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EASA Regulations for Piper PA-28

16 airworthiness directives and regulations affecting Piper PA-28.

EASA AD 2021-0107R2

Wings — Lower Main Wing Spar Caps — Inspection

EASA Airworthiness Directive 2021-0107R2 is an updated safety directive addressing inspection requirements for the lower main wing spar caps on Piper Aircraft, Inc. PA-28 and PA-32 aeroplanes. It mandates inspections to detect fatigue cracks in the lower main wing spar caps, which could lead to wing separation if undetected. The directive applies to multiple PA-28 and PA-32 models with specific serial numbers and includes detailed definitions and inspection procedures.

May 20, 2022
Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-28 (Archer)Piper Aircraft PA-28 (Cadet)Piper Aircraft PA-28 (Cherokee)Piper Aircraft PA-28 (Warrior)Piper Aircraft PA-28R (Arrow)Piper Aircraft PA-32 (Cherokee Six)Piper Aircraft PA-32R (Lance)Piper PA-28Piper PA-32

EASA AD 2021-0022

Engine — Main Bearing / Studs — Replacement

EASA Airworthiness Directive 2021-0022 is an airworthiness directive addressing Continental Aerospace Technologies GmbH TAE 125-02-99 and TAE 125-02-114 engines installed on various aircraft including Diamond DA 40, DA 42, DA 42M, CEAPR DR 400 series, Textron Aviation 172 series, and Piper PA-28 series. The directive mandates replacement of certain main bearing studs identified by specific batch numbers due to reported failures. It applies to all serial numbers listed in the associated service bulletin CG 125-1027 P1.

Jan 18, 2021
Airworthiness DirectiveMaintenanceSafety MgmtContinental Aerospace Technologies, Gmbh TAE125Diamond DA 40Diamond DA 42Diamond DA 42MCEAPR DR 400Textron Aviation 172Piper PA-28

EASA AD 2020-0228

[Correction] Engine — Turbocharger Hose — Replacement

EASA Airworthiness Directive 2020-0228 is a corrective directive addressing turbocharger hose replacement on certain Cessna F172 and Piper PA-28 aircraft equipped with Continental Aerospace Technologies TAE 125-02 diesel engines. The directive targets turbocharger hoses with part number TAE EPA 40-7520-H0131 01 from a specific defective batch that may fail and cause significant engine power loss. It applies to aircraft with engines installed via EASA Supplemental Type Certificates 10014287 and 10014364.

Dec 3, 2020
Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-28 (Archer)Piper Aircraft PA-28 (Cadet)Piper Aircraft PA-28 (Cherokee)Piper Aircraft PA-28 (Warrior)Textron Aviation 172 (Skyhawk)Textron Aviation F172Cessna F172Piper PA-28

EASA AD 2005-0035-CN

CANCELLED: Landing Gear - Main Undercarriage Structure - Inspection

EASA Airworthiness Directive 2005-0035-CN is a cancellation notice for the previous directive concerning the inspection of the main landing gear cylinder torque link attachment lugs on Piper Aircraft PA-28 and PA-32 aeroplanes. The affected aircraft include various PA-28 models and the PA-32-260, with specific serial numbers detailed in the directive. This cancellation reflects updated safety assessments and improved inspection procedures.

Feb 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-28 (Archer)Piper Aircraft PA-28 (Cadet)Piper Aircraft PA-28 (Cherokee)Piper Aircraft PA-28 (Warrior)Piper Aircraft PA-32 (Cherokee Six)Piper PA-28Piper PA-32

EASA AD 2017-0034R1

Engine — Gearbox — Modification / Inspection

EASA Airworthiness Directive 2017-0034R1 is a regulatory document addressing safety concerns related to Technify Motors GmbH TAE 125-02 engines installed on various aircraft including Diamond DA 40, DA 42, DA 42M, CEAPR DR 400, Cessna 172, and Piper PA-28. The directive mandates modification and inspection of the engine gearbox and clutch system to prevent oil leaks and potential engine power loss. It specifically targets affected gearboxes identified by part and serial numbers and requires replacement of the clutch with a dual mass flywheel.

Jan 18, 2018
Airworthiness DirectiveMaintenanceSafety MgmtContinental Aerospace Technologies, Gmbh TAE125Diamond DA 40Diamond DA 42Diamond DA 42MCEAPR DR 400Cessna 172Piper PA-28

EASA SIB CE-14-23

Piper PA-28, PA-32, PA-34, PA-44 and PA-46 Aeroplanes — Air Inlet Hose

The Special Airworthiness Information Bulletin SAIB: CE-14-23 is an FAA informational bulletin addressing an airworthiness concern for Piper Aircraft Models PA-28, PA-32, PA-34, PA-44, and PA-46 series airplanes. It highlights the risk of structural deterioration and possible collapse of the air inlet hose, which can reduce engine airflow and cause rough running or power loss. The bulletin does not mandate corrective action but provides important safety information for these Piper models.

Aug 26, 2014
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34Piper PA-44Piper PA-46

EASA SIB CE-11-42

Piper PA-28, PA-32, PA-34 and PA-44 Series - Flight Control Cable/Pulley Inspections

The Special Airworthiness Information Bulletin SAIB: CE-11-42 is an FAA informational bulletin addressing a potential airworthiness issue with flight control cables and pulleys on Piper PA-28, PA-32, PA-34, and PA-44 series airplanes. It highlights a manufacturing flaw in pulleys that can cause aileron control cables to fail, potentially resulting in loss of aileron control. The bulletin applies to all serial numbers of the specified Piper models and provides inspection guidance but does not mandate regulatory action.

