EASA Regulations & Airworthiness Directives

Browse 5057 EASA regulations with AI-powered summaries.

EASA AD 2025-0094R1

Electrical Power – Overhead Panel Wires Interference – Inspection / Modification

EASA Airworthiness Directive 2025-0094R1 is issued for Leonardo S.p.A. AB139 and AW139 helicopters, addressing interference issues between electrical cables and connectors in the overhead panel. The directive mandates inspections and modifications to prevent potential cable damage that could lead to fire and loss of helicopter control. It applies to all serial numbers from 31201 onward, focusing on Long Nose helicopter configurations.

Jul 3, 2026
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AB139Leonardo S.P.A. Helicopters AW139Leonardo AB139Leonardo AW139

EASA AD 2025-0171R2

Engine – High Pressure Turbine Rotor Stage 1 Blade – Inspection

EASA Airworthiness Directive 2025-0171R2 is an updated regulatory requirement addressing inspections of high pressure turbine (HPT) rotor stage 1 blades on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive mandates repetitive borescope inspections of specific affected turbine blades to detect cracks and prevent potential in-flight engine failures. It applies to multiple LEAP-1A engine variants and specifies affected part numbers for inspection and corrective actions.

Jul 3, 2026
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA AD CF-2026-26

Fuselage – Corrosion on Waste Box, Waste Access Doubler and Waste Service Door of Aft Waste Service Port

The Canadian Airworthiness Directive CF-2026-26 addresses corrosion issues on the waste box, waste access doubler, and waste service door of the aft waste service port on Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. This directive mandates inspections, repairs, and application of protective coatings to prevent structural damage caused by corrosion. It applies to aircraft with specific serial numbers ranging from 50001 to 50047 for BD-500-1A10 and 55001 to 55063 for BD-500-1A11.

Jul 3, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada Limited Partnership BD-500-1A10Airbus Canada Limited Partnership BD-500-1A11

EASA AD 2026-0129

Main Rotor Drive – Main Gearbox Flexible Mounting Plate – Maintenance Task

EASA Airworthiness Directive 2026-0129 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, and L1 models. It mandates maintenance on the main gearbox flexible mounting plate, specifically part numbers 332A38010600 and 332A38010620, to ensure proper torque on attachment bolts. This directive addresses a maintenance task correction related to helicopters performing external load transport with loads of 2.5 tons or less.

Jul 3, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2026-0123

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2026-0123 is an amendment concerning time limits and maintenance checks in the Airworthiness Limitations Section for GE Aviation Czech H75, H80, and H85 engine models. This directive applies to these engines installed on aircraft such as the Aircraft Industries L410-UVP-E20, L410-NG, Do 28 series, Thrush S-2R series, and Viking Air DHC-3 Otter. It mandates compliance with updated maintenance tasks and life limits to ensure continued airworthiness.

Jul 3, 2026
Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech H75, H80, H85Aircraft Industries L410-UVP-E20Aircraft Industries L410-NGDornier Do 28Thrush S-2RViking Air DHC-3 Otter

EASA AD 26-082

Flight Controls – Roll Spoiler Actuator Mount – Inspection

EASA Airworthiness Directive Proposal PAD No. 26-082 addresses the inspection of roll spoiler actuator mounts on Dornier 328-100 aeroplanes. The directive targets corrosion issues found around the pivot-bearing area of the roll spoiler actuator mounts, which could affect flight control. It applies to all manufacturer serial numbers of Dornier 328-100 aircraft.

Jul 2, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100

EASA AD 26-081

Fire Protection – Pyrotechnical Cartridge – Inspection

EASA Airworthiness Directive PAD No. 26-081 is a proposed directive addressing fire protection inspections for pyrotechnical cartridges installed on Dassault Aviation Mystère-Falcon and Fan Jet Falcon aeroplanes. It applies to all serial numbers of Fan Jet Falcon, Mystère-Falcon 20-( )5 series, Mystère-Falcon 200, and 20 GF models. The directive mandates repetitive inspections and potential replacement of specific pyrotechnical cartridges to ensure fire extinguishing capability.

