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EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350224 Airbus A330221 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941134 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787116 Show all...

EASA AD US-2019-02-03

Superseded by FAA AD 2021-02-06

FAA Airworthiness Directive 2019-02-03 is a final rule affecting all Boeing 787-8, 787-9, and 787-10 airplanes. It mandates revisions to the existing maintenance or inspection programs to incorporate new or more restrictive airworthiness limitations related to internal engine fire handle components. This directive addresses a latent failure risk that could prevent proper engine fire handle operation.

Airworthiness Directive

Boeing 7878910

EASA AD CF-2019-04

Cold Weather Operations — Introduction of Low Temperature Ground Wing Anti-Ice System

The Canadian Airworthiness Directive CF-2019-04 titled 'Cold Weather Operations — Introduction of Low Temperature Ground Wing Anti-Ice System' applies to Bombardier Inc. CL-600-2A12 (Challenger 601) and CL-600-2B16 (Challenger 601-3A/3R) aircraft with serial numbers 3001 to 3066 and 5001 to 5194. This directive mandates modifications to improve safety during cold weather ground operations by introducing a low temperature ground wing anti-ice system. It includes updates to flight manuals, maintenance schedules, and installation of the new anti-ice system.

Airworthiness Directive

Bombardier CL-600 (Challenger)
Bombardier CL-600-2A12
Bombardier CL-600-2B16

EASA AD CF-2015-28R2

Equipment / Furnishings — Damaged Decompression Window Louver Panel Assemblies and Detached Blowout Panels

Airworthiness Directive CF-2015-28R2 addresses damaged decompression window louver panel assemblies and detached blowout panels on Bombardier Inc. aeroplanes, specifically models CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 configured with a Class C Cargo Compartment. This directive mandates inspections and corrective actions to ensure the integrity of cargo compartment components that are critical for smoke detection and fire suppression. The directive updates maintenance requirements to prevent uncontrolled cargo compartment fires.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD 2019-0028

Flight Controls — Flight Control Primary Computer — Modification / Replacement

EASA Airworthiness Directive 2019-0028 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643 aeroplanes equipped with certain Flight Control Primary Computer (FCPC) software standards. The directive mandates modification or replacement of the FCPC software to newer standards to enhance Angle of Attack (AOA) blockage detection. It also allows removal of a previously required operational procedure from the Aircraft Flight Manual once the modification is completed.

Airworthiness Directive

Airbus A340211212213311312313541542642643

EASA AD 2018-0259R1

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 2014-0159R1

Fuselage — 9Â° Frame — Inspection

EASA Airworthiness Directive 2014-0159R1 is an updated safety directive addressing inspection requirements for the 9° frame on Airbus Helicopters SA 365 and AS 365 models, including SA 365 N, N1, and AS 365 N2 and N3 variants. The directive mandates repetitive inspections to detect cracks that could compromise structural integrity and requires corrective actions or modifications as necessary. This AD applies to all serial numbers except those with a specific Airbus Helicopters modification embodied in production.

Airworthiness Directive

Airbus Helicopters SA
Airbus Helicopters AS 365
Airbus Helicopters EC 155
Airbus Helicopters SA 365

EASA AD 2014-0162R2

Fuselage — 9Â° Upper Frame — Inspection

EASA Airworthiness Directive 2014-0162R2 is an updated safety directive addressing inspection requirements for the 9° upper frame on Airbus Helicopters SA 365 and AS 365 models, including SA 365 N, N1, and AS 365 N2 and N3 variants. The directive mandates repetitive inspections to detect cracks in the upper part of the 9° frame to prevent structural failure. It applies to all serial numbers except those with modification 07 53D21 incorporated during production.

Airworthiness Directive

Airbus Helicopters SA
Airbus Helicopters AS 365
Airbus Helicopters EC 155
Airbus Helicopters SA 365

EASA AD 2016-0208R1

Fuselage — Structural Parts / Joints — Modification / Reinforcement

EASA Airworthiness Directive 2016-0208R1 is a regulatory update addressing structural modifications and reinforcements for Airbus A340 series aeroplanes, including models A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643. The directive mandates modifications to fuselage structural parts and joints to prevent widespread fatigue damage that could compromise aircraft integrity and safety.

