EASA Regulations & Airworthiness Directives

Browse 5,156 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350222 Airbus A330220 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941132 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787114 Show all...

EASA AD US-2026-18-07

Oct 7, 2026

Fuselage - Fuselage Skin, Bear Strap and Stub Frame at the Forward Galley Door Cutout - Inspection

The Federal Aviation Administration's Airworthiness Directive 2026-18-07 addresses certain Boeing Model 737-8, 737-9, and 737-8200 airplanes. This final rule mandates inspections and on-condition actions to detect and repair cracks in the fuselage skin, bear strap, and stub frame at the forward galley door cutout. The directive aims to maintain structural integrity and ensure continued airworthiness of affected aircraft.

Airworthiness Directive

Boeing 7378 (MAX)8200 (MAX)9 (MAX)898200

EASA AD CF-2026-48

Oct 7, 2026

Pneumatic – 10th and 14th Stage Bleed Duct Damaged or Missing Insulation

The Canadian Airworthiness Directive CF-2026-48 addresses missing or damaged insulation on the 10th and 14th stage bleed air ducts of Mitsubishi Heavy Industries RJ Aviation ULC (formerly Bombardier Inc.) CL-600-2B19 aircraft. This directive mandates updated inspection and maintenance procedures to prevent structural integrity loss in the engine pylons caused by heat radiation from uninsulated bleed ducts.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
MHI RJ Aviation CL-600-2B19 (RJ 100)
MHI RJ Aviation CL-600-2B19 (RJ 440)
Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2B19

EASA PAD 26-120

Oct 6, 2026

Electrical Power – Emergency Electrical Network Management Unit – Modification / Re-Identification

EASA Airworthiness Directive PAD No. 26-120 is a proposed directive addressing the Emergency Electrical Network Management Unit (EENMU) on Airbus A350-941 and A350-1041 aeroplanes. It targets specific EENMU part numbers that may have incorrect firmware logic affecting the electrical power distribution system. The directive applies to all manufacturer serial numbers except those with Airbus modification 120968 incorporated during production.

Proposed AD

Airbus A3501041941

EASA AD 2026-0192

Oct 6, 2026

Fuselage – Tail Gearbox Fitting – Inspection

EASA Airworthiness Directive 2026-0192 is an airworthiness directive addressing the inspection of the tail gearbox fitting Part Number 4F5350A04152 on Leonardo S.p.A. AW189 helicopters. It applies to all serial numbers of the AW189 and requires inspection for cracks and corrosion due to reported fatigue cracking caused by mechanical damage to the anti-corrosion coating. The directive mandates a one-time inspection and reporting to ensure continued airworthiness.

Airworthiness Directive

Leonardo S.P.A. Helicopters AW189
Leonardo AW189

EASA AD 2021-0139R2

Oct 2, 2026

Doors – Cabin Lateral Sliding Plug Door Emergency Jettisoning System – Inspection / Modification

The document titled "Doors – Cabin Lateral Sliding Plug Door Emergency Jettisoning System – Inspection / Modification" applies to AIRBUS HELICOPTERS models SA 330, AS 332, EC 225, AS 332 C, AS 332 C1, AS 332 L, and AS 332 L1. It addresses inspection and modification requirements for the emergency jettisoning system of the cabin lateral sliding plug doors on these helicopter types. The directive aims to ensure the proper functionality and safety of the emergency door jettisoning mechanism.

Airworthiness Directive

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 PAD 26-119

Oct 2, 2026

Oxygen – Oxygen Pressure Regulator – Inspection

EASA Airworthiness Directive Proposal PAD No. 26-119 addresses an inspection requirement for the oxygen pressure regulators installed on ATR 42 and ATR 72 aeroplanes. This directive targets passenger oxygen regulators with Part Number 112054-01, affecting various ATR 42-500 and ATR 72 series models. The directive aims to ensure proper oxygen flow by inspecting and correcting any improperly assembled regulators.

Proposed AD

ATR ATR42
ATR 500
ATR ATR72
ATR 101
ATR 102
ATR 201
ATR 202
ATR 211
ATR 212
ATR 212A
ATR 42
ATR 72

EASA AD 2026-0191-E

Oct 2, 2026

SUSPENSION OF FLIGHT OPERATIONS

EASA Airworthiness Directive 2026-0191-E is an emergency directive issued by the European Union Aviation Safety Agency that suspends all flight operations of Elixir aeroplanes, covering all manufacturer serial numbers. This directive follows a fatal accident involving an Elixir aeroplane and the subsequent grounding issued by the manufacturer. The directive is an interim safety measure pending further investigation results.

