EASA Regulations & Airworthiness Directives

Browse 5,132 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350222Airbus A330220Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941132Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787114Show all...

EASA AD 2026-0120

Jun 23, 2026

Fuselage – Lateral Window Frame – Inspections

EASA Airworthiness Directive 2026-0120 is an airworthiness directive addressing inspections of the fuselage lateral window frame on Airbus A319, A320, and A321 NEO aircraft models. It mandates repetitive high frequency eddy current inspections of the horizontal upper stiffeners at fuselage frame 4 to detect cracks and requires corrective actions if discrepancies are found. This directive applies to specific MSN aircraft except those with certain Airbus modifications embodied in production.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A321 NEO

EASA AD CF-2026-33

Jun 23, 2026

Pneumatic – High Pressure Valve - Butterfly Clip Failure

The Pneumatic – High Pressure Valve - Butterfly Clip Failure Emergency Airworthiness Directive CF-2026-33 issued by Transport Canada applies to Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft models. This directive addresses the failure of butterfly clips on high pressure valves which may lead to bleed system isolation issues, hot air leaks, and potential structural overheating. It prohibits dispatching affected aircraft under certain Minimum Equipment List (MEL) items until corrective actions are taken.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus Canada BD-500-1A10
  • Airbus Canada BD-500-1A11

EASA AD CF-2026-07R1

Jun 22, 2026

Ice and Rain Protection – Engine Cowl Anti-Ice – Ejector Pipe Chafing

The Canadian Airworthiness Directive CF-2026-07R1 titled 'Ice and Rain Protection – Engine Cowl Anti-Ice – Ejector Pipe Chafing' applies to all serial numbers of the MHI RJ Aviation ULC model CL-600-2B19 aircraft. It addresses chafing damage to the engine cowl anti-ice ejector pipe and seal, which can lead to system degradation, ice accumulation, and potential engine shutdown. The directive mandates inspections and corrective actions to ensure continued airworthiness.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • MHI RJ Aviation ULC CL-600-2B19

EASA AD CF-2026-09R1

Jun 22, 2026

Ice and Rain Protection – Engine Cowl Anti-Ice – Ejector Pipe Chafing

The Canadian Airworthiness Directive CF-2026-09R1 addresses ice and rain protection specifically concerning engine cowl anti-ice systems on MHI RJ Aviation ULC aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25. It mandates inspections and potential replacements of the reactive exhaust pipe and sealing joint to prevent damage caused by chafing, which could lead to ice accumulation, engine ingestion of ice, and engine shutdown.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • MHI RJ Aviation ULC CL-600-2C10
  • MHI RJ Aviation ULC CL-600-2C11
  • MHI RJ Aviation ULC CL-600-2D15
  • MHI RJ Aviation ULC CL-600-2D24
  • MHI RJ Aviation ULC CL-600-2E25

EASA AD CF-2026-27

Jun 22, 2026

Nacelles/Pylons – Upper and Side Pylon Link Assemblies - Replacement

Canadian Airworthiness Directive CF-2026-27 addresses the replacement of upper and side pylon link assemblies on Airbus Canada Limited Partnership model BD-500-1A11 and BD-500-1A10 aircraft. The directive targets assemblies potentially manufactured from incorrect titanium alloy material, which could compromise structural integrity. It mandates verification and replacement of affected parts to ensure continued airworthiness.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus Canada BD-500-1A11
  • Airbus Canada BD-500-1A10

EASA AD 2026-0118

Jun 22, 2026

Rotors Flight Control – Tail Rotor Actuator – Inspection

EASA Airworthiness Directive 2026-0118 is issued for Airbus Helicopters SA 365 N, SA 365 N1, AS 365 N2, and AS 365 N3 models. It addresses inspection and modification requirements for tail rotor actuators with part numbers 704A47135036 or 704A47135059 to prevent interference that could block tail rotor pedal control. The directive mandates inspections and modifications to ensure safe yaw control of affected helicopters.

