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EASA Regulations & Airworthiness Directives

Browse 5,132 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 787115 Show all...

EASA AD 2025-0200

[Correction] Equipment / Furnishings — Passenger Seats — Modification

EASA Airworthiness Directive 2025-0200 is a correction issued by the European Union Aviation Safety Agency addressing passenger seat modifications on Dassault Aviation Mystère-Falcon 900, Falcon 900EX, Falcon 2000, Falcon 2000EX, and Falcon 7X aeroplanes. The directive targets specific single and double seat assemblies identified by part and serial numbers that have exhibited unsafe sliding without passenger input. It mandates modification or replacement of affected seats to ensure continued airworthiness and passenger safety.

Airworthiness Directive

Dassault Falcon 2000
Dassault Falcon 7X
Dassault Falcon 900EX
Dassault MystÃ¨re-Falcon 900

EASA AD 2025-0214

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Part 2 / Damage Tolerant Airworthiness Limitation Items — Amendment

The document titled 'Time Limits / Maintenance Checks — Airworthiness Limitations Section — Part 2 / Damage Tolerant Airworthiness Limitation Items — Amendment' is an amendment concerning the Airbus A300-600 aircraft. It addresses updates to the airworthiness limitations related to damage tolerant airworthiness limitation items, which are critical for maintaining the structural integrity of the aircraft over time.

Airworthiness Directive

Airbus A300-600

EASA AD G-2025-0005

ACRO AIRCRAFT SEATING LIMITED: Series 9 Passenger Seats — Modification

The Civil Aviation Authority Airworthiness Directive G-2025-0005 addresses a safety issue with Acro Aircraft Seating Limited Series 9 Passenger Seats. It applies to specific seat part numbers listed in the directive and mandates inspections and modifications to prevent seatback pivot bolts from becoming loose. This directive ensures continued airworthiness and occupant safety for aircraft equipped with these seats.

Airworthiness Directive

EASA AD US-2025-19-13

Engine - High-Pressure Turbine 1st-stage and 2nd-stage Hubs - Replacement

The Federal Aviation Administration's Airworthiness Directive 2025-19-13 addresses certain International Aero Engines AG Model V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines. This directive mandates the removal and replacement of specific high-pressure turbine (HPT) 1st-stage and 2nd-stage hubs due to a quality escape identified during angled ultrasonic inspections. The AD aims to prevent potential uncontained failures that could lead to engine and aircraft damage.

Airworthiness Directive

International Aero Engines Ag V2500-( )5

EASA AD 2025-0197R1

Flight Controls — Primary Flight Control System — Modification

EASA Airworthiness Directive 2025-0197R1 is a regulatory update addressing the primary flight control system modification for Airbus A350-941 and A350-1041 aeroplanes. It focuses on the replacement and modification of Rudder and Elevator Flight Control Remote Modules (FCRMs) contaminated by hydraulic fluid and mandates the installation of updated Flight Control and Guidance System software standards. This directive ensures continued airworthiness by mitigating risks of flight control surface runaway due to hydraulic contamination.

Airworthiness Directive

Airbus A350

EASA AD 2025-0213

Power Plant — Engine Mount Fitting — Inspections / Replacement

EASA Airworthiness Directive 2025-0213 is an airworthiness directive addressing inspections and replacement of engine mount fittings on Leonardo S.p.A. AW189 helicopters, specifically serial numbers 92001 to 92010. It targets corrosion issues found on the right-hand and left-hand engine external fittings, part numbers 8G5333A04351 and 8G5333A04551 respectively. The directive mandates repetitive inspections and potential replacement of these parts to ensure continued airworthiness.

Airworthiness Directive

Leonardo S.P.A. Helicopters AW189

EASA AD 2025-0211

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2025-0211 is an amendment concerning the time limits and maintenance checks in the Airworthiness Limitations Section for Pilatus PC-24 aeroplanes. This directive updates the mandatory maintenance tasks and life limits to ensure continued airworthiness of all PC-24 aircraft. It applies to all manufacturer serial numbers of the Pilatus PC-24 and references the latest approved Aircraft Maintenance Manual revisions.

Airworthiness Directive

Pilatus Aircraft PC-24

EASA AD 2025-0208

Flight Controls — Flight Control Primary Computer — Modification

Flight Controls — Flight Control Primary Computer — Modification is a regulatory document concerning the Airbus A330 aircraft. It addresses modifications related to the flight control primary computer system to enhance operational safety and reliability. The document applies specifically to the Airbus S.A.S. A330 type designation.

Airworthiness Directive

Airbus A330

EASA AD 2025-0209

Wings — Centre Wing Box and Belly Fairing Fasteners — Modification

EASA Airworthiness Directive 2025-0209 is an airworthiness directive applicable to Airbus A350-941 aeroplanes with manufacturer serial numbers 0005 through 0047. It addresses issues related to the centre wing box and belly fairing fasteners, specifically those fasteners with Part Number EN6115 code B. The directive mandates modifications to ensure structural integrity and compliance with safety standards.

Airworthiness Directive

Airbus A350

EASA AD 2025-0210

Wings — Centre Wing Box Fasteners — Replacement

EASA Airworthiness Directive 2025-0210 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes with specific manufacturer serial numbers. The directive addresses the replacement of centre wing box fasteners and the application of additional head nut cap protection to ensure continued airworthiness.