Airworthiness Directive

Elixir Aircraft Elixir
Elixir

EASA AD 2026-0190

Oct 1, 2026

Engine Oil – Oil Pump – Operational Prohibition

EASA Airworthiness Directive 2026-0190 is an operational prohibition directive affecting Rolls-Royce Deutschland RB211 Trent 800 series engines, specifically models 895-17, 892-17, 892B-17, 884-17, 884B-17, 877-17, and Trent 875-17 installed on aircraft such as the Boeing 777. The directive addresses oil pump issues related to certain part numbers that could lead to low oil pressure and potential dual in-flight engine shutdowns. It mandates restrictions on the installation and operation of affected oil pumps to ensure continued airworthiness.

Airworthiness Directive

Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 800
Boeing 777

EASA AD 2026-0189

Oct 1, 2026

Engine Oil – Oil Pump – Operational Prohibition

EASA Airworthiness Directive 2026-0189 is an operational prohibition directive affecting Rolls-Royce Deutschland Ltd & Co KG RB211 Trent 700 engines, specifically models Trent 768-60, 772-60, 772B-60, and 772C-60 installed on Airbus A330 aircraft. The directive addresses oil pump parts with specific part numbers that have been identified as non-serviceable due to potential failure modes leading to low oil pressure and possible dual in-flight engine shutdowns. It mandates restrictions on the installation and operation of affected oil pumps to ensure continued airworthiness and flight safety.

Airworthiness Directive

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

EASA SIB 2025-06R1

Oct 1, 2026

Potential Risk Management Issue after Engine Load Reduction Device Activation

EASA Safety Information Bulletin 2025-06R1 is an updated advisory addressing potential risk management issues following activation of the Load Reduction Device (LRD) on CFM International LEAP engines powering Boeing 737 Max and Airbus A320 NEO family aircraft. The bulletin highlights incidents where LRD activation after bird strikes caused oil leakage into the Environmental Control System (ECS), resulting in smoke in the cabin and flight deck. It provides information on the nature of the hazard, affected aircraft systems, and interim mitigation measures.

Safety Information Bulletin

CFM International LEAP-1A
CFM International LEAP-1C
CFM International LEAP-1A23
CFM International LEAP-1A24
CFM International LEAP-1A24E1
CFM International LEAP-1A26
CFM International LEAP-1A26CJ
CFM International LEAP-1A26E1
CFM International LEAP-1A29
CFM International LEAP-1A29CJ
CFM International LEAP-1A30
CFM International LEAP-1A32
CFM International LEAP-1A32X
CFM International LEAP-1A33
CFM International LEAP-1A33B2
CFM International LEAP-1A33B2X
CFM International LEAP-1A33X
CFM International LEAP-1A35A
CFM International LEAP-1A35AX
CFM International LEAP-1B
CFM International LEAP-1B21
CFM International LEAP-1B23
CFM International LEAP-1B25
CFM International LEAP-1B27
CFM International LEAP-1B28
CFM International LEAP-1B28B1
CFM International LEAP-1B28B2
CFM International LEAP-1B28B2C
CFM International LEAP-1B28B3
CFM International LEAP-1B28BBJ1
CFM International LEAP-1B28BBJ2
Boeing 737 Max
Airbus A320 NEO

EASA CZIB CZIB-2026-09-R1

Sep 30, 2026

Airspace of Saudi Arabia

The document titled Airspace of Saudi Arabia is a safety information bulletin issued by EASA concerning the FIR Jeddah (OEJD) airspace at all altitudes. It highlights increased risks due to ongoing military conflict and recent missile and drone attacks targeting aviation and infrastructure within Saudi Arabia, particularly affecting areas including Riyadh, Tabuk, Medina, and Yanbu. The bulletin applies to EU air operators and third country operators authorized by EASA operating in or through this airspace.

Safety Information Bulletin

All aircraft

EASA AD 2026-0188

Sep 30, 2026

Instruments – Warning Unit Emergency Off Switches – Operational Check

EASA Airworthiness Directive 2026-0188 is issued for Airbus Helicopters Deutschland GmbH EC135, EC635, and MBB-BK117 helicopter models. It addresses potential failures of emergency off switches in the warning units that could lead to engine shutdown or loss of fuel shut-off capability. The directive mandates operational checks and possible replacement of affected warning units to ensure continued airworthiness.

