EASA Regulations for ATR ATR42

70 airworthiness directives and regulations affecting ATR ATR42.

EASA AD 2019-0256

Oct 17, 2019

Time Limits / Maintenance Checks – Certification Maintenance Requirements and Airworthiness Limitations – Amendment

EASA Airworthiness Directive 2019-0256 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting ATR 42-200, ATR 42-300, and ATR 42-320 aeroplanes. It mandates compliance with updated airworthiness limitations and certification maintenance requirements as specified in the ATR 42-200/-300/-320 Time Limit Document Revision 09. This directive ensures continued safe operation by enforcing life limits and maintenance tasks for these aircraft models.

Airworthiness DirectiveSuperseded
  • ATR ATR42
  • ATR 42-200
  • ATR 42-300
  • ATR 42-320

EASA AD 2019-0111

May 21, 2019

Oxygen – Crew and Passenger Oxygen Cylinders – Inspection /; Replacement

EASA Airworthiness Directive 2019-0111 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning ATR 42 and ATR 72 aeroplanes. It addresses oxygen cylinders with Part Number 89794077 that may have a manufacturing defect leading to oxygen leakage. The directive mandates inspection and possible replacement of affected oxygen cylinders to ensure safety.

Airworthiness DirectiveSuperseded
  • ATR ATR42
  • ATR ATR72
  • ATR 42
  • ATR 72

EASA AD 2018-0259R1

Feb 7, 2019

Information Systems – Electronic Flight Bag Universal Serial Bus Receptacle – Modification

EASA Airworthiness Directive 2018-0259R1 is an updated directive addressing safety concerns related to USB receptacles installed in various aircraft including Fokker F27 and F28 models, Airbus A318 through A340 series, ATR42 and ATR72, Boeing 737 through 777, and Bombardier CL-600 and DHC-8 aircraft. The directive mandates modifications to the affected Lone Star Aviation USB receptacle part number LS03-05050-A to prevent overheating and smoke/fumes in the cockpit. It applies to aircraft with these USB receptacles installed via Fokker Services Supplemental Type Certificates, Service Bulletins, or minor modifications.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340
  • ATR ATR42
  • ATR ATR72
  • Boeing 737
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Bombardier CL-600 (Challenger)
  • De Havilland Canada DHC-8
  • Fokker CRR-0185
  • Fokker CRR-0186
  • Fokker CRR-0190
  • Fokker CRR-0210
  • Fokker CRR-0241
  • Fokker CRR-0265
  • Fokker CRR-0300
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Fokker F27
  • Fokker F28
  • Boeing 747
  • Bombardier CL-600
  • Bombardier DHC-8

EASA AD 2018-0105

May 8, 2018

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.

Airworthiness Directive
  • ATR ATR42
  • ATR ATR72
  • ATR 42-500
  • ATR 72-212A

EASA AD 2018-0080

Apr 11, 2018

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.

Airworthiness Directive
  • ATR ATR42
  • ATR ATR72
  • ATR 42-200
  • ATR 42-300
  • ATR 42-320
  • ATR 42-400
  • ATR 42-500
  • ATR 72-101
  • ATR 72-102
  • ATR 72-201
  • ATR 72-202
  • ATR 72-211
  • ATR 72-212
  • ATR 72-212A

EASA AD 2017-0222R1

Dec 15, 2017

Time Limits / Maintenance Checks – Certification Maintenance Requirements and Airworthiness Limitations – Amendment

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.

Airworthiness DirectiveSuperseded
  • ATR ATR42
  • ATR 42-400
  • ATR 42-500

EASA AD 2017-0221R1

Dec 15, 2017

Time Limits / Maintenance Checks – Certification Maintenance Requirements and Airworthiness Limitations – Amendment

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.

Airworthiness DirectiveSuperseded
  • ATR ATR42
  • ATR 42-200
  • ATR 42-300
  • ATR 42-320

EASA AD 2017-0244

Dec 7, 2017

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.

Airworthiness Directive
  • ATR ATR42
  • ATR 42-200
  • ATR 42-300
  • ATR 42-320
  • ATR 42-400
  • ATR 42-500

EASA SIB NM-10-18

Mar 9, 2010

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.

Safety Information Bulletin
  • ATR ATR42
  • ATR ATR72

EASA SIB NM-10-13

Jan 8, 2010

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.

Safety Information Bulletin
  • ATR ATR42
  • Cessna 525
  • Cessna 560XL
  • Cessna 750
  • Bombardier CL-600
  • Bombardier CL-601
  • Bombardier CL-604
  • Dassault Falcon 2000
  • Dassault Falcon 900
  • Dassault Falcon 7X
  • Embraer EMB 135
  • Embraer EMB 145
  • Embraer ERJ 135
  • Embraer ERJ 145
  • Gulfstream G100
  • Gulfstream G150
  • Gulfstream G200
  • Hawker Beechcraft Model 4000
  • Lockheed Martin 382G
  • Boeing 727