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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 SIB SAFO20012

Continuation of Air Carrier and Other Operations in Terminal Airspace when an Air Traffic Control Facility with Responsibility for That Controlled Airspace Closes Unexpectedly

The Safety Alert for Operators SAFO 20012 titled 'Continuation of Air Carrier and Other Operations in Terminal Airspace when an Air Traffic Control Facility with Responsibility for That Controlled Airspace Closes Unexpectedly' provides guidance for air carriers and commercial operators on safely continuing operations in terminal and controlled airspace when an Air Traffic Control Tower unexpectedly ceases operations. It addresses risks associated with such closures, especially at larger airports certificated under part 139, and offers safety recommendations for flightcrews, dispatchers, and operators. The document does not specify particular aircraft or engine models.

Jul 10, 2020
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2020-0153

Fuselage — Rear Fuselage Clips, Shear Webs and Angles — Replacement

EASA Airworthiness Directive 2020-0153 is an airworthiness directive addressing the replacement of rear fuselage clips, shear webs, and angles on Airbus A319, A320, and A321 aeroplanes. It applies to specific models except those with Airbus modification 30975 embodied in production. The directive aims to ensure structural integrity by mandating replacement of affected parts identified during fatigue testing.

Jul 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2020-0154

SUPERSEDED BY EASA AD 2021-0006

EASA Airworthiness Directive 2020-0154 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Trent 1000 engines installed on Boeing 787 aircraft. The directive addresses fuel pump life limitations for specific part numbers to prevent reduced engine thrust due to fuel pump wear. It applies to multiple Trent 1000 engine variants and mandates replacement of affected fuel pumps before exceeding revised life limits.

Jul 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787

EASA AD 2020-0151-E

Engine — Module 03 / Stage 2 High Pressure Turbine Disc — Replacement

EASA Airworthiness Directive 2020-0151-E is an emergency directive addressing the replacement of Stage 2 High Pressure Turbine discs in SAFRAN Helicopter Engines ARRIEL 1B, 1C, 1C2, and 1D1 models. These engines are commonly installed on Airbus Helicopters AS 350 B series, AS 365, and SA 365 helicopters, excluding the AS 365 N3 model. The directive targets specific turbine discs with part number 0292250400 and certain serial numbers that have been identified as potentially defective.

Jul 9, 2020
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIEL 1Airbus Helicopters AS 350 BAirbus Helicopters AS 365Airbus Helicopters SA 365

EASA AD US-2020-12-10

Tail Rotor Blades - Inspection / Repair / Replacement

Airworthiness Directive 2020-12-10 is a final rule issued by the FAA addressing Bell Textron Inc. helicopters, specifically models 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP equipped with tail rotor blades part number 212-010-750. The directive focuses on inspecting these tail rotor blades for corrosion and pitting to prevent potential cracks and loss of control. It updates previous requirements by excluding certain newer tail rotor blades from inspection applicability.

Jul 9, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 205Bell Textron Inc. (Bti) 212Bell Textron Inc. (Bti) 412Bell 205ABell 205A-1Bell 205BBell 212Bell 412Bell 412CFBell 412EP

EASA AD US-2020-13-08

Engine - High Pressure Compressor Case - Inspection

The Federal Aviation Administration Airworthiness Directive 2020-13-08 is a final rule addressing General Electric Company CF6-80E1A1, -80E1A2, -80E1A3, -80E1A4, and -80E1A4/B model turbofan engines. It mandates updated inspections of the high-pressure compressor (HPC) cases, specifically parts 1509M97G07 and 2083M69G03, to enhance safety and prevent engine failures. This directive updates the Airworthiness Limitations Section of the GE Engine Manual GEK99376 and the operator's continuous airworthiness maintenance program.

Jul 8, 2020
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CF6-80E1

EASA AD 2017-0240R1

Navigation — Barometric Setting — Operational Limitations / Master Minimum Equipment List — Amendment

EASA Airworthiness Directive 2017-0240R1 is an amendment addressing barometric setting operational limitations and Master Minimum Equipment List updates for Dassault Aviation Falcon 7X, 2000EX, and 900EX aeroplanes. It applies to specific serial numbers excluding those with certain Dassault modifications or service bulletins. The directive aims to mitigate risks related to erroneous barometric settings caused by a temporary defect in the Cursor Control Device affecting flight safety.

Jul 8, 2020
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtDassault Falcon 2000Dassault Falcon 7XDassault Falcon 900EXDassault Falcon 2000EX

EASA AD 2020-0150

SUPERSEDED BY EASA AD 2022-0117

EASA Airworthiness Directive 2020-0150 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting SAFRAN Helicopter Engines RTM 322-01/9 engines, commonly installed on NH Industries NH90 military helicopters. This directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the SAFRAN RTM 322-01/9 Engine Maintenance Manual Airworthiness Limitations Section approved on 30 September 2019.

Jul 8, 2020
Airworthiness DirectiveMaintenanceSafety MgmtSafran RTM 322NH Industries NH90

EASA AD 2020-0149

Landing Gear — Nose Landing Gear Door Attachment Bolts — Replacement

EASA Airworthiness Directive 2020-0149 is an airworthiness directive addressing the replacement of nose landing gear door attachment bolts on Saab-Fairchild SF340A, SAAB 340B, and SAAB 2000 aeroplanes. The directive targets bolts with part number 7232203-041, identified by specific tracking and work order numbers, which may be affected by hydrogen embrittlement. This AD mandates the replacement of these bolts to ensure continued safe operation of the affected aircraft.

