EASA Regulations & Airworthiness Directives

Browse 5,156 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 PAD 26-124

Oct 15, 2026

Doors – Forward and Aft Cargo Door Seals – Inspection / Replacement

EASA Airworthiness Directive Proposal 26-124 addresses inspection and replacement of forward and aft cargo door seals on Airbus A350-941 and A350-1041 aeroplanes. The directive targets specific cargo door seals with part numbers V0007007220200 and V0007007320200 that have been repaired using a maintenance procedure incorrectly published as a permanent repair. This proposal aims to ensure the integrity of cargo compartment fire extinguishing systems by mandating replacement of affected seals.

Proposed AD
  • Airbus A3501041941

EASA AD 2026-0177R1

Oct 15, 2026

Indicating / Recording Systems – Integrated Control Panels – Inspection

EASA Airworthiness Directive 2026-0177R1 is an updated regulatory requirement addressing inspection and potential replacement of Fire Integrated Control Panels (ICP) Part Number 727-7206-03 installed on Airbus A350-941 and A350-1041 aircraft. The directive mandates a general visual inspection to detect possible internal damage caused by mechanical shock that could lead to unintended engine in-flight shutdowns. It applies to all serial numbers of the affected Airbus A350 models.

Airworthiness Directive
  • Airbus A3501041941

EASA PAD 26-125

Oct 15, 2026

Pneumatic – Pylon / Wing Interface Bleed Duct and Fuel Pipe – Inspection / Modification / Replacement

EASA Airworthiness Directive 26-125 is a proposed directive addressing inspection, modification, and replacement of the pneumatic pylon/wing interface bleed duct and fuel pipe on Airbus A380-841, A380-842, and A380-861 aeroplanes. It targets specific bleed-air duct assemblies identified by part numbers related to the four wing-to-engine pylon interfaces. The directive aims to mitigate risks associated with bleed-air duct detachments and potential fuel leaks that could lead to fire hazards.

Proposed AD
  • Airbus A380841842861

EASA AD 2026-0196

Oct 13, 2026

Equipment / Furnishings – System Interface Unit – Replacement

EASA Airworthiness Directive 2026-0196 is issued for Airbus Helicopters H160-B models concerning the replacement of the System Interface Unit (SIU) Part Number 704A45751326. This directive addresses a discrepancy in the overhaul timing of the SIU, which is critical for beacon deployment in emergencies. The AD mandates replacement of affected SIUs to ensure continued airworthiness and safety.

Airworthiness Directive
  • Airbus Helicopters H160B

EASA PAD 26-123

Oct 13, 2026

Fuselage – Forward Fuselage Skin Panels – Inspection

EASA Airworthiness Directive PAD No. 26-123 is a proposed directive addressing inspection requirements for forward fuselage skin panels on Airbus A319, A320, and A321 aircraft models. It applies to specific serial numbers and panel part numbers identified in the directive. The directive focuses on detecting potential structural integrity issues caused by production quality deviations and certain repair conditions affecting the fuselage panels.

Proposed AD
  • Airbus A319153N
  • Airbus A320251N252N271N
  • Airbus A321251NX252NX271NX272NX

EASA AD 2026-0195

Oct 13, 2026

Tail Rotor Drive – Tail Gear Box Control Rod Bearings – Replacement / Life Limitation

EASA Airworthiness Directive 2026-0195 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus Helicopters SA 365 N models. It addresses the replacement and life limitation of tail gear box control rod bearings, specifically part number 360A33-4052-00, due to premature bearing spalling. This directive aims to ensure continued safe operation of the affected helicopters by mandating timely replacement of these components.

Airworthiness Directive
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters SA 365 N

EASA AD CF-2026-47R1

Oct 13, 2026

Wing – Wing Access Panels with Un-trimmed Stiffeners and/or Reduced Thickness - Inspection

Airworthiness Directive CF-2026-47R1 addresses inspection and modification requirements for wing access panels with un-trimmed stiffeners and/or reduced thickness on De Havilland Aircraft of Canada Limited model DHC-8 series 100, 200, and 300 aircraft. The directive focuses on ensuring that the right-hand wing access panel stiffener is trimmed and that correct thickness panels are installed to prevent potential ignition sources in the wing fuel tank. It applies to all serial numbers of the specified models.

