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EASA Regulations & Airworthiness Directives

Browse 4995 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320280Airbus A321276Airbus A319246Airbus A350214Airbus A330210All194Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941125Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332116Airbus Helicopters EC 225113Airbus Helicopters SA 330113Show all...

EASA AD 2020-0113

SUPERSEDED BY EASA AD 2022-0135

EASA Airworthiness Directive 2020-0113 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Falcon 2000 aeroplanes. It mandates compliance with the updated airworthiness limitations specified in Chapter 5-40, Revision 21, of the Dassault Falcon 2000 Aircraft Maintenance Manual. This directive ensures the continued airworthiness of these aircraft by enforcing maintenance tasks and life limits.

May 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 2000

EASA AD 2020-0114

SUPERSEDED BY EASA AD 2022-0136

EASA Airworthiness Directive 2020-0114 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Falcon 2000EX aeroplanes. It mandates compliance with the updated airworthiness limitations section in the Dassault Falcon 2000EX Aircraft Maintenance Manual, Chapter 5-40, Revision 13. This directive ensures the continued airworthiness of the Falcon 2000EX fleet by enforcing mandatory maintenance tasks and life limits.

May 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 2000Dassault Falcon 2000EX

EASA AD 2020-0115

SUPERSEDED BY EASA AD 2022-0137

EASA Airworthiness Directive 2020-0115 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Mystère-Falcon 900 aeroplanes. It mandates compliance with the updated airworthiness limitations detailed in Chapter 5-40, Revision 25, of the Dassault Mystère-Falcon 900 Aircraft Maintenance Manual. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components on these aircraft.

May 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtDassault Mystère-Falcon 900Dassault Mystère-Falcon 900

EASA AD 2020-0117

SUPERSEDED BY EASA AD 2022-0141

EASA Airworthiness Directive 2020-0117 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Falcon 900EX aeroplanes, including the Falcon 900EX Easy, Falcon 900LX, and Falcon 900DX variants. It mandates compliance with updated airworthiness limitations specified in the Dassault Falcon 900EX Easy/900LX/900DX Aircraft Maintenance Manual, Chapter 5-40, Revision 12. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components on these aircraft.

May 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 900EXDassault Falcon 900EX EasyDassault Falcon 900LXDassault Falcon 900DX

EASA AD 2020-0116

SUPERSEDED BY EASA AD 2022-0144

EASA Airworthiness Directive 2020-0116 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Falcon 900EX aeroplanes, specifically serial numbers 1 to 119 except 97. It mandates compliance with updated airworthiness limitations published in Revision 17 of the Falcon 900EX Aircraft Maintenance Manual, Chapter 5-40. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components.

May 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 900EX

EASA AD CF-2020-16

Cabin Pressure Control System - Safety Valve — Overtorque

The Canadian Airworthiness Directive CF-2020-16 titled "Cabin Pressure Control System - Safety Valve — Overtorque" addresses Bombardier BD-700-1A10 and BD-700-1A11 aircraft with specific serial numbers. It mandates inspection and corrective actions for the safety valves (part number GG435-3006-3) in the cabin pressure regulation system due to potential overtorque issues during installation. This directive ensures the integrity of the cabin pressure system by preventing possible leaks or depressurization.

May 19, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700Bombardier BD-700-1A10Bombardier BD-700-1A11

EASA SIB CE-20-09

M7 Aerospace SA227 Aeroplanes - Nacelle Keelson Webs and Surrounding Structural Areas - Inspection

The Special Airworthiness Information Bulletin SAIB CE-20-09 is an FAA information bulletin addressing an airworthiness concern for M7 Aerospace LLC Models SA227 airplanes. It focuses on inspection of the nacelle keelson webs and surrounding structural areas for cracks, damage, buckling, or wrinkles. This bulletin applies to all serial numbers of the SA227 aircraft under Type Certificate Data Sheets A5SW, A8SW, and A18SW.

May 18, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0170R1

Fuselage — Belly Fairing Panel Support Structure — Inspection

EASA Airworthiness Directive 2019-0170R1 is an updated regulatory requirement addressing inspection and repair of the forward belly fairing panel support structure on Airbus A380-841, A380-842, and A380-861 aircraft. It mandates repetitive detailed inspections for corrosion on specific structural profiles and introduces optional modification instructions to prevent corrosion. This directive applies to all serial numbers except those with Airbus modifications 75498 or 77715 incorporated during production.

May 15, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2020-0109

Fuselage — Frame 98 Flange Feet between Stringers 15 and 17 — Inspection / Modification

EASA Airworthiness Directive 2020-0109 is an airworthiness directive issued by EASA affecting Airbus A350-941 aeroplanes, except those with Airbus modification 114295 incorporated in production. It mandates inspection and potential modification of the fuselage frame 98 flange feet between stringers 15 and 17 to ensure structural integrity. The directive addresses potential fatigue and damage tolerance issues in the rear cone of the fuselage.

May 15, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD 2020-0108

Equipment / Furnishings — Emergency Locator Transmitter — Modification

EASA Airworthiness Directive 2020-0108 is an official regulatory document addressing a safety issue on Airbus A300-600 and A310 aeroplanes. It specifically targets Emergency Locator Transmitters (ELTs) with Part Number 01N65900 installed on these aircraft models. The directive mandates modifications to improve protection against electrical current injection that could cause battery fires.