Jul 7, 2020
Airworthiness DirectiveMaintenanceSafety MgmtSaab Ab 2000Saab Ab 340Saab-Fairchild SF340ASaab 340BSaab 2000

EASA AD 2020-0148

Fuel — Low Pressure Shut Off Valve — Inspection

EASA Airworthiness Directive 2020-0148 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aircraft models. It addresses a potential unsafe condition related to fuel leaks from low pressure shut off valves located on engine #1 and engine #2 pylon areas. The directive mandates inspection and corrective actions to prevent possible fuel spillage and fire hazards.

Jul 6, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA SIB SAFO20011

Operations in Oceanic Airspace during the COVID-19 Public Health Emergency

Operations in Oceanic Airspace during the COVID-19 Public Health Emergency is a Safety Alert for Operators (SAFO 20011) issued by the U.S. Federal Aviation Administration. It addresses potential disruptions in Air Traffic Control (ATC) services in oceanic airspace due to COVID-19 related ATC facility shutdowns. The document provides guidance for flightcrews and operators on contingency procedures to maintain safe operations during these interruptions.

Jul 6, 2020
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2020-0139R1

SUPERSEDED BY EASA AD 2025-0073

EASA Airworthiness Directive 2020-0139R1 is an updated directive addressing the inspection and potential repair of horizontal tail plane lateral load fitting bushings on Airbus A350-941 and A350-1041 aeroplanes. It applies to all serial numbers except those with Airbus modifications 110669 or 114806 incorporated. The directive mandates repetitive detailed inspections and corrective actions to prevent structural failure due to bushing migration and associated corrosion or fatigue damage.

Jul 3, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2020-0147

Engine Controls — Mixture Control Cable — Operational Restriction / Replacement

EASA Airworthiness Directive 2020-0147 is an airworthiness directive addressing mixture control cable issues on CEAPR DR400 aeroplanes, specifically models DR 400/120, DR 400/140 B, DR 400/180, and DR 400/180 R with certain serial numbers. It targets mixture control cables with Part Number 57.18.52.020 that may have uncripped cable sheaths, potentially causing loss of mixture control and engine shutdown. The directive mandates operational restrictions and replacement of affected parts to ensure continued airworthiness.

Jul 2, 2020
Airworthiness DirectiveMaintenanceSafety MgmtCeapr DR 400CEAPR DR400/120CEAPR DR400/140 BCEAPR DR400/180CEAPR DR400/180 R

EASA AD 2020-0146

Main Rotor — Main Rotor Hub — Replacement

EASA Airworthiness Directive 2020-0146 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning PZL SW-4 helicopters. It addresses the replacement of main rotor hubs (MRH) equipped with specific bearings and inserts that have been found to wear prematurely. The directive applies to all serial numbers of PZL SW-4 helicopters and focuses on ensuring continued safe operation by managing the life limits of affected MRHs.

Jul 2, 2020
Airworthiness DirectiveMaintenanceSafety MgmtWsk Pzl-Swidnik SW4PZL SW-4

EASA AD 2020-0145

Landing Gear — Main Landing Gear Hinge Arm / Barrel — Pin Replacement / Inspection / Spacer Modification

The document titled 'Landing Gear — Main Landing Gear Hinge Arm / Barrel — Pin Replacement / Inspection / Spacer Modification' is an airworthiness directive applicable to Airbus S.A.S. aircraft models A300, A300-600, and A300-600ST (Beluga). It addresses maintenance procedures related to the main landing gear hinge arm and barrel, focusing on pin replacement, inspection, and spacer modification to ensure continued airworthiness and safety.

Jul 1, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)Airbus A300-600ST

EASA SIB 2020-02R5

WITHDRAWN — RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin 2020-02R5 is an updated guidance document addressing operational recommendations related to the COVID-19 pandemic for national competent authorities, aircraft operators, and aerodrome operators. It provides non-mandatory recommendations to reduce the risk of SARS-CoV-2 spread in aviation operations, emphasizing cleaning, disinfection, and management of potentially infected individuals. The bulletin does not target specific aircraft or engine models but applies broadly to commercial air transport operations.

Jun 30, 2020
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2020-0144

Doors — Forward and Aft Cargo Door Retaining Rings — Inspection

EASA Airworthiness Directive 2020-0144 is an airworthiness directive issued for Airbus A350-941 and A350-1041 aeroplanes. It mandates inspections of the forward and aft cargo door retaining rings to detect potential damage that could compromise structural integrity. The directive also provides an optional modification to terminate repetitive inspections.

Jun 29, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD US-2020-11-12

Nacelles / Pylons - Thumbnail Fairing and Mid Strut Fairing Panels - Inspection / Replacement / Modification

Federal Aviation Administration Airworthiness Directive 2020-11-12 is a final rule addressing certain Boeing 737-8 and 737-9 airplanes. It focuses on inspection, replacement, and modification of the thumbnail fairing and mid strut fairing panels on the engine nacelle and strut to ensure proper electrical bonding and shielding against high intensity radiated fields (HIRF). This directive aims to prevent potential dual-engine power loss and misleading propulsion parameter displays.

Jun 29, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-8Boeing 737-9