued by the Federal Aviation Administration addressing certain Piper Aircraft, Inc. models PA-46-350P (Malibu Mirage), PA-46R-350T (Malibu Matrix), and PA-46-500TP (Malibu Meridian) airplanes. This directive corrects an error in the previously issued AD 2021-04-07 regarding the part number of the stall warning heat control modification kit. It requires inspection and correction of nonconforming stall warning heat control systems to ensure compliance with the proper design.

Apr 16, 2021

Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-46 (Malibu)Piper PA-46-350PPiper PA-46R-350TPiper PA-46-500TP

EASA AD US-2021-04-07

SUPERSEDED BY FAA AD 2021-09-02

FAA Airworthiness Directive 2021-04-07 is a final rule addressing Piper Aircraft, Inc. Models PA-46-350P (Malibu Mirage), PA-46R-350T (Malibu Matrix), and PA-46-500TP (Malibu Meridian) airplanes. It requires inspection and correction of stall warning heat control systems on certain airplanes to prevent stall warning failure due to ice formation on the stall vane during flight in icing conditions with landing gear down.

Mar 1, 2021

Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-46 (Malibu)Piper PA-46-350PPiper PA-46R-350TPiper PA-46-500TP

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

EASA SIB CE-11-09

Avidyne Corporation - Flight Management Computing Software System [Piper PA-46R-350T / Cirrus SR20, SR22]

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-09 informs operators and maintenance personnel about a software issue in the Avidyne Corporation Flight Management Computing Software System installed on Piper PA-46R-350T and Cirrus SR20/SR22 aircraft. The bulletin highlights a faulty transition logic causing incorrect altitude limits to be displayed on the Flight Management System. This issue affects aircraft equipped with the Avidyne Entegra Integrated Flight Display system, part number 700-00083-( ), across any software release.

Jan 17, 2011

Safety Information BulletinFlight OpsMaintenanceSafety MgmtPiper PA-46R-350TCirrus SR20Cirrus SR22