Airworthiness Directive

Airbus A350

EASA AD 2025-0212

Wings — Wing Rear Spars — Inspection

EASA Airworthiness Directive 2025-0212 is an airworthiness directive addressing inspection requirements for the wing rear spars on Airbus A380-841, A380-842, and A380-861 aeroplanes with specific manufacturer serial numbers. It mandates repetitive special detailed inspections of the wing outer rear spar top and bottom flanges to detect cracks that could compromise structural integrity. The directive applies to certain A380 aircraft and requires compliance with Airbus Service Bulletin A380-57-8263 Revision 01.

Airworthiness Directive

Airbus A380

EASA AD BR-2020-01-02R3

[Correction] Nacelles / Pylons - Engine Inboard and Outboard Pylon Lower Link Lugs - Inspection / Repair

Brazilian Airworthiness Directive AD No. 2020-01-02R3 is a regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) addressing inspection and repair requirements for engine inboard and outboard pylon lower link lugs on Embraer S.A. aircraft. The affected models include Embraer ERJ 170-100, ERJ 170-200, ERJ 190-100, ERJ 190-200, and ERJ 190-100 ECJ series airplanes. The directive mandates inspections, repairs, and modifications to prevent structural cracks that could compromise engine pylon integrity and aircraft safety.

Airworthiness Directive

Embraer ERJ 170
Embraer ERJ 190

EASA PAD 25-151

Rotors Flight Control — Tail Rotor Actuator — Inspection

EASA Airworthiness Directive PAD No. 25-151 is a proposed directive addressing inspection and modification requirements for the tail rotor actuator on Airbus Helicopters SA 365 and AS 365 models, including SA 365 N, N1, and AS 365 N2 and N3 variants. The directive focuses on inspecting and modifying the routing of the tail rotor actuator harness to prevent interference that could block tail rotor pedal control. This affects helicopters with tail rotor actuators having part numbers 704A47135036 or 704A47135059.

Airbus Helicopters SA
Airbus Helicopters AS 365
Airbus Helicopters EC 155

EASA AD 2024-0241R1

Fuselage - Frames / Inner Flange Couplings - Inspection

The document titled 'Fuselage - Frames / Inner Flange Couplings - Inspection' is an explanatory statement provided by EASA regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aircraft. Since there are currently no Airbus A400M aeroplanes in civil service, no public AD exists. The document serves as an informational record intended for military airworthiness authorities and design approval holders, recommending that military authorities issue their own applicable ADs.

Airbus Military A400M

EASA AD 2025-0174R1

Fuselage — Rear Structure / Rear Frame — Inspection

Fuselage — Rear Structure / Rear Frame — Inspection is a regulatory document concerning the inspection requirements for the rear structure and rear frame of AIRBUS HELICOPTERS DEUTSCHLAND EC135 and EC635 helicopter models. It provides guidance on maintaining the structural integrity of these specific helicopter fuselage components to ensure continued airworthiness and safety.

Airworthiness Directive

Airbus Helicopters EC135
Airbus Helicopters 635

EASA AD 2025-0203

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 4 — System Equipment Maintenance Requirements — Amendment

EASA Airworthiness Directive 2025-0203 is an amendment addressing the Airbus A350-941 and A350-1041 aeroplanes. It updates the Airworthiness Limitations Section Part 4 related to System Equipment Maintenance Requirements to ensure continued airworthiness. This directive applies to all manufacturer serial numbers of the affected Airbus A350 models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0204

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

EASA Airworthiness Directive 2025-0204 is an amendment addressing the Airbus A350-941 and A350-1041 aeroplanes. It updates the Damage Tolerant Airworthiness Limitation Items in the Airbus A350 Airworthiness Limitations Section (ALS) Part 2, Revision 11, to ensure continued airworthiness through revised maintenance tasks and intervals. This directive applies to all manufacturer serial numbers of the specified Airbus A350 models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0201

Aeroplane Flight Manual — Section Normal Procedures / Loss of Avionics — Engine Indications During Engine Start — Amendment

EASA Airworthiness Directive 2025-0201 is an amendment concerning Pilatus PC-12/47E aeroplanes with manufacturer serial numbers 1720 and 2001 to 2999 inclusive. It addresses an issue during engine start where battery voltage drops cause avionics shutdown, resulting in loss of engine parameter indications including Interstage Turbine Temperature (ITT). This directive mandates updates to the Aeroplane Flight Manual to enhance engine start procedures.

Airworthiness Directive

Pilatus Aircraft PC-12

EASA SIB SAIB-2025-08

Indicating/Recording System - Erroneous Illumination of Cabin Altitude Warning Lights in High Altitude Landing Mode

The Special Airworthiness Information Bulletin SAIB: 2025-08 is an FAA advisory addressing erroneous illumination of cabin altitude warning lights in high altitude landing mode on Boeing 737-700 and 737-800 series airplanes with specific serial numbers. This bulletin provides information and recommended corrective actions but does not mandate compliance. It highlights issues related to wiring errors in previous Boeing Alert Service Bulletins affecting the cabin altitude warning system.

Safety Information Bulletin

Boeing 737

EASA AD 2025-0202

Landing Gear — Nose Landing Gear Retraction Actuator — Inspection

EASA Airworthiness Directive 2025-0202 is an airworthiness directive addressing the nose landing gear retraction actuator on Airbus A330 and A340 aeroplanes. It applies to specific part numbers and serial numbers of the nose landing gear retraction actuator, requiring inspection due to potential disconnection risks. The directive targets all manufacturer serial numbers of affected A330 and A340 models.

Airworthiness Directive

Airbus A330
Airbus A340