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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 US-2019-10-03

Fuselage - Left and Right Side-Strut Support Fitting Lugs - Inspection

Federal Register Volume 84, Number 109 (June 6, 2019) is a final rule airworthiness directive issued by the FAA addressing all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates repetitive detailed and high frequency eddy current inspections of the left and right side-strut support fitting lugs to detect corrosion, cracks, or severed lugs. The directive aims to prevent potential failure of the side-strut support fitting joint and main landing gear attachment.

Jun 21, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD 2019-0146

SUPERSEDED BY EASA AD 2019-0150

EASA Airworthiness Directive 2019-0146 is an airworthiness directive addressing certain CFM56-5B, CFM56-5C, and CFM56-7B engines installed on aircraft including Airbus A318, A319, A320, A321, A340 and Boeing 737-600, 737-700, 737-800, and 737-900. The directive focuses on the replacement of rotating air high pressure turbine (HPT) front seals that are susceptible to cracking if removed and re-installed on different HPT disks. It mandates specific inspections and replacements to ensure continued airworthiness and safe operation of affected engines.

Jun 21, 2019
Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-5BCFM International CFM56-5CCFM International CFM56-7BAirbus A318Airbus A319Airbus A320Airbus A321Airbus A340Boeing 737-600Boeing 737-700Boeing 737-800Boeing 737-900

EASA AD 2019-0147

SUPERSEDED BY EASA AD 2019-0151-E

EASA Airworthiness Directive 2019-0147 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, and A320 aeroplanes. It addresses the inspection of main landing gear sliding tubes, specifically those with part number 201371304 and certain serial numbers, to detect potential cracks or defects. The directive applies to all manufacturer serial numbers of the specified aircraft models.

Jun 21, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320

EASA AD 2019-0121R1

SUPERSEDED BY EASA AD 2019-0193

EASA Airworthiness Directive 2019-0121R1 is an updated safety directive addressing Leonardo S.p.A. AW169 and AW189 helicopters. It mandates inspections and monitoring of the tail rotor servo actuator and duplex bearing to prevent potential loss of yaw control due to incorrect installation or bearing degradation. The directive includes repetitive inspections, thermal strip installations, and corrective actions to ensure continued airworthiness.

Jun 21, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AW169Leonardo S.P.A. Helicopters AW189Leonardo AW169Leonardo AW189

EASA AD 2019-0144

Aircraft Flight Manual — Amendment ; Ice and Rain Protection — Total Air Temperature Probe Heater / Electrical Circuit — Modification

The document titled 'Aircraft Flight Manual — Amendment ; Ice and Rain Protection — Total Air Temperature Probe Heater / Electrical Circuit — Modification' applies specifically to the Piaggio P180 aircraft. It details an amendment to the Aircraft Flight Manual concerning modifications to the ice and rain protection system, focusing on the total air temperature probe heater and its electrical circuit.

Jun 19, 2019
OtherFlight OpsMaintenancePiaggio P180

EASA AD CF-2019-23

Flight Controls — Pitch Trim System — Upgrade of the Horizontal Stabilizer Trim Electronic Control Unit

Canadian Airworthiness Directive CF-2019-23 mandates an upgrade to the Horizontal Stabilizer Trim Electronic Control Unit (HSTECU) on Bombardier Inc. BD-100-1A10 aircraft, serial numbers 20001 through 20337. This directive addresses the pitch trim system to enhance flight control safety by verifying the Motor Brake Assemblies' braking capability during power-up tests. The AD applies specifically to certain HSTECU part numbers installed on these aircraft.

Jun 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-100Bombardier BD-100-1A10

EASA AD 2019-0145

SUPERSEDED BY EASA ADR 2019-0260

The document titled SUPERSEDED BY EASA ADR 2019-0260 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for Europrop International GmbH TP400-D6 engines. It clarifies that no civil service aircraft currently use these engines, so no public AD exists. The document serves as an informational record for military authorities and design approval holders, recommending that military authorities issue their own applicable ADs for aircraft equipped with TP400-D6 engines.

