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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA AD 2021-0016

Main Rotor Drive — Main Gearbox / Magnetic Plug and Oil Filter / Planet Gears — Inspection / Modification / Replacement

EASA Airworthiness Directive 2021-0016 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters SA 365 C1, C2, and C3 models. It addresses inspection, modification, and replacement requirements related to the main rotor drive main gearbox magnetic plug, oil filter, and planet gears. The directive aims to improve detection of planet gear spalling to prevent potential gearbox seizure and loss of helicopter control.

Jan 13, 2021
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters SA 365 C1Airbus Helicopters SA 365 C2Airbus Helicopters SA 365 C3

EASA AD 2021-0013

Navigation — Global Navigation Satellite System — Replacement / Aircraft Flight Manual — Amendment

EASA Airworthiness Directive 2021-0013 addresses the replacement of Thales Topstar 200 LPV GPS/SBAS receivers on ATR 42-500 and ATR 72-212A aeroplanes. This directive applies to aircraft equipped with specific affected part numbers and mandates amendments to the Aircraft Flight Manual. The directive ensures continued airworthiness by mitigating risks associated with erroneous GPS position outputs during certain satellite constellation conditions.

Jan 13, 2021
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42-500ATR 72-212A

EASA AD 2021-0014

Wings — Outer Wing Lower Skin — Inspection

Wings — Outer Wing Lower Skin — Inspection is a regulatory document issued by FOKKER SERVICES concerning the inspection requirements for the outer wing lower skin on Fokker F28 aircraft. The document outlines necessary inspection procedures to ensure the structural integrity and airworthiness of the affected wing components. It specifically targets operators and maintenance organizations responsible for the upkeep of Fokker F28 aircraft.

Jan 13, 2021
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28

EASA AD 2021-0011

Equipment / Furnishings — Outboard Load System — Inspection / Modification

EASA Airworthiness Directive 2021-0011 is an airworthiness directive addressing the inspection and modification of the outboard load system on Airbus Helicopters Deutschland GmbH EC135 and EC635 helicopter models. It specifically targets Goodrich hoists with certain part numbers and their hook assemblies to prevent potential detachment of external loads or persons during hoist operations.

Jan 12, 2021
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC135Airbus Helicopters 635Airbus Helicopters EC635

EASA AD CF-2020-06R1

Standard Practices/Structures — Introduction of Barrel Nut Inspections

The Standard Practices/Structures — Introduction of Barrel Nut Inspections is a Canadian Airworthiness Directive CF-2020-06R1 issued by Transport Canada affecting all serial numbers of De Havilland Aircraft of Canada Limited DHC-8-100, DHC-8-200, DHC-8-300, and DHC-8-400 series aeroplanes. This directive mandates inspections of barrel nuts installed at multiple structural locations on these aircraft to detect and address cracking caused by corrosion. The inspections aim to maintain structural integrity and prevent potential loss of control of the aeroplane.

Jan 12, 2021
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland Aircraft of Canada Limited DHC-8-100De Havilland Aircraft of Canada Limited DHC-8-200De Havilland Aircraft of Canada Limited DHC-8-300De Havilland Aircraft of Canada Limited DHC-8-400

EASA AD CF-2021-01

Fire Protection — Powerplant Fire Extinguishing (FIREX) Interconnection Hose Not Properly Installed

Canadian Airworthiness Directive CF-2021-01 addresses a fire protection issue related to the powerplant fire extinguishing (FIREX) interconnection hose installation on Airbus Canada Limited Partnership aircraft models BD-500-1A10 and BD-500-1A11. The directive applies to specific serial numbers of these models and mandates corrective action to ensure the FIREX hose is properly secured. This measure aims to prevent ineffective fire extinguishing in the event of a powerplant fire.

Jan 11, 2021
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD 2021-0010

Fuel — Inward Vent Valve — Modification

EASA Airworthiness Directive 2021-0010 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-12/47E aeroplanes, specifically those with manufacturer serial numbers 1720 and 2001 or higher. The directive addresses an issue with inward vent valves that lack a chromate conversion coating, which could lead to corrosion and potential fire hazards. It mandates modification of affected inward vent valves to ensure continued airworthiness and safety.