Airworthiness Directive
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters SA 365 N
  • Airbus Helicopters SA 365 N1
  • Airbus Helicopters AS 365 N2
  • Airbus Helicopters AS 365 N3

EASA AD 2026-0119-E

Jun 22, 2026

Wings – Wing Mid Spars – Inspection

EASA Airworthiness Directive 2026-0119-E is an emergency directive addressing inspection requirements for the wing mid spars on Airbus A380-841, A380-842, and A380-861 aeroplanes with specific manufacturer serial numbers. It mandates special detailed inspections to detect cracks that could compromise wing structural integrity. The directive applies to certain serial numbers grouped into two categories with different compliance times.

Airworthiness Directive
  • Airbus A380

EASA PAD 26-074

Jun 19, 2026

Electrical Power – Direct Current Electrical Master Box – Inspection

EASA Airworthiness Directive PAD No. 26-074 is a proposed directive addressing the inspection of the direct current electrical master box on Airbus Helicopters AS 332 C, C1, L, and L1 models. It targets the printed circuit boards with part number GC11050 and serial numbers up to 400, aiming to prevent electrical short circuits that could affect the helicopter's DC power supply system.

Proposed AD
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 C
  • Airbus Helicopters AS 332 C1
  • Airbus Helicopters AS 332 L
  • Airbus Helicopters AS 332 L1

EASA AD 2026-0117

Jun 19, 2026

Engine – Low Pressure Turbine Discs – Inspection

EASA Airworthiness Directive 2026-0117 is an airworthiness directive addressing inspection requirements for Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft and potentially other types. It mandates inspections of low pressure turbine stage 3 and stage 4 discs, specifically parts with P/N KH36323 and KH33943, to detect cracks caused by rubbing contact with interstage static seals. The directive aims to prevent turbine disc failure and potential damage to the aircraft.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Boeing 787

EASA AD CF-2026-24

Jun 19, 2026

Fire Protection – Main Wheel Well Bin Sensing Element – Incompatible Connector Nut - Replacement

Canadian Airworthiness Directive CF-2026-24 addresses a fire protection issue related to the main wheel well bin sensing element on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. The directive mandates the replacement of incompatible connector nuts that have shown corrosion, which could compromise the fire detection system. This AD applies to specific serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus Canada BD-500-1A10
  • Airbus Canada BD-500-1A11

EASA AD CF-2026-25

Jun 19, 2026

Indicating/Recording System – Misleading Caution Messages Posted on Engine Indicating and Crew Alerting System during Air Driven Generator Deployment

Canadian Airworthiness Directive CF-2026-25 addresses misleading caution messages displayed on the Engine Indicating and Crew Alerting System (EICAS) during Air Driven Generator (ADG) deployment in MHI RJ Aviation ULC aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25. The directive mandates updates to the Aircraft Flight Manual (AFM) to correct message logic and clarify procedures during emergency power conditions.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • MHI RJ Aviation ULC CL-600-2C10
  • MHI RJ Aviation ULC CL-600-2C11
  • MHI RJ Aviation ULC CL-600-2D15
  • MHI RJ Aviation ULC CL-600-2D24
  • MHI RJ Aviation ULC CL-600-2E25

EASA AD US-2026-13-51

Jun 19, 2026

Power Plant - Engine Mount System - Inspection

Emergency Airworthiness Directive FAA AD 2026-13-51 addresses a critical safety issue affecting Gulfstream Aerospace Corporation Model GVIII-G700 and GVIII-G800 airplanes. The directive focuses on inspecting the engine mount system, specifically the engine thrust strut mounts, due to reports of broken hollow pin caps caused by missing or displaced sleeve bushings. This condition risks structural failure of the engine mount system and possible in-flight engine separation.

Airworthiness Directive
  • Gulfstream Aerospace Corporation GVIIIG700G800

EASA AD US-2026-12-07

Jun 18, 2026

Auto Flight - Mode Control Panel - Replacement

The Federal Aviation Administration's Airworthiness Directive 2026-12-07 is a final rule addressing certain Boeing 787-8, 787-9, and 787-10 airplanes. It mandates replacement of the existing mode control panel (MCP) with an updated version to prevent uncommanded changes to the MCP selected altitude. This directive aims to enhance flight safety by mitigating risks of controlled flight into terrain or mid-air collisions.