Jun 19, 2019
OtherMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA SIB CE-19-11

Eastern Marine Aero Worldwide Infant Life Vests - Protective Plugs

The Eastern Marine Aero Worldwide Infant Life Vests - Protective Plugs Special Airworthiness Information Bulletin (SAIB: CE-19-11) informs the aviation community about an airworthiness concern involving Eastern Marine Aero Worldwide Infant Life Vests Model EAM-IN-V20L8, part numbers P0640-XXX. The bulletin highlights the need to ensure that protective plugs in the survivor locator light batteries are removed before use to allow proper activation of the light. This bulletin applies to all aircraft using these specific infant life vests.

Jun 18, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD US-2019-08-51

[Final Rule] Flight Controls - Angle of Attack Sensors - Replacement

[Final Rule] Flight Controls - Angle of Attack Sensors - Replacement is a Federal Aviation Administration (FAA) airworthiness directive (AD) addressing all Cirrus Design Corporation Model SF50 airplanes. This AD mandates the replacement of angle of attack (AOA) sensors with improved versions due to incidents where the stall warning and protection system (SWPS) or Electronic Stability & Protection (ESP) System engaged inappropriately. The directive aims to mitigate unsafe flight conditions caused by faulty AOA sensors.

Jun 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtCirrus Design Corporation SF50Cirrus SF50

EASA AD US-2019-10-06

Fuel - Fuel Vent Check Valve - Replacement / Airplane Flight Manual Revision

Federal Aviation Administration Airworthiness Directive 2019-10-06 is a final rule addressing certain Aviat Aircraft Inc. Models A-1C-180 and A-1C-200 airplanes equipped with Rapco part number RA1798-00-1 fuel vent check valves. The directive requires revising the airplane flight manual to include a pre-flight check of these fuel vent check valves and mandates replacing any inoperative valves with Aviat part number 38266-501 valves. This AD aims to prevent fuel starvation caused by fuel vent check valves sticking in the closed position.

Jun 18, 2019
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAviat Aircraft A-1 (Husky)Aviat A-1C-180Aviat A-1C-200

EASA AD 2019-0123R1

SUPERSEDED BY EASA AD 2020-0157

EASA Airworthiness Directive 2019-0123R1 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes regarding the landing gear gravity extension system. It mandates inspections and modifications to the wing landing gear emergency up-lock actuator wiring to prevent failure during gravity extension. This directive ensures continued airworthiness by requiring specific inspections and corrective actions to maintain safe landing gear operation.

Jun 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD BR-2019-06-01

Wings - Wing Lower Skin Stringers - Inspection

Brazilian Airworthiness Directive 2019-06-01 is an official regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) addressing structural inspections on Embraer S.A. ERJ 190 series aircraft, specifically models ERJ 190-100 and ERJ 190-200 with certain serial numbers. The directive mandates inspections of wing lower skin stringers between ribs 7 and 10 on both half wings to detect cracks and fuel leakage risks. This AD applies to aircraft registered in Brazil and aims to maintain structural integrity and flight safety.

Jun 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190Embraer ERJ 190-100Embraer ERJ 190-200

EASA AD 2019-0142

SUPERSEDED BY EASA AD 2023-0059

EASA Airworthiness Directive 2019-0142 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Fan Jet Falcon aeroplanes equipped with the Supplemental Structural Inspection Program (SSIP). It mandates compliance with updated maintenance tasks and life limits as specified in the Dassault Fan Jet Falcon Aircraft Maintenance Manual Chapter 5-40 Revision 10. This directive ensures continued structural integrity and airworthiness of these aircraft.

Jun 17, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDassault Fan Jet Falcon

EASA AD 2019-0141

SUPERSEDED BY EASA AD 2023-0060

EASA Airworthiness Directive 2019-0141 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Fan Jet Falcon aeroplanes. It mandates compliance with updated airworthiness limitations specified in Chapter 5-40 of the Dassault FJF Aircraft Maintenance Manual, Revision 18. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components on these aircraft.

