Browse 4983 EASA regulations with AI-powered summaries.
EASA AD 2025-0210
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.
EASA AD 2025-0212
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.
EASA AD BR-2020-01-02R3
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.
EASA AD 25-151
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.
EASA AD 2024-0241R1
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.
EASA AD 2025-0174R1
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.
EASA AD 2025-0203
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.
EASA AD 2025-0204
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.
EASA AD 2025-0201
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.
EASA SIB SAIB-2025-08
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.
EASA AD 2025-0202
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.
EASA AD CF-2025-48
Canadian Airworthiness Directive CF-2025-48 addresses insulation installation issues on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. The directive targets insufficient overlap of insulation blankets between frame 27 and 29 near STR 23 LH, which could compromise fire protection. It mandates replacement of specific insulation blanket part numbers to restore proper fire resistance.
EASA AD 2025-0199
EASA Airworthiness Directive 2025-0199 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Leonardo S.p.A. A119 and AW119MKII helicopters equipped with Pratt & Whitney Canada PT6B-37A engines. It mandates repetitive acceleration checks and replacement of the rear pneumatic line on affected engines to address potential fuel flow issues caused by trapped residues.
EASA SIB SAIB-2025-07
The FAA Special Airworthiness Information Bulletin SAIB: 2025-07 addresses airworthiness concerns related to the installation of the Belt-Driven Vortech V-1S supercharger assembly on certain Bellanca Model 17-30A and Cessna aircraft models, including 180K, 210-5(205), 210-5A(205A), A185F, P206B, TU206G, and U206B. The bulletin highlights issues with Supplemental Type Certificates SE10233SC and SA10232SC, which approve these modifications on specific Teledyne Continental Motors O-470 engine models and Cessna 182 variants. It is an informational bulletin and does not mandate regulatory action at this time.
EASA AD 2025-0194
EASA Airworthiness Directive 2025-0194 is a corrective directive addressing Airbus A380-841 and A380-842 aeroplanes equipped with Rolls-Royce RB211 Trent 900 engines. It mandates a modification to the primary flight control and guidance unit (FCGU) software to prevent uncommanded thrust reduction during soft go-around maneuvers. The directive applies to specific FCGU hardware and software part numbers identified in the document.
EASA AD 2025-0198
Power Plant — Right-Hand Engine Firewall — Modification is an airworthiness directive concerning the AIRBUS DEFENCE & SPACE S.A. CN-235 aircraft. This document addresses modifications to the right-hand engine firewall to ensure continued airworthiness and safety of the affected aircraft model.
EASA AD 2025-0151R2
EASA Airworthiness Directive 2025-0151R2 is an updated regulatory document addressing safety concerns related to the escape slide inflation reservoir regulator valve on Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It mandates inspection, modification, and replacement of affected reservoirs and orifice fittings to prevent uncommanded deployment of escape slides during flight. The directive applies to all manufacturer serial numbers of the specified aircraft models.
EASA AD CF-2025-47
Canadian Airworthiness Directive CF-2025-47 addresses the fuel distribution system on Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. It focuses on the twisted Motive Flow (MF) flexible fuel line assemblies installed in the pylon to wing area, which could lead to fuel leaks and fire risks. This directive applies to specific serial numbers of these aircraft models.
EASA AD 2025-0158R1
EASA Airworthiness Directive 2025-0158R1 is a regulatory update addressing inspection and replacement requirements for main landing gear door actuators on Airbus A318, A319, A320, and A321 aircraft models. It targets actuators with part number 114122015 and specific serial numbers identified in Airbus Alert Operators Transmission A32N033-24 Revision 02. The directive aims to prevent landing gear extension issues caused by actuator assembly errors.
EASA AD 2025-0196
EASA Airworthiness Directive 2025-0196 is an amendment addressing safety concerns for Airbus Helicopters EC 175 B models. It mandates inspections, modifications, and updates related to the integrated modular avionics Ethernet network and rotorcraft flight manual emergency procedures. The directive targets all EC 175 B helicopters except those with specific Airbus Helicopters modifications already embodied.