EASA Regulations & Airworthiness Directives

Browse 4968 EASA regulations with AI-powered summaries.

EASA AD 26-073

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.

Jun 17, 2026
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000Airbus A330

EASA AD 2026-0095R1

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.

Jun 17, 2026
Airworthiness DirectiveMaintenanceSafety MgmtGuimbal, Helicopteres CABRIGuimbal Cabri

EASA AD US-2026-09-12

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.

Jun 16, 2026
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD 2026-0116

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.

Jun 15, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters H160Airbus Helicopters H160-B

EASA AD 2026-0112

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.

Jun 15, 2026
Airworthiness DirectiveMaintenanceSafety MgmtGrob Aircraft Se G 109

EASA AD 2026-0115

Stabilizers – Torque Tube Assembly – Inspection

EASA Airworthiness Directive 2026-0115 is issued for Leonardo S.p.A. A109 series helicopters including A109A, A109AII, A109C, A109E, A109K2, A109LUH, A109S, and AW109SP models. It mandates inspections of the horizontal stabilizer torque tube assembly to detect debonding issues that could lead to cracks and potential loss of the horizontal stabilizer. The directive applies to specific part numbers and serial numbers of torque tube assemblies as detailed in the document.

Jun 15, 2026
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A109ALeonardo A109AIILeonardo A109CLeonardo A109ELeonardo A109K2Leonardo A109LUHLeonardo A109SLeonardo AW109SP

EASA AD 2023-0147R3

Time Limits / Maintenance Checks – Main Gearbox Suspension Bar Pins / Fittings – Re-calculation of Life Limits / Replacement / Modification; Fuselage – Main Gearbox Suspension Bar Pins / Fittings – Replacement / Modification

The document titled 'Time Limits / Maintenance Checks – Main Gearbox Suspension Bar Pins / Fittings – Re-calculation of Life Limits / Replacement / Modification; Fuselage – Main Gearbox Suspension Bar Pins / Fittings – Replacement / Modification' is an airworthiness directive applicable to Airbus Helicopters models SA 330, AS 332, and EC 225. It addresses the maintenance and life limits of main gearbox suspension bar pins and fittings, including recalculations and required replacements or modifications. The directive ensures continued airworthiness and safety of the affected helicopter models by updating maintenance requirements.

Jun 15, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA SIB 2026-06

Ebola Virus Disease – Operational Recommendations

EASA Safety Information Bulletin 2026-06 titled "Ebola Virus Disease – Operational Recommendations" provides updated guidance on managing the operational safety environment related to the Ebola Bundibugyo virus disease outbreak. It applies to national competent authorities, aircraft operators, and aerodrome operators, focusing on risk management, infection control, and procedures for suspected cases during commercial air travel. The document does not reference specific aircraft or engine models.

Jun 12, 2026
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2026-0114

Landing Gear – Main Landing Gear Axles – Inspections

EASA Airworthiness Directive 2026-0114 is an airworthiness directive addressing inspections of main landing gear axles on Airbus A350-1041 aeroplanes. It applies to specific main landing gear axles with designated part numbers and requires repetitive detailed inspections to detect corrosion damage. The directive provides instructions for inspection and corrective actions to maintain continued airworthiness.

Jun 12, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-1041

EASA AD 2026-0113

Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment

EASA Airworthiness Directive 2026-0113 is an amendment concerning Rolls-Royce Trent XWB engines installed on Airbus A350 aircraft, including models Trent XWB-75, XWB-79, XWB-79B, XWB-84, and XWB-97. This directive updates the Time Limits Manual and Maintenance Programme to ensure continued airworthiness through mandatory maintenance tasks and life limits. It applies to all serial numbers of the affected engines.

Jun 11, 2026
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350

EASA AD 2026-0110

[Correction] Fuselage – Screws and Nuts installed on Firewalls – Inspection

EASA Airworthiness Directive 2026-0110 is a corrective directive addressing Airbus Helicopters EC 175 B models manufactured before 19 November 2025. It mandates inspection of screws and nuts installed on the firewalls between the engine compartment and the electronic engine control units (EECU) and main gearbox (MGB) compartments for incorrectly applied high-temperature sealant. The directive aims to prevent potential ignition of the sealant that could lead to fires and engine power loss.

Jun 10, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC 175 B

EASA AD US-2026-10-02

Fuselage - Airworthiness Limitations Section - Maintenance / Inspection

Fuselage - Airworthiness Limitations Section - Maintenance / Inspection is a final rule airworthiness directive issued by the Federal Aviation Administration (FAA) addressing certain Honda Aircraft Company LLC Model HA-420 airplanes. This directive mandates updates to the Airworthiness Limitations Section (ALS) of the maintenance manual to include inspections for tool damage on the interior fuselage skin fiber at the forward pressure bulkhead ring angle. The directive aims to prevent crack propagation that could lead to pressurization leaks and loss of pressurization.