Jan 11, 2021
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-12Pilatus PC-12/47E

EASA AD 2021-0006

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

EASA Airworthiness Directive 2021-0006 is an airworthiness directive addressing fuel pump replacement life limitations for Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft. It mandates the removal and replacement of specific fuel pumps with part numbers G5030FPU01 and TPS1000-05 before exceeding newly established reduced life limits to prevent fuel pump performance degradation. This directive applies to all serial numbers of affected Trent 1000 engine models.

Jan 7, 2021
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787

EASA AD US-2021-01-03

Engine - High-Pressure Turbine 1st Stage and 2nd Stage Disks - Removal

The Federal Aviation Administration's Airworthiness Directive 2021-01-03 addresses certain International Aero Engines AG V2500 series turbofan engines installed on aircraft such as the Airbus A321-231. This directive mandates the removal from service of specific high-pressure turbine (HPT) 1st-stage and 2nd-stage disks due to an identified unsafe condition following an uncontained disk failure event. The AD aims to prevent potential engine failures that could lead to damage to the engine, aircraft, or loss of the airplane.

Jan 7, 2021
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5International Aero Engines Ag V2500-A1Airbus A321-231

EASA AD 2021-0007

Nacelles / Pylons — Inboard Pylon Box Dog Head Fitting Holes — Inspection

EASA Airworthiness Directive 2021-0007 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes equipped with Rolls-Royce Trent 900 or Engine Alliance GP7200 engines. The directive mandates inspections of the inboard pylon box Dog Head fitting fastener holes to detect cracks that could compromise structural integrity. It applies to all manufacturer serial numbers of these aircraft models.

Jan 7, 2021
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2021-0003

SUPERSEDED BY EASA AD 2021-0196

EASA Airworthiness Directive 2021-0003 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, L1, L2 and EC 225 LP models equipped with specific cabin plug doors (Part Numbers 332A221301.XX or 332AS251406.XX). The directive addresses the installation of additional emergency exit placards on cabin plug doors to improve passenger understanding of emergency door jettisoning procedures.

Jan 6, 2021
Airworthiness DirectiveSafety MgmtMaintenanceAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1Airbus Helicopters AS 332 L2Airbus Helicopters EC 225 LP

EASA SIB AIR-21-01

Textron Aviation (McCauley Propeller Systems) - Alternative Method of Compliance to FAA AD 2020-19-06

Textron Aviation (McCauley Propeller Systems) - Alternative Method of Compliance to FAA AD 2020-19-06 is an FAA-approved alternative method of compliance for Airworthiness Directive 2020-19-06. It specifically addresses the eligibility criteria for installation of McCauley governors with serial numbers after 180501, including new governors and those maintained according to specific McCauley Alert Service Bulletins. This document applies to McCauley propeller governors used on affected aircraft.

Jan 6, 2021
AMC/GMMaintenanceSafety Mgmt

EASA AD US-2020-25-10

Engine - High Pressure Turbine Rotor Stage 2 Disks - Inspection / Replacement

The Federal Aviation Administration's Airworthiness Directive 2020-25-10 is a final rule addressing certain General Electric Company GEnx-1B and GEnx-2B model turbofan engines equipped with specific high-pressure turbine (HPT) rotor stage 2 disks. This directive mandates inspection and potential replacement of these disks due to the risk of undetected subsurface anomalies that could lead to uncontained disk failure. The directive applies to multiple GEnx engine variants including GEnx-1B64/P2, GEnx-1B67/P2, GEnx-1B70/75/P2, and others.

Jan 5, 2021
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric GEnx

EASA SIB SAFO20016

Saircorp / Flight Boss Ltd. (Saircorp) Consoles

SAFO 20016 is a Safety Alert for Operators issued by the U.S. Federal Aviation Administration concerning the use of Saircorp consoles in Textron Aviation Inc. Model 172-, 177-, 182-, 185-, 205-, 206-, 210-, 310-, 320-, 337-, and 340-series airplanes, as well as other aircraft. The alert highlights safety risks posed by these unsecured metal consoles, which can shift during flight and interfere with aircraft controls or emergency equipment access.

