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 2020-0130

Jun 8, 2020

Landing Gear — Main Landing Gear Torque Link Apex Pin — Replacement / Inspection

EASA Airworthiness Directive 2020-0130 is an airworthiness directive addressing the replacement and inspection of the main landing gear torque link Apex pins on Airbus A318, A319, A320, and A321 aeroplanes. The directive targets specific parts identified by part number 201383606 and serial numbers listed in Airbus Alert Operators Transmission A32N018-20 Revision 01. It aims to ensure continued airworthiness by mitigating risks associated with torque link pin failures.

Airworthiness Directive

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD TCD-4753B-2020

Jun 5, 2020

AFM Limitations Change - Pilot Training - Icing Conditions

Japan Civil Aviation Bureau Airworthiness Directive No. TCD-4753B-2020 mandates new pilot training requirements for Mitsubishi Model MU-2B and MU-2B-30 series airplanes when operating in known or forecast icing conditions. This directive updates the Airplane Flight Manual (AFM) Limitations Section to require pilots-in-command to have completed specific Mitsubishi Icing Awareness Training. The directive aims to enhance flight safety by reducing icing-related incidents caused by pilot error.

Airworthiness Directive

Mitsubishi Heavy Industries MU-2B (Japan production)
Mitsubishi MU-2B30

EASA AD 2020-0131

Jun 5, 2020

Equipment / Furnishings — Hoist Cable Cutter Frame — Modification

EASA Airworthiness Directive 2020-0131 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Leonardo S.p.A. AB139 and AW139 helicopters. It addresses the hoist cable cutter frame installed on single and double hoist control panels with specific part numbers. The directive mandates a modification to prevent inadvertent activation of the hoist cable cutter during night operations.

Airworthiness Directive

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

EASA AD 2020-0129

Jun 5, 2020

Pneumatic — Overheat Detection System / Insulation Mufflers — Modification / Replacement

EASA Airworthiness Directive 2020-0129 is an airworthiness directive affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses issues with the pneumatic overheat detection system and insulation mufflers, specifically requiring modification or replacement of affected bleed air insulation mufflers and sleeves installed in wings, pylons, and certain pneumatic tubing. This directive ensures continued airworthiness by mandating compliance with updated service bulletins.

Airworthiness Directive

Airbus A380

EASA AD 2020-0127

Jun 4, 2020

Ice and Rain Protection — Wing Anti-Ice Outboard Flexible Hoses — Inspection

EASA Airworthiness Directive 2020-0127 is an airworthiness directive addressing the inspection of wing anti-ice outboard flexible hoses on Dassault Aviation Falcon 10 aeroplanes. It applies to all serial numbers of Falcon 10 aircraft and focuses on inspecting and replacing damaged wing anti-ice flexible hoses with part number 115S018A315. The directive also introduces a new serviceable hose part number 115S118A319 with a defined life limit.

Airworthiness Directive

Dassault Falcon 10

EASA AD 2020-0128

Jun 4, 2020

Tail Rotor — Tail Rotor Duplex Bearing and Plug — Inspection

EASA Airworthiness Directive 2020-0128 is an airworthiness directive addressing inspection requirements for the tail rotor duplex bearing and plug on Leonardo S.p.A. A119 and AW119MKII helicopters. It applies to helicopters with manufacturer serial numbers up to 14972, excluding certain serial numbers, and focuses on inspecting and correcting issues related to the tail rotor pitch change mechanism components.

Airworthiness Directive

Leonardo S.P.A. Helicopters A109
Leonardo S.P.A. Helicopters A119
Leonardo A119
Leonardo AW119MKII

EASA SIB AIR-20-10

Jun 3, 2020

FAA AD 2020-03-16 Alternative Methods of Compliance and FAQ

FAA AD 2020-03-16 Alternative Methods of Compliance and FAQ is a Special Airworthiness Information Bulletin providing information on four alternative methods of compliance (AMOCs) related to FAA Airworthiness Directive 2020-03-16. This directive affects Textron Aviation Inc. Models 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, and T210M airplanes and addresses inspections and corrosion issues on the carry-thru spar lower cap. The bulletin also answers frequently asked questions about the AD and compliance options.