Jun 17, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDassault Fan Jet Falcon

EASA AD US-2019-11-06

Fuselage - Skin under the Drag Link Assembly - Inspection

Federal Aviation Administration Airworthiness Directive 2019-11-06 is a final rule addressing certain Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. It mandates repetitive inspections of the fuselage skin under the drag link assembly for cracks at specific fastener locations. The directive aims to ensure continued airworthiness by detecting and correcting skin cracks that could compromise structural integrity.

Jun 14, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-600Boeing 737-700Boeing 737-700CBoeing 737-800Boeing 737-900Boeing 737-900ER

EASA AD US-2019-11-08

SUPERSEDED BY FAA AD 2020-05-28

FAA Airworthiness Directive 2019-11-08 is a final rule addressing all International Aero Engines, LLC PW1133G-JM, PW1133GA-JM, PW1130G-JM, PW1129G-JM, PW1127G-JM, PW1127GA-JM, PW1127G1-JM, PW1124G-JM, PW1124G1-JM, and PW1122G-JM model turbofan engines. It mandates the removal and replacement of the main gearbox (MGB) assembly and electronic engine control (EEC) software due to high-cycle fatigue fractures causing in-flight engine shutdowns. This directive aims to prevent engine failure, loss of thrust control, and potential loss of the airplane.

Jun 14, 2019
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines PW1100International Aero Engines PW1400

EASA AD 2019-0143

Engine — Power Turbine Disc — Inspection / Replacement

EASA Airworthiness Directive 2019-0143 is an airworthiness directive addressing inspection and replacement of power turbine discs on GE Aviation Czech M601 series engines. It applies to multiple M601 engine variants installed on aircraft such as the Aircraft Industries L-410 series, Air Tractor AT series, Allied Ag Cat G-164 series, PZL-106 Kruk, RUAG Do 28 series, and Thrush S-2R series. The directive mandates inspections and replacement of certain power turbine discs identified by part and serial numbers to ensure continued safe operation.

Jun 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech M601Aircraft Industries L-410Air Tractor ATAllied Ag Cat G-164PZL-106 KrukRUAG Do 28Thrush S-2R

EASA AD CF-2011-42R1

Fuselage - Longeron Cracking - Inspection / Repair.

The Canadian Airworthiness Directive CF-2011-42R1 addresses fuselage longeron cracking in Bell Helicopter Textron Canada Limited Model 407 helicopters, specifically those equipped with upper left longeron assemblies part numbers 206-031-314-037, 206-031-314-177, or spare assembly 206-031-314-219B. This directive mandates inspections and repairs to detect and correct cracking in the upper left longeron to maintain structural integrity and ensure flight safety. It applies to helicopters with serial numbers 53000 through 53900, 53911 through 54061, and 54300.

Jun 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBell 407Bell Helicopter Textron Canada Limited Model 407

EASA AD 2019-0140

Oxygen — Chemical Oxygen Generators — Replacement

The document titled 'Oxygen — Chemical Oxygen Generators — Replacement' pertains to the Airbus A330 aircraft type. It addresses the replacement requirements for chemical oxygen generators installed on these aircraft to ensure continued safety and compliance with airworthiness standards. This document is relevant for operators and maintenance organizations managing Airbus A330 fleets.

Jun 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA SIB CE-19-10

Rockwell Collins Pro Line 4 and Pro Line 21 Flight Management Systems

The Special Airworthiness Information Bulletin SAIB: CE-19-10 is an FAA informational bulletin addressing an issue with certain versions of the Rockwell Collins Pro Line 4 and Pro Line 21 Flight Management Systems (FMS), specifically FMC-3000, FMC-4200, FMC-5000, and FMC-6000 versions 97 through 3.2. The bulletin informs operators that deleting waypoints using the DELETE function on these FMS versions may cause the aircraft to make an incorrect turn direction during departures, STARs, or approaches. This bulletin does not apply to any specific aircraft type but relates to the affected FMS equipment installed on various aircraft.

Jun 12, 2019
Safety Information BulletinFlight OpsSafety Mgmt