Airworthiness Directive

Airbus A340211212213311312313541542642643

EASA AD 2019-0024

Airworthiness Limitation Section – TT-Straps – Storage Life Limit

EASA Airworthiness Directive 2019-0024 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters Deutschland GmbH BO105 helicopter models including BO105 A, C, D, S, and LS A-3 variants. The directive addresses the storage life limits and service life of specific Bendix and Lord Tension Torsion (TT) straps used in these helicopters to ensure continued airworthiness and safety.

Airworthiness DirectiveSuperseded

Airbus Helicopters BO 105
Airbus Helicopters BO105

EASA AD US-2019-01-01

[Correction] Powerplant - Airplane Flight Manual Revision

The Correction to Airworthiness Directive 2019-01-01 is a final rule issued by the Federal Aviation Administration (FAA) that applies to Boeing 787-8 airplanes powered by Rolls-Royce Trent 1000 series turbofan engines. This correction addresses an error in the original directive related to the identification of a referenced Rolls-Royce service bulletin. The directive requires revising the airplane flight manual to limit extended operations (ETOPS) for the affected aircraft and engines.

Airworthiness Directive

Boeing 7878

EASA AD 2019-0021

[Correction] Rotorcraft Flight Manual / Emergency Procedures — Amendment ; Navigation — Attitude and Heading Reference System — Modification

The [Correction] Rotorcraft Flight Manual / Emergency Procedures — Amendment ; Navigation — Attitude and Heading Reference System — Modification is a regulatory document affecting AIRBUS HELICOPTERS models SA 330, AS 332, and EC 225. It addresses corrections and modifications related to the rotorcraft flight manual emergency procedures and updates to the navigation system, specifically the attitude and heading reference system. This amendment ensures updated operational guidance and system modifications for these helicopter types.

Airbus Helicopters SA 330
Airbus Helicopters AS 332
Airbus Helicopters EC 225

EASA AD 2019-0022

[Correction] Tail Rotor — Duplex Bearings — Replacement

EASA Airworthiness Directive 2019-0022 is a corrective directive addressing the replacement of tail rotor duplex bearings on Leonardo S.p.A. AB139, AW139, AW169, and AW189 helicopters. The directive targets specific part numbers and serial numbers of tail rotor duplex bearings identified as potentially defective due to a quality non-conformity. It mandates replacement of affected bearings to ensure continued airworthiness and safe operation of the helicopters.

Airworthiness Directive

Leonardo S.P.A. Helicopters AB139
Leonardo S.P.A. Helicopters AW139
Leonardo S.P.A. Helicopters AW169
Leonardo S.P.A. Helicopters AW189
Leonardo AB139
Leonardo AW139
Leonardo AW169
Leonardo AW189

EASA AD 2019-0027

Oxygen – Oxygen Crew and Courier Distribution System Flexible Hoses – Inspection / Replacement

EASA Airworthiness Directive 2019-0027 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330-223F and A330-243F freighter aeroplanes. It addresses the inspection and replacement of flexible hoses in the Oxygen Crew and Courier Distribution System (OCCDS) to prevent oxygen leakage. The directive mandates repetitive detailed inspections and functional testing of specific part numbers of flexible hoses and requires replacement if any damage or leakage is found.

Airworthiness DirectiveSuperseded

Airbus A330223F243F

EASA AD 2019-0025

Time Limits / Maintenance Checks - Airworthiness Limitations Section - Amendment

EASA Airworthiness Directive 2019-0025 is an amendment concerning the Hélicoptères Guimbal Cabri G2 helicopters. It mandates compliance with updated airworthiness limitations defined in the latest Maintenance Manual issue 06, including new and more restrictive maintenance tasks and life limits. This directive ensures continued airworthiness by requiring operators to follow the approved Aircraft Maintenance Programme incorporating these updated limitations.