Airworthiness Directive
  • De Havilland Canada DHC-8102103106201202301311314315
  • De Havilland Aircraft of Canada Limited DHC-8 series 100
  • De Havilland Aircraft of Canada Limited DHC-8 series 200
  • De Havilland Aircraft of Canada Limited DHC-8 series 300

EASA AD 2026-0194

Oct 12, 2026

Aircraft Flight Manual Supplement – Abnormal Procedures – Amendment

EASA Airworthiness Directive 2026-0194 is an amendment concerning Airbus A330 models modified with the Elbe Flugzeugwerke GmbH Passenger to Freighter conversion under EASA Supplemental Type Certificate 10063798. This directive addresses updates to the Aircraft Flight Manual Supplement related to abnormal procedures for these converted A330 aircraft. It applies to all serial numbers of the affected Airbus A330 variants modified up to Revision 41 of the STC.

Airworthiness Directive
  • Airbus A330201202203223243301302303321322323341342343

EASA AD CF-2026-49

Oct 12, 2026

Engine Controls – Throttle Quadrant Assembly – Throttle Lever Jamming - Replacement

Canadian Airworthiness Directive CF-2026-49 addresses a throttle lever jamming issue in the throttle quadrant assembly (TQA) of Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. The directive mandates replacement of affected TQAs due to a production torque defect causing thrust reverser lockout cam detachment. This AD ensures safe engine control by preventing throttle lever jamming during flight.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus BD-500-1A10 (A220-100)
  • Airbus BD-500-1A11 (A220-300)
  • Airbus Canada BD-500-1A10
  • Airbus Canada BD-500-1A11

EASA AD US-2026-19-04

Oct 12, 2026

Hydraulic Power - Alternating Current Motor Pump - Inspection

The Federal Aviation Administration (FAA) Airworthiness Directive 2026-19-04 is a final rule addressing all Boeing Model 777-200, -200LR, -300, -300ER, and 777F series airplanes. It targets the alternating current motor pump (ACMP) with part number 731966, which has been linked to an overheated condition causing a fire in the main landing gear wheel well. This directive mandates inspections and prohibits installation of affected ACMP parts to mitigate fire risk.

Airworthiness Directive
  • Boeing 777200200LR300300ER
  • Boeing 777F

EASA AD CF-2026-50

Oct 12, 2026

Tail Rotor – Tail Rotor Pitch Link Spherical Bearing Missing Hard Coating - Inspection

Canadian Airworthiness Directive CF-2026-50 addresses the issue of missing hard coating on the tail rotor pitch link spherical bearings installed on Bell Helicopter Textron Canada Limited model 429 helicopters, serial number 57001 and subsequent. The directive mandates repetitive visual inspections and replacement of affected tail rotor pitch link assemblies with part numbers 429-012-212-105 or 429-012-212-107 if wear or damage is detected. This AD aims to prevent loss of tail rotor directional control due to premature bearing wear.

Airworthiness Directive
  • Bell 429
  • Bell Helicopter Textron Canada Limited 429

EASA AD US-2026-20-12

Oct 12, 2026

Turbine - High-Pressure Turbine Interstage Seal - Replacement

The Federal Register document titled 'Turbine - High-Pressure Turbine Interstage Seal - Replacement' is a final rule airworthiness directive (AD 2026-20-12) issued by the FAA affecting Engine Alliance Model GP7270, GP7272, and GP7277 engines. It addresses an unsafe condition related to uncontained failure of the high-pressure turbine interstage seal, which was reported during an aborted takeoff on an Airbus A380 equipped with these engines. The AD mandates removal and replacement of certain high-cycle HPT interstage seals to prevent potential engine fire and aircraft damage.

Airworthiness Directive
  • Engine Alliance GP7200
  • Engine Alliance GP7270
  • Engine Alliance GP7272
  • Engine Alliance GP7277
  • Airbus A380

EASA PAD 26-122

Oct 9, 2026

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

EASA Airworthiness Directive 26-122 is a proposed amendment affecting Airbus A350-941 and A350-1041 aeroplanes. It updates the Damage Tolerant Airworthiness Limitation Items in the Airbus A350 Airworthiness Limitations Section Part 2, Revision 12, introducing new and more restrictive maintenance tasks. This directive ensures continued airworthiness by mandating compliance with updated maintenance requirements.

Proposed AD
  • Airbus A3501041941

EASA SIB SAIB-2026-17

Oct 9, 2026

Vertical Navigation Approach Disconnect Following Missed Approach

The FAA Aviation Safety Information Bulletin SAIB: 2026-17 titled "Vertical Navigation Approach Disconnect Following Missed Approach" informs operators of Boeing 737-600/-700/-800/-900/-900ER/-7/-8/-9/-8200 series airplanes equipped with Flight Management Computer software versions U14.0 or U14.1 about a potential vertical navigation (VNAV) mode disconnect during subsequent approaches after a missed approach. This bulletin provides information on the anomaly but does not mandate any regulatory action.