May 14, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A310

EASA AD CF-2020-15

Tail Rotor Drive — Failure of Tail Rotor Drive Shaft Coupling Bolted Connections

Canadian Airworthiness Directive CF-2020-15 addresses the failure risk of tail rotor drive shaft coupling bolted connections on Bell Textron Canada Limited model 206 series helicopters, including 206, 206A, 206B, and 206L variants. The directive mandates replacement of certain MS21042-series nuts with more reliable NAS9926-series nuts or alternate parts to prevent loss of tail rotor drive and potential loss of helicopter control. It also covers specific configurations affected by Supplemental Type Certificates SH2750NM and SH99-202 and provides tailored corrective actions for different helicopter groups.

May 14, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAir Comm Corporation CAA UK AAN 25273Bell 206Bell 206ABell 206BBell 206L

EASA AD US-2020-10-04

Engine - Interstage High-Pressure Turbine Rotor Seal - Inspection / Replacement

The document titled "Engine - Interstage High-Pressure Turbine Rotor Seal - Inspection / Replacement" is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2020-10-04) addressing General Electric Company GE90-110B1 and GE90-115B turbofan engines. It mandates inspections and potential replacement of the interstage high-pressure turbine (HPT) rotor seal to prevent unsafe conditions. The directive applies specifically to these engine models installed on Boeing 777-300ER aircraft.

May 13, 2020
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric GE90Boeing 777-300ER

EASA AD 2020-0106

Equipment / Furnishings — Light Cover / Oxygen Container Gap Seal — Modification

EASA Airworthiness Directive 2020-0106 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes, except those with Airbus modification 78554 incorporated in production. The directive addresses an issue with gap seals between light covers and passenger service unit oxygen container lids on the main deck. It mandates a modification to ensure proper functioning of oxygen container lids.

May 12, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA SIB CE-20-10

Textron Aviation Inc. Hawker 750, 800, 800XP, 850XP and 900XP Airplanes - Air Distribution System - Loss of Cabin Pressure

The Special Airworthiness Information Bulletin SAIB: CE-20-10 is an FAA information bulletin addressing a potential loss of cabin pressure issue in Textron Aviation Inc. Hawker 750, 800, 800XP, 850XP, and 900XP series airplanes. It highlights reports of sudden disconnections in the air distribution system ducts and sleeves that can cause rapid cabin altitude changes. This bulletin is informational and does not mandate corrective action under 14 CFR part 39.

May 12, 2020
Safety Information BulletinSafety MgmtMaintenance

EASA AD 2020-0105

Rotors Flight Control — Main Rotor Actuator Single-Axis Actuators — Inspection / Replacement

EASA Airworthiness Directive 2020-0105 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters Deutschland GmbH EC135 and EC635 helicopter models. It addresses inspection and replacement requirements for main rotor actuator single-axis actuators with specific part numbers to ensure continued airworthiness and flight safety. The directive applies to all variants and serial numbers of the affected helicopter models.

May 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC135Airbus Helicopters 635Airbus Helicopters EC635

EASA SIB 2020-08

[Correction] DECOMATIC Titanium Bolts

EASA Safety Information Bulletin 2020-08 is a correction notice regarding DECOMATIC titanium bolts manufactured between May and December 2013. These bolts, identified by specific part numbers listed in the bulletin, were produced with an improper heat treatment process that may cause hydrogen embrittlement leading to premature failure. The bulletin applies to all aeronautical products using these affected bolts and aims to raise awareness among manufacturers, maintenance organizations, and operators.

May 8, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0103

[Correction] Equipment / Furnishings — Emergency Locator Transmitter Protection — Modifications

EASA Airworthiness Directive 2020-0103 is a correction issued by the European Union Aviation Safety Agency concerning Airbus A318, A319, A320, and A321 aeroplanes. It addresses modifications related to the Emergency Locator Transmitter (ELT) protection, specifically targeting ELTs with Part Number 01N65900. The directive mandates modifications to improve ELT battery current injection protection to prevent potential battery fires.

May 8, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB SAFO20007

AmSafe, Inc. Airbag System—s Electronic Module Assembly - Damage or Loose Installation

SAFO 20007 is a Safety Alert for Operators issued by the FAA regarding the AmSafe, Inc. Airbag System’s Electronic Module Assembly (EMA). It addresses potential hazards caused by damage or loose installation of the EMA, EMA bracket, or EMA housing, which can lead to inadvertent airbag deployment. This alert is relevant to all aircraft equipped with the AmSafe seatbelt airbag system.

May 7, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0102

Rotors Flight Control — Tail Rotor Control System — Inspection

EASA Airworthiness Directive 2020-0102 is an airworthiness directive addressing the tail rotor control system inspection for Airbus Helicopters Deutschland GmbH EC135 and EC635 models, including various subtypes up to serial number 1276. It mandates inspections of the tail rotor control system to ensure safety after hard landings and to prevent potential control failures. The directive applies to all affected EC135 and EC635 helicopters as specified.

May 6, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC135Airbus Helicopters 635Airbus Helicopters EC635

EASA AD 2020-0101

Landing Gear — Main Landing Gear Hinge Pins — Replacement

EASA Airworthiness Directive 2020-0101 is issued for ATR 72 series aeroplanes, specifically models ATR 72-101, -102, -201, -202, -211, -212, and -212A. It addresses the replacement of main landing gear hinge pins with part numbers D61000 and D60999 that have been identified as potentially thermally abused during production. This directive mandates the replacement of affected hinge pins to ensure continued airworthiness and prevent structural failure of the main landing gear.

May 5, 2020
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR72ATR 72