Airworthiness Directive
  • Boeing 7878910

EASA PAD 26-076

Jun 18, 2026

Flight Controls – Maintenance and Avionics Interface Computer Software – Modification; Airplane Flight Manual – Amendment

EASA Proposed Airworthiness Directive 26-076 addresses Dassault Aviation Falcon 7X aeroplanes, serial numbers 2 through 400 inclusive, that have not incorporated modification M1000. This directive focuses on maintenance and avionics interface computer software modifications and amendments to the Airplane Flight Manual to improve flight control safety. It supersedes a previous emergency AD and mandates software upgrades and procedural updates to ensure proper crew awareness of inboard slat configurations during flight.

Proposed AD
  • Dassault Falcon 7X

EASA PAD 26-075

Jun 18, 2026

Integrated Modular Avionics – Primus APEX DFZ Build 6.0 Software – Modification

EASA Airworthiness Directive PAD No. 26-075 is a proposed directive addressing the Primus APEX DFZ Build 6.0 software modification for Pilatus PC-24 aeroplanes, specifically those with manufacturer serial numbers 101 to 337 and 501 to 600. This directive targets the integrated modular avionics system to correct flight director calculation errors on affected aircraft. It applies to PC-24 aircraft equipped with earlier software versions and mandates software updates and flight manual amendments.

Proposed AD
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA PAD 26-073

Jun 17, 2026

Engine Oil – Lubrication / Scavenge Oil Pumps – Installation Criteria

EASA Airworthiness Directive PAD No. 26-073 is a proposed directive addressing installation criteria for lubrication and scavenge oil pumps on Rolls-Royce Trent 7000 series engines, which power Airbus A330 (NEO) aircraft. The directive applies to specific part numbers of oil pumps installed on Trent 7000-68, -70, -72, -72C, and -72D engines. It aims to ensure proper installation to prevent engine failures related to low oil pressure.

Proposed AD
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Airbus A330

EASA AD 2026-0095R1

Jun 17, 2026

Main Rotor Drive – Main Rotor Mast – Inspection

The document titled 'Main Rotor Drive – Main Rotor Mast – Inspection' is a regulatory instruction concerning the inspection of the main rotor drive and main rotor mast components specifically for GUIMBAL HELICOPTERES CABRI helicopters. It outlines inspection requirements to ensure the continued airworthiness and safety of these critical helicopter parts. The document is intended for operators and maintenance organizations responsible for these aircraft.

Airworthiness DirectiveSuperseded
  • Guimbal, Helicopteres CABRI
  • Guimbal Cabri

EASA AD US-2026-09-12

Jun 16, 2026

Fuselage - Aft Drain Mast Fuselage Skin - Inspections

The Federal Aviation Administration Airworthiness Directive 2026-09-12 is a final rule addressing certain Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates repetitive inspections of the fuselage skin and structure around the aft drain mast to detect cracks or corrosion. This directive aims to maintain structural integrity and prevent rapid decompression due to potential cracks beneath the aft drain mast.

Airworthiness Directive
  • Boeing 737100200200C300400500

EASA AD 2026-0116

Jun 15, 2026

Doors – Emergency Exit Rope on the Jettisonable Window Systems – Cleaning

EASA Airworthiness Directive 2026-0116 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters H160-B models. It addresses the cleaning and operational testing of the emergency exit rope on the jettisonable window systems to ensure proper functionality. The directive mandates maintenance actions to prevent blockage of the window jettison mechanism caused by contamination on the ropes.

Airworthiness Directive
  • Airbus Helicopters H160B

EASA AD 2026-0112

Jun 15, 2026

Fuel – Fuel Shut-off Valve – Inspection / Replacement

Fuel – Fuel Shut-off Valve – Inspection / Replacement is a maintenance document applicable to the GROB AIRCRAFT SE:G 109 type designation. It provides instructions and requirements for inspecting and, if necessary, replacing the fuel shut-off valve on this specific aircraft model. The document aims to ensure the continued airworthiness and safe operation of the G 109 by addressing potential issues with the fuel shut-off valve.

Airworthiness Directive
  • Grob Aircraft Se G 109