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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 2024-0156

Landing Gear — Main Landing Gear Bogie Beam Axle — Replacement

EASA Airworthiness Directive 2024-0156 is an airworthiness directive addressing the replacement of the main landing gear bogie beam axle on Airbus A350-941 aeroplanes. It specifically targets affected parts with Part Number 55-3575047-00 and certain serial numbers due to identified anodic burns that reduce fatigue life. The directive mandates replacement of these parts to prevent potential structural failure of the main landing gear.

Aug 13, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD 2024-0155

Wings — RIB 1 corner fitting and Upper / Lower Wing Skin Cover Edge Glow Sealant — Inspection / Modification

EASA Airworthiness Directive 2024-0155 is an airworthiness directive issued for Airbus A350-941 and A350-1041 aeroplanes. It addresses inspection and modification requirements related to the RIB 1 corner fitting and upper/lower wing skin cover edge glow sealant to ensure proper lightning strike protection on the wing tanks. This directive applies to specific manufacturer serial numbers as defined by Airbus service bulletins.

Aug 13, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD US-2024-12-09

[Correction] Wings - Wing Skin / Shim - Inspection

The Correction to Airworthiness Directive 2024-12-09 issued by the Federal Aviation Administration (FAA) addresses all Boeing Company Model 757 airplanes. This correction fixes an incorrect AD number referenced in the original final rule related to inspections of the wing upper skin and drag fittings to detect cracks, loose fasteners, and shim migration. The directive ensures continued airworthiness by mandating inspections and on-condition repairs to maintain structural integrity of the engine strut attachment.

Aug 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD 2024-0147R1

Fuselage — Centre Fuselage Forward Pressure Bulkhead — Inspection

EASA Airworthiness Directive 2024-0147R1 is an updated regulatory requirement addressing inspection and reinforcement of the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aircraft. It mandates repetitive inspections for fatigue damage at frame 35 (or 35.8 for A321) and requires modification to reinforce the bulkhead to ensure structural integrity. This directive applies to all serial numbers except those with specific Airbus modifications embodied in production or service.

Aug 7, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD ISR-I-34-2024-07-1

Pitot-Static tubing improper rerouting after aircraft conversion from PAX to Freighter

Airworthiness Directive ISR I-34-2024-07-1 issued by the Civil Aviation Authority of Israel addresses improper rerouting of pitot-static tubing after conversion of Boeing 767-300 aircraft from passenger to freighter configuration. This directive applies to aircraft with the CAAI STC SA-218 modification installed, affecting the pitot and static system tubing connected to the first officer's Air Data Computer. The issue involves potential water traps in specific flexible hoses and rigid tubes that may impair system functionality.

Aug 6, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 767Israel Aerospace Industries CAA Israel STC SA218Boeing 767-300

EASA AD 2019-0069R2

[Correction] Equipment / Furnishings — Overhead Stowage Compartments — Modification

EASA Airworthiness Directive 2019-0069R2 is a regulatory document addressing the modification of overhead stowage compartments (OHSC) and pivoting OHSC (POHSC) on Airbus A318, A319, A320, and A321 aircraft. The directive mandates modifications to improve the robustness of these compartments to prevent detachment caused by loose or missing screws. This AD applies specifically to various Airbus A320 family models as listed in the applicable service bulletins.

Aug 5, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD CF-2022-66R1

Fire Protection — Inspection and Replacement of Defective Cargo Fire Extinguisher Containers

The Canadian Airworthiness Directive CF-2022-66R1 addresses fire protection concerns related to the inspection and replacement of defective cargo fire extinguisher containers on MHI RJ Aviation ULC model CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. It mandates inspection of serial numbers of high rate of discharge (HRD) and low rate of discharge (LRD) cargo fire extinguisher containers and replacement of affected units to ensure proper fire suppression capabilities. This directive updates previous requirements to reflect new identification markings on modified containers.

