Browse 216 EASA regulations with AI-powered summaries.
EASA AD 2025-0106
EASA Airworthiness Directive 2025-0106 is an airworthiness directive issued by EASA concerning Airbus A350-1041 aeroplanes. It mandates inspection of the primary structure of the left-hand and right-hand pylons for missing chamfers under critical fastener heads. This directive applies specifically to certain manufacturer serial numbers of the Airbus A350-1041 model.
EASA AD 2025-0100
EASA Airworthiness Directive 2025-0100 is an airworthiness directive affecting Airbus A350-1041 aeroplanes equipped with Rolls-Royce Trent XWB-97 engines. It addresses the replacement and modification of hydro-mechanical units (HMU) with specific part numbers to prevent engine transient N1 shaft speed exceedance caused by worn Combining Spill Valve (CSV) pistons. The directive mandates compliance with Airbus and Rolls-Royce service instructions to ensure continued safe operation.
EASA AD 2025-0099
EASA Airworthiness Directive 2025-0099 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses the replacement and maintenance requirements of Flight Control Remote Modules (FCRM) due to hydraulic fluid contamination risks. The directive applies to specific FCRM part numbers and aims to prevent potential loss of control of rudder, elevator, or aileron surfaces.
EASA AD 2025-0095
EASA Airworthiness Directive 2025-0095 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes with specific manufacturer serial numbers. It mandates inspections of the main landing gear brake rod center pin and nut sub-assemblies to detect corrosion and potential detachment risks. The directive aims to ensure continued airworthiness and prevent landing gear extension failures.
EASA AD 2025-0093
EASA Airworthiness Directive 2025-0093 is an airworthiness directive affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates functional checks of the nose landing gear (NLG) shock absorber sliding piston assemblies with specific part numbers to address potential mechanical noise and corrosion issues. The directive applies to certain NLG piston assemblies identified by part numbers 6407A2000-01, 6407A2000-02, 6407A2000-03, 5035A3200-01, and 5035A3200-02.
EASA AD 2025-0073
EASA Airworthiness Directive 2025-0073 is an airworthiness directive addressing inspection requirements for the horizontal tail plane lateral load fitting bushings on Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 114806. The directive mandates repetitive detailed inspections of affected bushings to detect migration and potential damage. It applies to all manufacturer serial numbers of the specified models and provides instructions for corrective actions and optional modification as terminating action.
EASA AD 2025-0035
EASA Airworthiness Directive 2025-0035 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 116830 incorporated in production. The directive addresses issues related to hydraulic engine driven pumps and requires a software update to the Hydraulic Monitoring and Control Application (HMCA) to enhance protection against overheating. This directive is effective from 26 February 2025.
EASA AD 2019-0207R2
EASA Airworthiness Directive 2019-0207R2 is an updated safety directive addressing inspection requirements for the passenger and crew door girt bar fitting assemblies on Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 115327. The directive mandates repetitive detailed inspections of affected girt bar fitting assemblies with part numbers V5217170000000 or V5217170000100 to detect potential safety hook jamming issues. It aims to prevent possible failure of passenger door slide deployment during emergencies.
EASA AD 2025-0008
EASA Airworthiness Directive 2025-0008 is an airworthiness directive applicable to Airbus A350-941 and A350-1041 aeroplanes. It addresses the replacement and life limitation of Flight Control Remote Modules (FCRM) with specific part numbers CA71323-013, CA71323-014, CA71323-015, and CA71323-016. The directive mandates compliance with Airbus Service Bulletin A350-27-P066 to ensure continued airworthiness.
EASA AD 2024-0248
EASA Airworthiness Directive 2024-0248 is an airworthiness directive issued by EASA concerning the Airbus A350-941 and A350-1041 aeroplanes. It addresses the nose landing gear lower torque link, specifically part number 5035-0401 with certain serial numbers, requiring replacement or life limitation actions to ensure continued airworthiness.