Jun 30, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34Piper PA-44

EASA SIB CE-11-14

Piper PA-28, PA-32 and PA-34 - Vertical Stabilizer Forward Attachment Point Corrosion

The Special Airworthiness Information Bulletin CE-11-14 issued by the FAA on January 5, 2011, addresses potential corrosion on the vertical stabilizer forward attachment point of Piper PA-28, PA-32, and PA-34 aircraft. It highlights corrosion risks on specific parts, including steel fitting 62453-00 and aluminum bulkhead/frame assembly 62444-xx, based on service data from routine maintenance inspections. The bulletin provides inspection guidance from Piper service manuals and reminds operators to focus on corrosion prevention and detection.

Jan 17, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34

EASA SIB CE-11-13

Piper PA-34 aeroplanes - Forward Wing Spar Corrosion

The FAA Special Airworthiness Information Bulletin CE-11-13 is an informational bulletin addressing potential corrosion on the forward wing spar of Piper PA-28, PA-32, and PA-34 aircraft. It highlights corrosion risks at the fuselage attach fitting, landing gear attach point, and behind the leading edge fuel tank, and recommends incorporating Piper Service Bulletin 1006 to mitigate these issues. This bulletin does not mandate regulatory action but serves as guidance for owners and operators of the affected Piper models.

Jan 17, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34

EASA SIB CE-11-11

Piper PA-28, PA-32, and PA-34 - Aileron Hinge Fitting Corrosion

The FAA Special Airworthiness Information Bulletin CE-11-11 provides information regarding potential corrosion on the aileron hinge fittings of Piper PA-28, PA-32, and PA-34 aircraft. This bulletin is informational only and does not mandate any regulatory action but highlights the importance of inspections as outlined in the aircraft service manuals.

Jan 14, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34

EASA SIB CE-11-10

Piper PA-28, PA-32, PA-34, and PA-44 - Corrosion on Flap Hinges, Brackets, and Ribs

The Special Airworthiness Information Bulletin FAA SAIB CE-11-10 is an informational bulletin addressing potential corrosion issues on flap hinges, brackets, and ribs of Piper Aircraft models PA-28, PA-32, PA-34, and PA-44. It highlights corrosion found on specific parts including hinges (part numbers 62324-xx), ribs (62328-xx), and brackets (62323-00 and 65899-00). The bulletin provides guidance to operators to focus on inspections outlined in the aircraft service manuals to mitigate corrosion risks.

Jan 14, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34Piper PA-44

EASA SIB CE-11-01

Piper PA-28, PA-32, PA-34 and PA-44 series - Horizontal Stabilator Turnbuckle

The Special Airworthiness Information Bulletin SAIB: CE-11-01 is an FAA informational bulletin addressing a potential airworthiness concern involving the horizontal stabilator turnbuckle and control cable assembly on Piper PA-28, PA-32, PA-34, and PA-44 series airplanes. The issue involves stress corrosion cracking that could lead to failure of the turnbuckle/control cable assembly and loss of pitch control. This bulletin applies to all serial numbers of the specified Piper models.

Oct 15, 2010
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34Piper PA-44

EASA SIB CE-10-17

Piper PA-28 and PA-32 Main Landing Gear Torque Link Inspection Interval

The Special Airworthiness Information Bulletin (SAIB) CE-10-17 is an FAA informational bulletin addressing the inspection interval for the main landing gear torque link on Piper PA-28 and PA-32 aircraft models. It specifically concerns certain serial numbers of PA-28-140, PA-28-150/-160/-180, PA-28-235, PA-32-260, and PA-32-300 aircraft. The bulletin recommends incorporating Piper Service Bulletin 1199 to enhance inspection frequency and replacement times for the main landing gear torque link assemblies.

May 28, 2010
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32

EASA SIB CE-09-23

Fuel Starvation due to a Blocked Fuel Tank Outlet

Special Airworthiness Information Bulletin SAIB: CE-09-23 is an FAA informational bulletin addressing fuel starvation risks in Piper PA-28, PA-32, and PA-34 series airplanes. It highlights concerns about environmental deterioration of a sloshing compound previously used to repair leaking fuel tanks, which can peel and block fuel tank outlets, potentially starving the engine of fuel.

Apr 15, 2009
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34

EASA SIB CE-09-17

Piper PA-28 Fuel Supply and Vent Lines Maintenance

The Special Airworthiness Information Bulletin (SAIB) CE-09-17 issued by the FAA addresses fuel vent and supply hose maintenance for all serial numbers of Piper PA-28 series aircraft. It highlights concerns about environmental deterioration of fuel inlet and vent lines inside the wings, which may cause fuel odors or staining but does not mandate regulatory action. The bulletin serves as an informational alert to owners and operators about potential fuel leakage risks associated with aging hoses.

Mar 13, 2009
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28

EASA SIB 2008-84R1

Funkwerk Avionics (formerly Filser Electronic) TRT600 and TRT800 Series Transponders — Intermittent Loss of Detection, Insufficient Mode S Reply.

EASA Safety Information Bulletin 2008-84R1 addresses intermittent loss of detection and insufficient Mode S replies from Funkwerk Avionics TRT600 and TRT800 Series Transponders, including units formerly manufactured by Filser Electronic. These transponders are installed on various aircraft such as Cessna 150, 172, 182, 210, Diamond DA 20, Mooney M20J, Piper PA-28, and multiple sailplane models. The bulletin highlights issues affecting radar tracking and Mode S interrogation responses in European airspace.

Nov 12, 2008
Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 172Cessna 182Cessna 210Diamond DA 20Mooney M20JPiper PA-28