Airworthiness Directive

Guimbal, Helicopteres CABRI
Hélicoptères Guimbal Cabri G2

EASA AD RU-2018-322-07

Wings - Lower Rear Panel of the Center Wing - Inspection

Airworthiness Directive 2018-322-07 from the Federal Air Transport Agency of the Russian Federation mandates inspection of the lower rear panel of the center wing on RRJ-95 aircraft. This directive addresses detected cracks in the rib of the left-hand longitudinal beam part number T7.92.1000.006.000.73. It requires a one-time detailed inspection during the next periodic maintenance and outlines reporting and follow-up procedures.

Airworthiness Directive

Irkut Corporation Jsc RRJ-95
RRJ-95

EASA AD 2019-0026

Wings — Slat Tracks Number 10 — Inspection / Replacement

EASA Airworthiness Directive 2019-0026 is an airworthiness directive addressing Airbus A330 and A340 aeroplanes. It focuses on the inspection and replacement of wing slat tracks number 10 installed on Slat 4 on both left and right sides, specifically parts with part numbers F574-64110-000 or F574-64110-002. The directive mandates inspections and replacement to ensure continued airworthiness and safety.

Airworthiness Directive

Airbus A330
Airbus A340

EASA AD DCA-750XL-35

Engine Mount Chafing — Inspection

Airworthiness Directive DCA/750XL/35 Engine Mount Chafing – Inspection is issued by the Civil Aviation Authority of New Zealand and applies to Pacific Aerospace Limited 750XL aircraft with serial numbers 101 through 215, 220, and 8001, 8002. This directive mandates inspection and preventive measures to address potential chafing damage involving the engine mount, Beta control rod, and inter-turbine temperature sensing probe. The directive references compliance with Pacific Aerospace Mandatory Service Bulletin PACSB/XL/102 issue 2 or later revisions.

Airworthiness Directive

Nzskydive 750XL
Pacific Aerospace 750XL

EASA AD CF-2009-11R3

Failure of the Main Landing Gear Stabilizer Braces

Airworthiness Directive CF-2009-11R3 addresses the failure of the main landing gear stabilizer braces on Bombardier Inc. DHC-8-400, -401, and -402 aircraft, serial numbers 4001, 4003 and subsequent, equipped with main landing gear forward stabilizer brace part number 46401-7. This directive mandates inspections, corrective actions, and installation of an elbow restrictor to prevent potential collapse of the main landing gear due to fatigue cracks. The directive is issued by Transport Canada under Canadian Aviation Regulation 521.427.

Airworthiness Directive

De Havilland Canada DHC-8
Bombardier DHC-8-400

EASA AD DCA-750XL-36

Fuel Pickup Assembly and Wing Spar Web — Inspection

Airworthiness Directive DCA/750XL/36 Fuel Pickup Assembly and Wing Spar Web – Inspection is issued by the Civil Aviation Authority of New Zealand for Pacific Aerospace Limited 750XL aircraft, specifically serial numbers 177, 186 through 213, 220, 8001, and 8002. This directive mandates inspection of the fuel pickup assembly and wing spar web to detect cracks that may arise from a pre-stressed installation condition. The directive references Pacific Aerospace Mandatory Service Bulletin PACSB/XL/109 issue 1 dated 16 January 2019 for inspection and corrective actions.

Airworthiness Directive

Nzskydive 750XL
Pacific Aerospace 750XL

EASA AD DCA-750XL-34

Port Wing Internal Tank Abrasion — Inspection

Airworthiness Directive DCA/750XL/34 is issued by the Civil Aviation Authority of New Zealand and applies to Pacific Aerospace Limited 750XL aircraft, serial numbers 100 through 213 (excluding 206) and 8001. This directive mandates inspection and potential repair of the port wing internal tank to address abrasion caused by fuel finger filters. The directive aims to prevent fuel leaks due to chafing damage in the wing skin.

Airworthiness Directive

Nzskydive 750XL
Pacific Aerospace 750XL