EASA Regulations for ATR ATR42

67 airworthiness directives and regulations affecting ATR ATR42.

EASA AD 2018-0105

Electric / Electronic Common Installation — Electrical Harness Brackets and Wire Bundles — Inspection

EASA Airworthiness Directive 2018-0105 is an official safety directive addressing inspection requirements for electrical harness brackets and wire bundles on ATR 42 and ATR 72 aeroplanes. It applies specifically to certain manufacturer serial numbers of ATR 42-500 and ATR 72-212A models. The directive mandates inspections to detect missing brackets and potential wire damage that could lead to system failures.

May 8, 2018

Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42-500ATR 72-212A

EASA AD 2018-0080

Landing Gear — Main Landing Gear Universal Joints — Inspection / Replacement

EASA Airworthiness Directive 2018-0080 is an official regulatory document addressing inspection and replacement requirements for main landing gear universal joints on ATR 42 and ATR 72 aeroplanes. It applies to multiple ATR 42 variants including -200, -300, -320, -400, and -500, as well as ATR 72 models 101, 102, 201, 202, 211, 212, and 212A. The directive mandates repetitive inspections and corrective actions to prevent structural failure of the main landing gear universal joints.

Apr 11, 2018

Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42-200ATR 42-300ATR 42-320ATR 42-400ATR 42-500ATR 72-101ATR 72-102ATR 72-201ATR 72-202ATR 72-211ATR 72-212ATR 72-212A

EASA AD 2017-0221R1

SUPERSEDED BY EASA AD 2019-0256

EASA Airworthiness Directive 2017-0221R1 is a regulatory update affecting ATR 42-200, ATR 42-300, and ATR 42-320 aeroplanes. It mandates compliance with Revision 8 of the ATR42-200/-300/-320 Time Limits Document, which includes updated certification maintenance requirements and airworthiness limitations. This directive ensures continued airworthiness by enforcing life limits and maintenance tasks for these aircraft models.

Dec 15, 2017

Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR 42-200ATR 42-300ATR 42-320

EASA AD 2017-0222R1

SUPERSEDED BY EASA AD 2020-0136

EASA Airworthiness Directive 2017-0222R1 is an amendment affecting ATR 42-400 and ATR 42-500 aeroplanes. It mandates compliance with updated airworthiness limitations and certification maintenance requirements as specified in the ATR42-400/-500 Time Limits Document Revision 11 Temporary revision 01. This directive ensures continued airworthiness by enforcing replacement of life-limited parts and adherence to maintenance tasks.

Dec 15, 2017

Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR 42-400ATR 42-500

EASA AD 2017-0244

Wings — Outer Wing Box Upper Rib Feet — Inspection

EASA Airworthiness Directive 2017-0244 is an inspection directive applicable to ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, and ATR 42-500 aeroplanes. It mandates repetitive detailed visual inspections of the outer wing box upper rib feet and upper skin between ribs 24 and 29 to detect cracks that could compromise structural integrity. The directive includes requirements for corrective repairs if discrepancies are found.

Dec 7, 2017

Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR 42-200ATR 42-300ATR 42-320ATR 42-400ATR 42-500

EASA SIB NM-10-18

ATR42 and ATR72 aeroplanes - Flight Data Recorder (FDR) Redesigned Aileron Sensors

The FAA Special Airworthiness Information Bulletin SAIB: NM-10-18 provides information regarding redesigned aileron sensors for the Flight Data Recorder (FDR) installed on ATR - GIE Avions de Transport Regional Model ATR42 and ATR72 airplanes. This bulletin addresses issues found with the left aileron surface position data recorded by the FDR on these aircraft models. The document is informational and does not mandate compliance.

Mar 9, 2010

Safety Information BulletinMaintenanceSafety MgmtATR ATR42ATR ATR72

EASA SIB NM-10-13

Honeywell FMZ-2000/IC-615/IC-800/IC-1080 and NZ-2000 Primus Epic FMS software

The FAA Special Airworthiness Information Bulletin SAIB: NM-10-13 provides information regarding the Honeywell FMZ-2000/IC-615/IC-800/IC-1080 and NZ-2000 Primus Epic Flight Management System (FMS) software. It identifies specific part numbers of the software installed on various aircraft models including ATR42, multiple Cessna models, Bombardier CL-600 series, Dassault Falcon variants, Embraer EMB and ERJ series, Gulfstream G series, Hawker Beechcraft Model 4000, Lockheed Martin Model 382G, and Boeing 727 airplanes. The bulletin addresses the transmission of incorrect navigation information during RNAV procedures.

Jan 8, 2010

Safety Information BulletinSafety MgmtATR ATR42Cessna 525Cessna 560XLCessna 750Bombardier CL-600Bombardier CL-601Bombardier CL-604Dassault Falcon 2000Dassault Falcon 900Dassault Falcon 7XEmbraer EMB 135Embraer EMB 145Embraer ERJ 135Embraer ERJ 145Gulfstream G100Gulfstream G150Gulfstream G200Hawker Beechcraft Model 4000Lockheed Martin 382GBoeing 727