Safety Information Bulletin

EASA AD 2020-0126

Jun 3, 2020

Flight Controls — Flap Drive Struts and Lever Bearing Assemblies — Inspection

EASA Airworthiness Directive 2020-0126 is an airworthiness directive issued for Airbus A350-1041 aeroplanes. It mandates inspections of the flap drive struts and lever bearing assemblies at flap station 3 on both right-hand and left-hand sides to detect wear and corrosion. This directive aims to prevent potential flap detachment during flight by ensuring the structural integrity of these components.

Airworthiness Directive

Airbus A3501041

EASA AD BR-2020-05-03

Jun 2, 2020

Aircraft Flight Manual - Operational Envelope Temperature / Minimum Airspeed Limitation - Amendment

The Aircraft Flight Manual - Operational Envelope Temperature / Minimum Airspeed Limitation - Amendment is a Brazilian Airworthiness Directive (AD No. 2020-05-03) issued by ANAC that applies to Embraer EMB-500 and EMB-505 aircraft equipped with PW617F-E, PW617F1-E, or PW535E engines. It addresses operational limitations related to static air temperatures below -54°C to ensure safe aircraft operation within the approved flight envelope.

Airworthiness Directive

Embraer EMB-500 (Phenom 100)
Embraer EMB-505 (Phenom 300)
Embraer EMB-500
Embraer EMB-505

EASA AD 2020-0125

Jun 2, 2020

Aircraft Flight Manual Section Limitations — Amendment

EASA Airworthiness Directive 2020-0125 is an amendment addressing flight control law limitations on Airbus A320neo aircraft models A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, and A320-273N. It mandates updates to the Aircraft Flight Manual (AFM) to incorporate temporary revisions or later AFM revisions that include new center of gravity (CG) envelopes enabled by Airbus modification 163923. This directive aims to ensure safe operation by limiting flight configurations that could reduce angle of attack protection efficiency.

Airworthiness Directive

Airbus A320
Airbus A320neo

EASA AD 2019-0171R2

Jun 2, 2020

Aircraft Flight Manual Section Limitations — Amendment

EASA Airworthiness Directive 2019-0171R2 is an amendment addressing Airbus A321neo aircraft equipped with specific Elevator Aileron Computer (ELAC) units. It mandates changes to the Aircraft Flight Manual (AFM) limitations to mitigate reduced angle of attack protection caused by certain ELAC software versions. The directive applies to various A321neo models except those with Airbus modification 163923 installed in production.

Airworthiness Directive

Airbus A321
Airbus A321neo

EASA SIB 2020-09

May 29, 2020

CEAPR DR 400 Aeroplanes - Defective Seat Belt Attachment Rivet Assembly

EASA Safety Information Bulletin 2020-09 is a safety information bulletin addressing a defective seat belt attachment rivet assembly in CEAPR DR 400 aeroplanes. The affected models include DR 400/100, DR 400/120, DR 400/140 B, DR 400/160, DR 400/180, and DR 400/180 R with specific serial numbers from 2703 to 2734. The bulletin provides guidance on inspection and corrective actions related to the rivet assembly holding the front seat belt retractor.

Safety Information Bulletin

EASA SIB 2020-10

May 29, 2020

CEAPR DR 400 Aeroplanes - Defective Warning Lights Panel

EASA Safety Information Bulletin 2020-10 is an airworthiness bulletin addressing defective warning lights panels on CEAPR DR 400 series aeroplanes, specifically models DR 400/100, DR 400/120, DR 400/140 B, DR 400/160, DR 400/180, and DR 400/180 R with certain serial numbers. The bulletin informs operators about a wiring defect that may cause a short circuit during the warning lights test when the pitot heater is on. It provides guidance on inspection and corrective actions via CEAPR Service Bulletin 190902.

Safety Information Bulletin

EASA AD 2020-0124

May 29, 2020

Engine Fuel and Control – Fuel Pump – Replacement [Life Limitation]

EASA Airworthiness Directive 2020-0124 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Rolls-Royce Trent 1000-D2, Trent 1000-J2, and Trent 1000-K2 engines, commonly installed on Boeing 787 aircraft. The directive addresses fuel pump life limitations due to wear-related performance degradation. It mandates replacement of affected fuel pumps to maintain engine performance and safety.