Jul 1, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDassault Fan Jet FalconDassault Mystère-Falcon 20Dassault Mystère-Falcon 20GFDassault 200Dassault Mystère-Falcon 20-( )5Dassault Mystère-Falcon 200Dassault 20 GF

EASA AD 2026-0124

Flight Controls – Aileron Hinge / Cotter Pins – Inspection

EASA Airworthiness Directive 2026-0124 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Tecnam P2006T and P2006T NG aeroplanes. It mandates inspection of the aileron hinge assemblies and cotter pins to ensure their integrity and prevent potential detachment of the ailerons. This directive applies to specific serial numbers of these aircraft models and aims to maintain flight safety by addressing a critical flight control component issue.

Jul 1, 2026
Airworthiness DirectiveMaintenanceSafety MgmtTecnam P2006TTecnam P2006T NG

EASA AD US-2026-13-17

Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment

Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment is a Federal Aviation Administration (FAA) airworthiness directive addressing interference issues affecting Boeing 737-8, 737-9, and 737-8200 airplanes. This directive responds to increased 5G Lower C-Band interference in Canadian airspace that compromises radio altimeter reliability and impacts critical airplane systems during takeoff and landing. The amendment mandates updates to the airplane flight manual to restrict certain operations relying on radio altimeter data when flying in Canadian airspace.

Jul 1, 2026
Airworthiness DirectiveFlight OpsSafety MgmtBoeing 737Boeing 737-8Boeing 737-9Boeing 737-8200

EASA AD US-2026-13-15

Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment

The document titled "Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment" is a Federal Aviation Administration (FAA) final rule airworthiness directive (AD 2026-13-15) addressing interference issues affecting radio altimeters on various Boeing aircraft models including 707, 717, 727, DC-8, DC-9, DC-10, MD-10, MD-11, MD-81 through MD-88, and MD 90-30 airplanes. This AD responds to increased 5G Lower C-Band wireless broadband interference in Canadian airspace that compromises radio altimeter reliability and the proper functioning of critical airplane systems during approach, landing, and go-around phases. The directive mandates revisions to the airplane flight manual (AFM) to restrict certain operations dependent on radio altimeter data when operating in Canadian airspace.

Jul 1, 2026
Airworthiness DirectiveFlight OpsSafety MgmtBoeing 707Boeing 717Boeing 727Boeing DC-10Boeing DC-8Boeing DC-9Boeing MD-10Boeing MD-11Boeing MD-88Boeing MD-90McDonnell Douglas DC-8McDonnell Douglas DC-9McDonnell Douglas DC-10McDonnell Douglas MD-10McDonnell Douglas MD-11McDonnell Douglas MD-81McDonnell Douglas MD-82McDonnell Douglas MD-83McDonnell Douglas MD-84McDonnell Douglas MD-85McDonnell Douglas MD-86McDonnell Douglas MD-87McDonnell Douglas MD-88McDonnell Douglas MD-90-30

EASA AD US-2026-13-16

Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment

The Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment is a Federal Aviation Administration (FAA) airworthiness directive addressing interference issues affecting Boeing Model 757 and Model 767 airplanes. This directive responds to increased 5G Lower C-Band interference in Canadian airspace that compromises radio altimeter reliability and affects critical airplane systems during approach, landing, and go-around phases. It mandates revisions to the airplane flight manual to restrict certain operations relying on radio altimeter data when operating in Canadian airspace.

Jul 1, 2026
Airworthiness DirectiveFlight OpsSafety MgmtBoeing 757Boeing 767

EASA AD US-2026-13-02

NOT ELIGIBLE FOR ADOPTION - EASA POSITION ATTACHED

The Federal Aviation Administration's Airworthiness Directive 2026-13-02 is a final rule addressing all transport and commuter category airplanes equipped with radio altimeters. This directive responds to interference risks from 5G Lower C-Band wireless broadband operations in Canadian airspace, which can impair radio altimeter functionality. It requires revising airplane flight manuals and modifying certain airplanes to radio altimeter tolerant standards to ensure safe operations in Canadian airspace.

Jul 1, 2026
Airworthiness DirectiveFlight OpsSafety Mgmt

EASA AD 2026-0126-CN

CANCELLED: Fire Protection – Safe Selector Switches on the Control Panel with Metallic Snap Wire

EASA Airworthiness Directive Cancellation Notice 2026-0126-CN is an official cancellation of the previous DGCA AD 2003-084(B) R1 concerning fire protection safe selector switches with metallic snap wire on Dassault Aviation Mystère-Falcon 900 and Falcon 2000 aeroplanes. This cancellation confirms that no unsafe conditions related to metallic lock wires on fire extinguisher control switches have been reported since the original directive. The notice applies to all serial numbers of the affected aircraft models.