Jan 4, 2021
Safety Information BulletinSafety MgmtFlight Ops

EASA AD 2021-0001

SUPERSEDED BY EASA AD 2021-0034

EASA Airworthiness Directive 2021-0001 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841 and A380-842 aeroplanes equipped with Rolls-Royce RB211 Trent 900 engines. The directive mandates inspections of the front engine mount, strut mount, and thrust link due to concerns about salvage welds on the compressor intermediate case lugs in certain engines. It aims to ensure continued airworthiness by requiring repetitive inspections and corrective actions to prevent potential engine detachment in flight.

Jan 4, 2021
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD US-2020-26-09

Wings - Center Wing Box Fastener Holes - Inspection

FAA Airworthiness Directive 2020-26-09 is a final rule addressing all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates inspections of the center wing box fastener holes for cracks using high frequency eddy current, ultrasonic, or detailed internal inspection methods. The directive aims to maintain structural integrity by detecting and repairing cracks in critical wing components.

Jan 4, 2021
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD US-2020-25-01

Wings - Lower Forward Wing Fittings - Inspection

Federal Register Volume 85, Number 235 (December 7, 2020) is a final rule airworthiness directive issued by the FAA addressing certain Textron Aviation Inc. airplanes (formerly Beechcraft Corporation) including Models F90, 65-90, B90, C90, H90 (T-44A), E90, 99 series, A99 series, B99, C99, 100 series, A100, and B100. The directive targets fatigue cracks in the lower forward wing fittings caused by the installation of a specific washer part number. It mandates inspection and corrective actions to ensure continued airworthiness and safety.

Jan 4, 2021
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 100 (King Air)Textron Aviation 65 (Queen Air)Textron Aviation 90 (King Air)Textron Aviation 99 (Airliner)Textron Aviation F90Textron Aviation 65-90Textron Aviation B90Textron Aviation C90Textron Aviation H90Textron Aviation E90Textron Aviation 99 seriesTextron Aviation A99 seriesTextron Aviation B99Textron Aviation C99Textron Aviation 100 seriesTextron Aviation A100Textron Aviation B100

EASA AD CF-2020-54R1

SUPERSEDED BY TCCA AD CF-2023-32

Canadian Airworthiness Directive CF-2020-54R1 addresses cracking issues in the main landing gear (MLG) shock strut lower pin, part number 19146-3, on Bombardier Inc. model CL-600-2B16 aircraft with specified serial numbers. The directive mandates repetitive lubrication, detailed visual inspections, and non-destructive testing of the affected pins to detect and prevent structural failure. It applies to various CL-600-2B16 variants including CL-604, CL-605, and CL-650 models.

Dec 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBombardier CL-600 (Challenger)Bombardier CL-600-2B16Bombardier CL-604Bombardier CL-605Bombardier CL-650

EASA AD 2020-0283

SUPERSEDED BY EASA AD 2022-0197

EASA Airworthiness Directive 2020-0283 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 and A340 aeroplanes. It addresses fuel pumps with specific part numbers installed at designated locations on these aircraft models. The directive mandates inspections and potential replacements of fuel pumps showing erosion to prevent fuel tank ignition risks.

Dec 24, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD 2020-0022R2

Time Limits / Maintenance Checks — Main Gear Box / Particle Detectors — Inspection; Main Rotor Drive — Planet Gear Assemblies — Replacement / Modification

EASA Airworthiness Directive 2020-0022R2 is an updated regulatory requirement affecting Airbus Helicopters AS 332 L, L1, C, and C1 models. It addresses inspection, replacement, and modification requirements related to the main gearbox (MGB) planet gear assemblies and particle detectors to mitigate risks associated with gear spalling and cracking. The directive mandates specific inspections and installation of a Full Flow Magnetic Plug (FFMP) device to enhance safety and continued airworthiness.

Dec 23, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1