Airworthiness DirectiveSuperseded

Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
Boeing 787

EASA AD 2020-0122

May 29, 2020

Equipment / Furnishings — Overhead Stowage Compartment Fixation Brackets — Inspection

EASA Airworthiness Directive 2020-0122 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-271N, A321-211, and A321-271N aeroplanes with specific manufacturer serial numbers. The directive addresses the inspection of overhead stowage compartment X-fixation brackets to ensure their correct installation and presence. It mandates a one-time detailed inspection to prevent potential overhead stowage compartment failure that could cause passenger injury.

Airworthiness Directive

Airbus A320
Airbus A321

EASA AD 2020-0123

May 29, 2020

Wings – Centre Wing Box Fasteners – Replacement

EASA Airworthiness Directive 2020-0123 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes, except those with Airbus modification 109799 incorporated in production. The directive addresses an unsafe condition related to the rotation of certain fasteners in the centre wing box, which could lead to fuel vapour leakage inside the cabin. This directive mandates the replacement of affected fasteners with improved friction material fasteners to ensure continued airworthiness.

Airworthiness DirectiveSuperseded

Airbus A350941

EASA AD 2020-0121

May 28, 2020

Flight Controls – elevator Control Pushrod – Inspection / Replacement

EASA Airworthiness Directive 2020-0121 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting various Grob sailplanes including ASTIR CS series, CLUB ASTIR II, TWIN ASTIR models, and G 103 series powered and unpowered sailplanes. The directive addresses the inspection and potential replacement of the elevator control pushrod in the vertical fin to prevent corrosion-related failures. This AD applies to all serial numbers of the specified models and mandates inspection procedures defined by Fiberglas-Technik R. Lindner GmbH & Co. KG.

Airworthiness DirectiveSuperseded

E Aerospace Fischer Gmbh ASTIR CS TOP
Fiberglas Technik R. Lindner Grob Sailplanes
Grob ASTIR CS
Grob CLUB ASTIR II
Grob TWIN ASTIR
Grob G 103

EASA AD 2020-0097R1

May 28, 2020

Fuselage – Passenger Seat Tracks – Inspection / Repair / Replacement

EASA Airworthiness Directive 2020-0097R1 is an updated directive addressing inspection and potential repair or replacement of passenger seat tracks on ATR 42 and ATR 72 aeroplanes. It applies to specific seat track part numbers manufactured between 2012 and 2017 and targets certain serial number ranges of ATR 42 and ATR 72 aircraft. The directive aims to ensure the structural integrity of seat tracks to prevent failure during emergency landings.

Airworthiness DirectiveSuperseded

ATR ATR42
ATR ATR72
ATR 42
ATR 72

EASA AD 2020-0112R1

May 27, 2020

Fuselage – Structure, Windshield Frame and Closing Panel / Circumferential Junction Areas – Inspections

EASA Airworthiness Directive 2020-0112R1 is an updated directive addressing structural inspections on Airbus A310 aeroplanes. It mandates repetitive special detailed inspections of specific fuselage areas, including the windshield frame and circumferential junctions, to detect cracks that could compromise structural integrity. This directive applies to all certified Airbus A310 models and serial numbers.

Airworthiness DirectiveSuperseded

Airbus A310

EASA AD 2020-0110R1

May 27, 2020

Fuselage – Structure, Windshield Frame and Closing Panel / Skin Lap Joint / Centre Wing Bottom Skin – Inspection

EASA Airworthiness Directive 2020-0110R1 is an updated directive addressing structural inspections on Airbus A300 aeroplanes of all certified models and manufacturer serial numbers. It mandates repetitive special detailed inspections of specific fuselage areas including the windshield frame, skin lap joint, and centre wing bottom skin to detect cracks that could compromise structural integrity. This directive applies to various groups of A300 aircraft differentiated by embodied Airbus modifications and service bulletins.

Airworthiness DirectiveSuperseded

Airbus A300