Jun 30, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 2000Dassault Mystère-Falcon 900Dassault Aviation Mystère-Falcon 900Dassault Aviation Falcon 2000

EASA AD 2026-0125R1

Landing Gear – Nose landing Gear Hydraulic Actuator Rod End – Inspection

EASA Airworthiness Directive 2026-0125R1 is an updated regulatory requirement addressing the inspection of the nose landing gear hydraulic actuator rod end on Diamond Aircraft Industries GmbH DA 42, DA 42 M, DA 42 NG, and DA 42 M-NG aeroplanes. It mandates repetitive inspections of specific affected parts with part numbers X11-0006-SMRCD10IRMR.7403 and X11-0006-GARSW-10RR to detect cracks that could cause rudder control issues. The directive also includes operational limitations and corrective actions to ensure continued airworthiness.

Jun 30, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries DA 42Diamond Aircraft Industries GmbH DA 42Diamond Aircraft Industries GmbH DA 42 MDiamond Aircraft Industries GmbH DA 42 NGDiamond Aircraft Industries GmbH DA 42 M-NG

EASA AD 2026-0127

Main Rotor – Swashplate – Inspection

EASA Airworthiness Directive 2026-0127 is an airworthiness directive addressing the inspection of the main rotor swashplate and its bearing bolts on MBB-BK117 D-3 and D-3m helicopters. It mandates repetitive inspections of the swashplate bolts, specifically those with Part Number D623M2050206, to detect excessive wear that could compromise helicopter control.

Jun 30, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117MBB-BK117 D-3MBB-BK117 D-3m

EASA AD 2026-0125-E

Landing Gear – Nose landing Gear Hydraulic Actuator Rod End – Inspection

EASA Airworthiness Directive 2026-0125-E is an emergency directive addressing the inspection of the nose landing gear hydraulic actuator rod end on Diamond Aircraft Industries GmbH models DA 42, DA 42 M, DA 42 NG, and DA 42 M-NG aeroplanes. It mandates repetitive inspections of specific affected parts with part numbers X11-0006-SMRCD10IRMR.7403 and X11-0006-GARSW-10RR to detect cracks that could cause rudder control issues. The directive also imposes operational limitations on go-around and touch-and-go maneuvers until initial inspections are completed.

Jun 29, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries DA 42Diamond Aircraft Industries GmbH DA 42Diamond Aircraft Industries GmbH DA 42 MDiamond Aircraft Industries GmbH DA 42 NGDiamond Aircraft Industries GmbH DA 42 M-NG

EASA AD 26-077

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items – Amendment

EASA Airworthiness Directive PAD No. 26-077 is a proposed amendment affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items, introducing new and more restrictive maintenance limitations. This directive ensures continued airworthiness by mandating compliance with the latest Airbus A380 ALS revision 14.

Jun 29, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 26-078

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2, Damage Tolerant Airworthiness Limitation Items – Amendment

EASA Airworthiness Directive PAD No. 26-078 is a proposed amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 2, specifically the Damage Tolerant Airworthiness Limitation Items (DT-ALI), to Revision 12. This directive ensures continued airworthiness by mandating compliance with the latest maintenance tasks and intervals.

Jun 29, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 26-079

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3, Certification Maintenance Requirements – Amendment

EASA Airworthiness Directive 26-079 is a proposed amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 3, Certification Maintenance Requirements, specifically Revision 08 of the Airbus A380 ALS. This directive mandates compliance with new and/or more restrictive maintenance tasks to ensure continued airworthiness of these aircraft models.

Jun 29, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 26-080

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4, System Equipment Maintenance Requirements – Amendment

EASA Airworthiness Directive PAD No. 26-080 is a proposed amendment concerning the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 4, System Equipment Maintenance Requirements (SEMR) to Revision 17. This directive mandates compliance with new and more restrictive maintenance tasks and life limits to ensure continued airworthiness.

Jun 29, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861