Aug 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)MHI RJ Aviation ULC CL-600-2C10MHI RJ Aviation ULC CL-600-2C11MHI RJ Aviation ULC CL-600-2D15MHI RJ Aviation ULC CL-600-2D24MHI RJ Aviation ULC CL-600-2E25

EASA AD 2024-0154

Fuel — Fuel Tank / Bonding Straps — Inspection

EASA Airworthiness Directive 2024-0154 is an airworthiness directive addressing the inspection and maintenance of fuel tank bonding straps on Dornier 328-100 and Dornier 328-300 aeroplanes. It mandates repetitive inspections and provides an optional modification to replace existing bonding straps with nickel-plated versions to ensure electrical bonding integrity and prevent ignition risks. The directive applies to all manufacturer serial numbers of these aircraft models.

Aug 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100Dornier 328-300

EASA AD CF-2024-28

Wings - Left Hand Main Landing Gear Fuse Pin Missing

Canadian Airworthiness Directive CF-2024-28 is an emergency directive addressing the missing left hand main landing gear fuse pin on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. This directive applies to specific serial numbers of these models and mandates inspections to ensure the presence and correct installation of the Pintle Fuse Pins in the main landing gear assembly. The directive aims to prevent potential landing gear collapse during takeoff due to missing or damaged fuse pins.

Aug 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD 2024-0153

SUPERSEDED BY EASA ADR 2025-0084

The document titled SUPERSEDED BY EASA ADR 2025-0084 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for Europrop International GmbH TP400-D6 engines in civil service. It clarifies that no publicly available AD exists because these engines are not used in civil aviation, and the document serves only as information for design approval holders and military airworthiness authorities. The legally binding AD requirements for affected military aircraft with TP400-D6 engines are issued by the respective military authorities of the aircraft's country of registration.

Aug 1, 2024
OtherMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA AD 2024-0151

Aircraft Flight Manual / Complementary Performance Data File — Amendment

EASA Airworthiness Directive 2024-0151 is an amendment applicable to Airbus A321 aeroplanes, including multiple variants such as A321-111, A321-131, A321-251N, and others. This directive addresses an error in the main landing gear tyre width data used in aircraft performance calculations. The directive mandates updates to the Aircraft Flight Manual and Complementary Performance Data File to correct performance computations.

Jul 31, 2024
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A321

EASA SIB 2011-28R1

Maintenance of Emergency Evacuation Systems

EASA Safety Information Bulletin 2011-28R1 is an airworthiness bulletin addressing the maintenance of emergency evacuation systems on Airbus A318, A319, A320, and A321 aircraft. It emphasizes the importance of proper maintenance and reporting of malfunctions in evacuation systems such as slides, slides/rafts, and door mechanisms to ensure their reliability during emergencies. The bulletin updates references to the latest Airbus service publications and reinforces the need for accurate data collection during system testing and deployments.

Jul 30, 2024
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0149

SUPERSEDED BY EASA AD 2026-0027

EASA Airworthiness Directive 2024-0149 is issued for SAFRAN Helicopter Engines ARRIUS 2B2 engines, which are commonly installed on Airbus Helicopters Deutschland EC135 and EC635 models. This directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the latest Airworthiness Limitations Section of the ARRIUS 2B2 Maintenance Manual. It ensures continued airworthiness by enforcing life limits and maintenance intervals for engine components.

Jul 30, 2024
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2Airbus Helicopters EC135Airbus Helicopters EC635

EASA AD 2024-0148

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2024-0148 is an amendment addressing the time limits and maintenance checks in the Airworthiness Limitations Section for SAFRAN Helicopter Engines ARRIUS 1A engines. These engines are commonly installed on Airbus Helicopters AS 355 N twin-engine helicopters. The directive mandates compliance with updated maintenance tasks and life limits to ensure continued airworthiness.