Safety Information Bulletin
  • Boeing 7376007008 (MAX)8008200 (MAX)9 (MAX)900900ER7898200

EASA PAD 26-121

Oct 8, 2026

Equipment / Furnishings – System Interface Unit – Replacement

EASA Airworthiness Directive Proposal 26-121 is a regulatory document addressing the replacement of the System Interface Unit (SIU) on Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 (except D-2m variant) and D-3 helicopters. The directive applies to SIU Manufacturer Part Number 503-24-6-G installed on helicopters with serial numbers 20001 to 20360 and 21001 to 21999. It aims to ensure continued airworthiness by mandating replacement of affected SIUs based on their time since manufacture or last overhaul.

Proposed AD
  • Airbus Helicopters MBB-BK 117
  • Airbus Helicopters MBB-BK 117 D-2
  • Airbus Helicopters MBB-BK 117 D-3
  • Airbus Helicopters MBB-BK117 D-2
  • Airbus Helicopters MBB-BK117 D-3

EASA AD 2020-0271R1

Oct 8, 2026

Main Rotor – Swashplate Boot – Inspection

EASA Airworthiness Directive 2020-0271R1 is an updated regulation addressing inspection requirements for the main rotor swashplate boot on Leonardo S.p.A. AB139, AW139, and AW189 helicopters. It focuses on the inspection and maintenance of the affected main rotor swashplate boot part number 3G6230V00251 and its bonded stainless steel external rings to prevent in-flight failures. The directive mandates detailed inspections and adhesive restoration to ensure continued airworthiness.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters AB139
  • Leonardo S.P.A. Helicopters AW139
  • Leonardo S.P.A. Helicopters AW189
  • Leonardo AB139
  • Leonardo AW139
  • Leonardo AW189

EASA AD US-2026-20-02

Oct 8, 2026

Master Minimum Equipment List - Amendment

The Master Minimum Equipment List - Amendment is a final rule airworthiness directive issued by the FAA affecting The Boeing Company Model 787-8 and 787-9 airplanes equipped with certain Rolls-Royce Deutschland Ltd & Co KG Trent 1000 engine variants. It addresses a safety concern related to the lack of data supporting engine operability when dispatched under MMEL item 75-33-01, which involves operating with an inoperative engine intermediate pressure bleed valve (IPBV).

Airworthiness Directive
  • Boeing 78789

EASA AD US-2026-19-01

Oct 7, 2026

[Correction] Rotorcraft flight control - Torque Tube Assembly and Roller Bearings - Replacement / Inspection

The document titled "[Correction] Rotorcraft flight control - Torque Tube Assembly and Roller Bearings - Replacement / Inspection" is a final rule correction to Airworthiness Directive (AD) 2026-19-01 issued by the Federal Aviation Administration (FAA). It applies to all MD Helicopters, LLC Model 369 series, 500N, and 600N helicopters. The AD mandates repetitive inspections and potential replacement of the torque tube assembly and roller bearings to ensure flight control safety.

Airworthiness Directive
  • Md Helicopters Inc (Mdhi) 369
  • Md Helicopters Inc (Mdhi) 369A
  • Md Helicopters Inc (Mdhi) 369D
  • Md Helicopters Inc (Mdhi) 369E
  • Md Helicopters Inc (Mdhi) 369F
  • Md Helicopters Inc (Mdhi) 369FF
  • Md Helicopters Inc (Mdhi) 369H
  • Md Helicopters Inc (Mdhi) 369HE
  • Md Helicopters Inc (Mdhi) 369HM
  • Md Helicopters Inc (Mdhi) 369HS
  • Md Helicopters Inc (Mdhi) 500N
  • Md Helicopters Inc (Mdhi) 600N
  • MD Helicopters 369
  • MD Helicopters 500N
  • MD Helicopters 600N

EASA AD US-2026-18-08

Oct 7, 2026

Fuselage - Cargo Track Crown Fitting - Inspection

Fuselage - Cargo Track Crown Fitting - Inspection is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2026-18-08) addressing certain Boeing 767-300F series airplanes. This directive requires inspection and possible replacement of titanium cargo track crown fittings due to suspect material certifications. The AD aims to prevent cargo track failure that could compromise airplane controllability and damage critical systems in the main cargo compartment.

Airworthiness Directive
  • Boeing 767300F