EASA Regulations & Airworthiness Directives

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

EASA PAD 26-082

Jul 2, 2026

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.

Proposed AD
  • Deutsche Aircraft Gmbh Dornier 328
  • Dornier 328-100

EASA PAD 26-081

Jul 1, 2026

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.

Proposed AD
  • Dassault Fan Jet Falcon
  • Dassault Mystère-Falcon 20
  • Dassault Mystère-Falcon 20GF
  • Dassault 200
  • Dassault Mystère-Falcon 20-( )5
  • Dassault Mystère-Falcon 200
  • Dassault 20 GF

EASA AD 2026-0124

Jul 1, 2026

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.

Airworthiness Directive
  • Tecnam P2006T
  • Tecnam P2006T NG

EASA AD US-2026-13-17

Jul 1, 2026

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.

Airworthiness Directive
  • Boeing 737898200

EASA AD US-2026-13-15

Jul 1, 2026

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.

Airworthiness Directive
  • Boeing 707
  • Boeing 717
  • Boeing 727
  • Boeing DC-10
  • Boeing DC-8
  • Boeing DC-9
  • Boeing MD-10
  • Boeing MD-11
  • Boeing MD-88
  • Boeing MD-90
  • McDonnell Douglas DC-8
  • McDonnell Douglas DC-9
  • McDonnell Douglas DC-10
  • McDonnell Douglas MD-10
  • McDonnell Douglas MD-11
  • McDonnell Douglas MD-81
  • McDonnell Douglas MD-82
  • McDonnell Douglas MD-83
  • McDonnell Douglas MD-84
  • McDonnell Douglas MD-85
  • McDonnell Douglas MD-86
  • McDonnell Douglas MD-87
  • McDonnell Douglas MD-88
  • McDonnell Douglas MD-90-30

EASA AD US-2026-13-16

Jul 1, 2026

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.

Airworthiness Directive
  • Boeing 757
  • Boeing 767

EASA AD US-2026-13-02

Jul 1, 2026

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.

Airworthiness Directive
All aircraft

EASA AD 2026-0126-CN

Jun 30, 2026

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.

Airworthiness Directive
  • Dassault Falcon 2000
  • Dassault Mystère-Falcon 900
  • Dassault Aviation Mystère-Falcon 900
  • Dassault Aviation Falcon 2000

EASA AD 2026-0125R1

Jun 30, 2026

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.

Airworthiness Directive
  • Diamond Aircraft Industries DA 42
  • Diamond Aircraft Industries GmbH DA 42
  • Diamond Aircraft Industries GmbH DA 42 MNG
  • Diamond Aircraft Industries GmbH DA 42 NG

EASA AD 2026-0127

Jun 30, 2026

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.

Airworthiness Directive
  • Airbus Helicopters MBB-BK 117
  • MBB-BK117 D-3
  • MBB-BK117 D-3m

EASA AD 2026-0125-E

Jun 29, 2026

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.

Airworthiness DirectiveSuperseded
  • Diamond Aircraft Industries DA 42
  • Diamond Aircraft Industries GmbH DA 42
  • Diamond Aircraft Industries GmbH DA 42 MNG
  • Diamond Aircraft Industries GmbH DA 42 NG

EASA PAD 26-077

Jun 29, 2026

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.

Proposed AD
  • Airbus A380

EASA PAD 26-078

Jun 29, 2026

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.

Proposed AD
  • Airbus A380841842861

EASA PAD 26-079

Jun 29, 2026

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.

Proposed AD
  • Airbus A380841842861

EASA PAD 26-080

Jun 29, 2026

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.

Proposed AD
  • Airbus A380841842861

EASA AD 2025-0288R1

Jun 26, 2026

Engine – Low Pressure Compressor Blades – Removal from Service

EASA Airworthiness Directive 2025-0288R1 is an updated regulatory requirement addressing the removal from service of certain low pressure compressor blades installed on Rolls-Royce Deutschland RB211 Trent 700 engines, commonly found on Airbus A330 aircraft. The directive identifies specific part numbers and serial numbers of affected compressor blades that have undergone non-conforming repairs, posing a risk of blade cracking and potential engine failure. It mandates inspections, removal, and replacement of these parts to ensure continued airworthiness.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700
  • Airbus A330

EASA AD 2026-0122

Jun 26, 2026

Flight Controls – Droop Nose Geared Rotary Actuator Ring – Inspection / Replacement

EASA Airworthiness Directive 2026-0122 is an airworthiness directive applicable to Airbus A350-941 and A350-1041 aeroplanes. It addresses inspection and replacement requirements for the droop nose geared rotary actuator ring, specifically part number 4776A0000-03, due to identified corrosion issues. The directive mandates inspection and corrective actions to ensure continued safe operation of the affected flight control components.

Airworthiness Directive
  • Airbus A3509411041

EASA AD CF-2026-33R1

Jun 25, 2026

Pneumatic – High Pressure Valve - Butterfly Clip Failure

The Pneumatic – High Pressure Valve - Butterfly Clip Failure Emergency Airworthiness Directive CF-2026-33R1 issued by Transport Canada applies to Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft models. It addresses the issue of missing or broken butterfly clips on high pressure valves that can cause bleed system isolation failure, hot air leakage, and potential structural damage. This directive mandates compliance with specific Minimum Equipment List (MEL) items to mitigate safety risks.

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

EASA AD 2025-0237R1

Jun 24, 2026

[Correction] Equipment / Furnishings – 80 VU Rack Attachments – Inspection / Repair

The document titled '[Correction] Equipment / Furnishings – 80 VU Rack Attachments – Inspection / Repair' is a correction notice related to Airbus S.A.S. aircraft models A318, A319, A320, and A321. It addresses inspection and repair procedures for the 80 VU rack attachments used in these aircraft. The correction ensures accurate maintenance guidelines for these specific equipment components.

Correction
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2026-0121-E

Jun 24, 2026

Engine – Propeller Gearbox – Inspection

EASA Airworthiness Directive 2026-0121-E is an emergency directive addressing the inspection of propeller gearboxes installed on BRP-Rotax 912, 912 i, and 914 series engines used in various general aviation aircraft. The directive mandates a one-time inspection to verify the presence of the oil spray nozzle assembly and securing screws in the propeller gearbox. It applies to all serial numbers of the affected engines and gearboxes as specified in the associated BRP-Rotax Alert Service Bulletin ASB-2026-001R00.

Airworthiness Directive
  • Brp-Rotax Gmbh & Co Kg 912 A
  • Brp-Rotax Gmbh & Co Kg 912 F
  • Brp-Rotax Gmbh & Co Kg 912 S
  • Brp-Rotax Gmbh & Co Kg 912 iSc
  • Brp-Rotax Gmbh & Co Kg 914 F