Jun 10, 2026
Airworthiness DirectiveMaintenanceSafety MgmtHonda Aircraft Company HA-420

EASA AD 2026-0111

Tail Rotor Drive - Shaft Sleeves – Inspection

EASA Airworthiness Directive 2026-0111 is an airworthiness directive addressing the inspection of tail rotor drive shaft sleeves on Airbus Helicopters AS 350 B2, AS 350 B3, EC 130 B4, and EC 130 T2 models, excluding those with modification 079809. The directive mandates repetitive inspections of specific tail rotor drive shaft sleeves, part number 704A33698045, to detect damage caused by increased hardness due to high temperatures. This AD aims to prevent potential failure of the tail rotor drive shaft and loss of yaw control.

Jun 10, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 350 B2Airbus Helicopters AS 350 B3Airbus Helicopters EC 130 B4Airbus Helicopters EC 130 T2

EASA AD 2026-0060R1

Fuel – Fuel Low Pressure Shut-Off Valve – Leak Check

EASA Airworthiness Directive 2026-0060R1 is a regulatory update addressing fuel low pressure shut-off valve (LPSOV) leak checks on Airbus A330 and A340 aeroplanes. It applies to specific Airbus A330 and A340 models equipped with affected LPSOV parts identified by certain part numbers. The directive mandates repetitive leak checks and corrective actions to prevent fuel leaks that could lead to fire hazards.

Jun 9, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD US-2026-10-05

Goodrich Cabin Attendant Seats - Replacement

The Federal Aviation Administration's Airworthiness Directive 2026-10-05 is a final rule addressing Goodrich cabin attendant seats installed on various Airbus SAS Model A330 and A340 series airplanes. This directive requires replacing non-compliant seat track attachments and hardware and re-identifying the seats with new part numbers to ensure compliance with safety standards. The affected aircraft include Airbus A330-200, A330-300, A330-743L, A330-841, A330-941, A340-200, A340-300, A340-541, A340-542, A340-641, and A340-642 models.

Jun 8, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330-200Airbus A330-300Airbus A330-743LAirbus A330-841Airbus A330-941Airbus A340-200Airbus A340-300Airbus A340-541Airbus A340-542Airbus A340-641Airbus A340-642

EASA AD 2026-0107

Navigation – Radio Altimeter and Ground Proximity System Antennas – Modification

EASA Airworthiness Directive 2026-0107 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Defence and Space C-295 aeroplanes with manufacturer serial numbers 188, 189, and 191. The directive mandates modifications to the radio altimeter and ground proximity system antenna installations to ensure structural integrity. This AD applies specifically to these aircraft models and requires compliance with Airbus Defence and Space service bulletins SB-295-34-0091C and SB-295-34-0092C.

Jun 8, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Defence & Space C-295Airbus Defence and Space C-295

EASA AD 2026-0109

Oxygen – Low Pressure Oxygen Hoses – Replacement

EASA Airworthiness Directive 2026-0109 is issued for MBB-BK117 D-2 and D-3 helicopters modified with EASA Supplemental Type Certificate 10051018 up to revision 5. It addresses the replacement of low-pressure oxygen hoses installed in Emergency Medical Service interiors manufactured by Mecaer Aviation Group. The directive mandates replacing specific oxygen hoses and assemblies to prevent potential oxygen leakage.

Jun 8, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117MBB-BK117 D-2MBB-BK117 D-3

EASA AD US-2026-11-05

Rotorcraft Flight Control - Auxiliary Servo Assembly - Inspections

The Federal Aviation Administration's Airworthiness Directive 2026-11-05 is a final rule addressing various helicopters including Sikorsky S-61 models and others. It mandates inspections and maintenance actions related to the auxiliary servo assembly and yaw pedal damper housing to prevent loss of tail rotor authority. This directive targets specific helicopter models such as Carson S-61L, Croman SH-3H, Glacier CH-3E, Reynolds USAF CH-3 variants, Sikorsky S-61 series, and Siller CH-3E and SH-3A helicopters.

Jun 8, 2026
Airworthiness DirectiveMaintenanceSafety MgmtSikorsky S-61Carson S-61LCroman SH-3HGlacier CH-3EReynolds USAF CH-3Siller CH-3ESiller SH-3A

EASA AD 2026-0104

Rotorcraft Flight Manual – Limitations Section – Amendment

EASA Airworthiness Directive 2026-0104 is an amendment to the Rotorcraft Flight Manual – Limitations Section for Airbus Helicopters H160-B models. It addresses a safety issue identified during HELIONIX software development flight tests related to the Automatic Flight Control System's Assisted Take-Off mode under One Engine Inoperative conditions. The directive mandates changes to the flight manual to enhance pilot limitations and ensure safe operation.

Jun 8, 2026
Airworthiness DirectiveFlight OpsSafety MgmtAirbus Helicopters H160Airbus Helicopters H160-B

EASA SIB SN-2026-005

Autopilots and Trim Runaways in General Aviation Aircraft

The Civil Aviation Authority Safety Notice SN–2026/005 Version 2 is a guidance document addressing autopilots and electric pitch trim runaways in General Aviation aircraft. It applies to all General Aviation pilots, operators, and organisations managing or maintaining GA aircraft equipped with autopilot or electric pitch trim systems. The notice highlights the importance of system checks, pilot training, and immediate actions in case of trim runaway events to enhance flight safety.

May 27, 2026
Safety Information BulletinFlight OpsMaintenanceTrainingSafety Mgmt