EASA AD 2024-0234
EASA Airworthiness Directive 2024-0234 is an airworthiness directive issued by EASA concerning Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection of the pylons rib 9, specifically the two pylon bolts on both left-hand and right-hand sides, due to detected excessively deep spot faces that could compromise structural integrity.
EASA AD 2023-0189R1
EASA Airworthiness Directive 2023-0189R1 is a revision addressing the Airbus A350-941 and A350-1041 aeroplanes equipped with Trent XWB engines. It focuses on the replacement and inspection of the Engine Bleed Air System (EBAS) T-Duct, part number RR03-11011-001, due to a manufacturing quality issue that could lead to cracking and potential engine failure. The directive mandates compliance with Airbus and Rolls-Royce service bulletins to ensure continued airworthiness.
EASA AD 2024-0220
The document titled 'Oxygen — Cabin Oxygen Containers — Inspection' is an AIRBUS S.A.S. directive specifically addressing the inspection requirements for cabin oxygen containers installed on the Airbus A350 aircraft. It outlines necessary procedures to ensure the safety and reliability of oxygen supply systems on this aircraft type. The directive aims to maintain compliance with airworthiness standards for the Airbus A350 fleet.
EASA AD 2024-0199
EASA Airworthiness Directive 2024-0199 is an update addressing corrosion and cracks found in broadband antenna adapter plates and related parts on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates inspections and corrective actions to ensure the continued airworthiness of these aircraft. It applies to all serial numbers of the affected Airbus models and includes new provisions for the recently certified A321-253NY variant.
EASA AD 2024-0190
[Correction] Aircraft Flight Manual — Normal Procedures — Amendment is a regulatory document addressing updates to the flight manual procedures for Airbus S.A.S. aircraft models A350 and A380. This amendment corrects previously issued information to ensure accurate and safe operational guidance for these specific aircraft types. The document focuses on normal procedures relevant to flight crews operating the Airbus A350 and A380.
EASA AD 2024-0182R1
EASA Airworthiness Directive 2024-0182R1 is a regulatory update addressing inspection and maintenance requirements for Rolls-Royce Trent XWB series engines, specifically models Trent XWB-75, -79, -79B, -84, and -97, installed on Airbus A350 aircraft. The directive focuses on inspecting and replacing certain main fuel hose assemblies identified by specific part numbers to prevent potential engine fires. It mandates repetitive inspections and corrective actions to ensure continued airworthiness of affected engines.
EASA AD 2024-0189
EASA Airworthiness Directive 2024-0189 is an amendment addressing the Safe Life Airworthiness Limitations Items for Airbus A350-941 and A350-1041 aeroplanes. It updates the Airbus A350 Airworthiness Limitations Section Part 1 to Revision 08, Issue 2, ensuring mandatory compliance with new and more restrictive maintenance limits. This directive applies to all manufacturer serial numbers of the affected Airbus A350 models.
EASA AD 2024-0188
EASA Airworthiness Directive 2024-0188 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses potential mechanical noise and structural issues related to the nose landing gear shock absorber, specifically parts with Part Numbers 6406Axxxx and 4816Axxxx. The directive mandates repetitive functional steering checks to detect and correct increased friction and possible corrosion that could lead to nose landing gear failure.
EASA AD 2024-0186
EASA Airworthiness Directive 2024-0186 is an airworthiness directive addressing oxygen crew cylinder assemblies on Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection and replacement of specific oxygen cylinder assemblies with part numbers 4441227-058-000 and 4441227-058-001 due to a design defect causing loss of retention of the regulator inlet filter retainer. The directive applies to all manufacturer serial numbers of these aircraft models.
EASA AD 2024-0180
EASA Airworthiness Directive 2024-0180 is an amendment addressing the Airworthiness Limitations Section Part 5 related to fuel airworthiness limitations for Airbus A350-941 and A350-1041 aeroplanes. This directive mandates compliance with new and more restrictive maintenance tasks and life limits as specified in Airbus A350 ALS Part 5 Variation 7.1. It applies to all manufacturer serial numbers of the affected Airbus A350 models.