Airworthiness Directive

Airbus Helicopters EC135
Airbus Helicopters 635
Airbus Helicopters MBB-BK 117
Airbus Helicopters EC635
MBB-BK117

EASA AD 2026-0187

Sep 29, 2026

Equipment / Furnishing – Cargo Hook Barrel Nuts and Retainers – Inspection

EASA Airworthiness Directive 2026-0187 is an airworthiness directive addressing Leonardo AW169 helicopters, specifically those with serial numbers listed in the directive's appendix. It mandates inspection of cargo hook barrel nuts and retainers, part number 6F5310A07112, to ensure correct installation and prevent potential damage to structural elements and electrical cables in the underfloor area.

Airworthiness Directive

Leonardo S.P.A. Helicopters AW169
Leonardo AW169

EASA PAD 26-118

Sep 29, 2026

Fire Protection – Fire-extinguishing Pipes – Replacement

EASA Airworthiness Directive Proposal 26-118 addresses a safety issue on Airbus A380-861 aeroplanes equipped with EA GP7200 engines. It concerns the replacement of fire-extinguishing pipes, specifically part number L2621011100200, located in the core zone of each engine pylon. The directive aims to improve fire protection by mandating the installation of redesigned fire-extinguishing pipes.

Proposed AD

Airbus A380

EASA AD 2026-0185

Sep 29, 2026

Flight Controls – Angle of Attack Probes – Functional Checks

Flight Controls – Angle of Attack Probes – Functional Checks is a regulatory document applicable to ATR ATR42 and ATR72 aircraft types. It addresses the procedures and requirements for performing functional checks on the angle of attack probes, which are critical components of the flight control system. The document ensures that these probes operate correctly to maintain flight safety and control accuracy.

Other

ATR ATR42
ATR ATR72

EASA AD 2026-0186

Sep 29, 2026

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2026-0186 is an amendment addressing time limits and maintenance checks for SAFRAN Helicopter Engines RTM 322-01/9 and RTM 322-01/9A models, commonly installed on NH Industries NH90 military helicopters. This directive updates the Airworthiness Limitations Section (ALS) in the engine maintenance manuals to ensure continued airworthiness. It mandates compliance with new and/or more restrictive maintenance tasks and life limits.

Airworthiness Directive

Safran RTM 322
NH Industries NH90

EASA PAD 26-117

Sep 28, 2026

Fuel – Hoses – Inspection / Replacement

EASA Airworthiness Directive Proposal 26-117 is a regulatory document addressing fuel hose inspection and replacement for DG Aviation GmbH DG-500 M, DG-500 MB, and DG-800 B powered sailplanes. It targets the 40mm fuel hose fixed to the primer valve, requiring inspection and replacement to prevent fuel leakage and potential fire risk. This directive applies to all serial numbers except DG-800 B sailplanes modified per DG Flugzeugbau GmbH Technical Note 800/41 Instruction 4.

Proposed AD

Dg Aviation Gmbh DG-500
Dg Aviation Gmbh DG-800
DG Aviation GmbH DG-500 M
DG Aviation GmbH DG-500 MB
DG Aviation GmbH DG-800 B

EASA AD CF-2026-47

Sep 28, 2026

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

Canadian Airworthiness Directive CF-2026-47 addresses 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 the right-hand wing access panel stiffener is trimmed and that both left-hand and right-hand access panels of correct thickness are installed to prevent potential fuel tank ignition risks. This AD applies to all serial numbers of the specified models and supersedes a previous directive issued in 2025.

Airworthiness Directive

De Havilland Canada DHC-8
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 SIB 2026-07R2

Sep 25, 2026

EASA Safety Publication Tool – Log of Revisions

EASA Safety Information Bulletin 2026-07R2 is an airworthiness bulletin that updates the EASA Safety Publication Tool taxonomy with changes effective from 01 June 2026. It includes updates to Type Certificate Holder names and additions of new aircraft types such as the Epic Aircraft LLC E1000 and Pilatus PC12/47G. Affected aircraft types include models from DAHER AIRCRAFT SAS, ONTIC ENGINEERING AND MANUFACTURING, INC., DE HAVILLAND AIRCRAFT OF CANADA LTD., and others.

Safety Information Bulletin

Epic Aircraft LLC E1000
Pilatus PC12/47G
DAHER AIRCRAFT SAS
ONTIC ENGINEERING AND MANUFACTURING INC.
DE HAVILLAND AIRCRAFT OF CANADA LTD.

EASA PAD 26-116

Sep 25, 2026

Equipment / Furnishings – System Interface Unit – Replacement

EASA Airworthiness Directive Proposal 26-116 is a regulatory document addressing Airbus Helicopters H160-B helicopters. It mandates the replacement of the System Interface Unit (SIU) Part Number 704A45751326 to ensure continued airworthiness and safety. The directive clarifies maintenance intervals and overhaul requirements for this critical component.

Proposed AD

Airbus Helicopters H160B