Jul 30, 2024
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 1Airbus Helicopters AS 355 N

EASA AD 2024-0150

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2024-0150 is an amendment addressing the time limits and maintenance checks in the Airworthiness Limitations Section for SAFRAN Helicopter Engines ARRIUS 2K2 engines, commonly installed on Leonardo A109 helicopters. This directive mandates compliance with updated maintenance tasks and life limits as specified in the latest SAFRAN Arrius 2K2 Maintenance Manual. It ensures continued airworthiness by enforcing new or more restrictive maintenance requirements.

Jul 30, 2024
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2Leonardo A109

EASA AD CF-2024-27

Flight Controls — Incorrect Airplane Flight Manual Approach Speed Adder and Landing Distance Factors for SLAT-FLAP FAIL Caution Crew Alerting System Message and Jammed or Inoperative Slat/Flap Control Lever

Airworthiness Directive CF-2024-27 is issued by Transport Canada and addresses incorrect approach speed adders and landing distance factors in the Airplane Flight Manual (AFM) for Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft models. This directive applies to specific serial numbers of these models and corrects errors related to the SLAT-FLAP FAIL caution Crew Alerting System message and jammed or inoperative Slat/Flap Control Lever procedures. The directive mandates updates to the AFM to ensure accurate performance data is used during approach and landing.

Jul 29, 2024
Airworthiness DirectiveFlight OpsSafety MgmtBombardier BD-700Bombardier BD-700-1A10Bombardier BD-700-1A11

EASA AD 2024-0146

Fuel — Fuel Tanks — Mounting Plates of Fuel Tank Bleed Valves — Inspection / Repair / Replacement / Modification

EASA Airworthiness Directive 2024-0146 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters EC 175 B models. It addresses corrosion issues found on the mounting plates of fuel tank bleed valves installed on specific flexible fuel tanks with part numbers 509505-5, 509506-5, 509507-4, and 509510-5. The directive mandates inspection, repair, replacement, and modification of these parts to ensure continued airworthiness.

Jul 29, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC 175 B

EASA AD BR-2024-07-01

Kidde Aerospace & Defense - Overheat Detection System Sensing Elements - Inspection

Brazilian Airworthiness Directive AD No. 2024-07-01 issued by ANAC mandates inspection and possible replacement of Kidde Aerospace & Defense Overheat Detection System sensing elements on Embraer ERJ 190-100 ECJ aircraft as identified in Embraer Service Bulletin 190LIN-36-0013 revision 03. The directive addresses defective sensing elements produced before January 31, 2021, which may fail to detect thermal bleed leaks and pose fire risks. It applies to all affected aircraft registered in Brazil.

Jul 29, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190Embraer ERJ 190-100 ECJ

EASA AD US-2024-12-10

Main Rotor Drive - Angle Gearbox Mount - Repetitive Inspections

The Federal Aviation Administration's Airworthiness Directive 2024-12-10 is a final rule addressing all Centerpointe Aerospace Inc. Model S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, and S-58JT helicopters. It mandates repetitive fluorescent penetrant inspections of the main rotor drive angle gearbox mount to detect cracks and requires removal from service if cracks are found. This directive aims to mitigate the risk of structural failure due to fatigue cracking in the angle gearbox mount.

Jul 29, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCenterpointe Aerospace, Inc S-58Centerpointe Aerospace S-58BTCenterpointe Aerospace S-58DTCenterpointe Aerospace S-58ETCenterpointe Aerospace S-58FTCenterpointe Aerospace S-58HTCenterpointe Aerospace S-58JT

EASA AD 2024-0118R1

SUPERSEDED BY EASA AD 2025-0206

EASA Airworthiness Directive 2024-0118R1 addresses safety concerns for Rolls-Royce Deutschland Ltd & Co KG Trent 1000 series engines installed on Boeing 787 aircraft. The directive mandates inspections of high pressure turbine (HPT) blades, specifically part numbers KH10575 and KH64485, to detect cracking that could lead to engine failure. It updates inspection thresholds and methods to ensure continued airworthiness of affected engines.

Jul 29, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787