Browse 262 EASA regulations with AI-powered summaries.
EASA AD 2025-0030
EASA Airworthiness Directive 2026-0028 supersedes previous directives related to Airbus S.A.S. aircraft models A318, A319, A320, and A321. This directive addresses updated safety requirements and maintenance procedures for these aircraft types. It ensures continued airworthiness and compliance with the latest regulatory standards.
EASA AD 2025-0031
EASA Airworthiness Directive 2025-0031 is an amendment addressing the Time Limits and Maintenance Checks in the Airworthiness Limitations Section Part 3 for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with updated Certification Maintenance Requirements. The directive ensures continued airworthiness by requiring operators to follow the latest Airbus ALS Part 3 Revision 10 maintenance tasks and intervals.
EASA AD 2025-0032
EASA Airworthiness Directive 2025-0032 is an amendment addressing the Time Limits and Maintenance Checks in the Airworthiness Limitations Section Part 4 for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with updated system equipment maintenance requirements. This directive ensures continued airworthiness by enforcing specific maintenance tasks and life limits.
EASA AD 2025-0033
EASA Airworthiness Directive 2025-0033 is an amendment addressing time limits and maintenance checks in the Airworthiness Limitations Section Part 5 related to fuel airworthiness limitations for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with Airbus A318/A319/A320/A321 ALS Part 5 Revision 09. The directive ensures continued airworthiness by enforcing updated maintenance tasks and life limits for fuel system components.
EASA AD 2024-0247
EASA Airworthiness Directive 2024-0247 is issued for Airbus A318, A319, A320, A321, A330, and A340 aeroplanes. It addresses issues related to Trimmable Horizontal Stabilizer Actuators (THSA) that have erroneous accumulated life data in their release certificates. This directive applies to specific THSA parts identified by Collins Aerospace and Airbus documentation.
EASA AD 2024-0231
EASA Airworthiness Directive 2024-0231 is an airworthiness directive applicable to Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive detailed inspections of the cargo bulkhead frame 24A vertical members and female fittings located behind the 80VU rack to detect elongation and potential damage. The directive aims to prevent possible system failures caused by affected parts hitting the 80VU rack, which could lead to reduced control of the aircraft.
EASA AD 2024-0230
EASA Airworthiness Directive 2024-0230 is an airworthiness directive addressing inspection requirements for the bottom wing skin panel 2 on Airbus A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. It mandates detailed inspections of specific wing areas prone to fatigue cracking, particularly around the bottom wing skin manhole access panel number 2 between ribs 13 and 26. The directive applies to all manufacturer serial numbers of the affected aircraft models.
EASA AD 2024-0201R1
EASA Airworthiness Directive 2024-0201R1 is an updated regulatory requirement addressing inspections of the outer wing bottom buttstrap on Airbus A319, A320, and A321 aeroplanes. It mandates repetitive special detailed inspections of the wing surface area between rib 19 and rib 21 forward of stringer 8 on both left and right sides to detect cracks that could compromise structural integrity. This directive applies to all manufacturer serial numbers of the specified Airbus models.
EASA AD 2024-0217
EASA Airworthiness Directive 2024-0217 is an airworthiness directive addressing inspection requirements for the fuselage double joggle areas at frame 16 and frame 20 on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various models of these aircraft except those with specific Airbus modifications or service bulletins embodied. The directive mandates special detailed inspections and corrective actions to detect and address cracks that could compromise fuselage structural integrity.
EASA AD 2024-0216
EASA Airworthiness Directive 2024-0216 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses issues with certain main landing gear door actuators, specifically those with Part Number 114122015 and listed serial numbers, which may cause jamming or inability to open the landing gear doors during maintenance. The directive mandates inspections and corrective actions to ensure safe operation of the landing gear.
EASA AD 2024-0208
EASA Airworthiness Directive 2024-0208 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated damage tolerant airworthiness limitations as specified in Airbus A318/A319/A320/A321 Airworthiness Limitations Section Part 2 Revision 10 Variation 10.3. This directive ensures continued airworthiness by requiring operators to incorporate new or more restrictive maintenance tasks.
EASA AD 2024-0203
EASA Airworthiness Directive 2024-0203 is an airworthiness directive addressing the replacement of trimmable horizontal stabilizer actuators (THSA) on Airbus A318, A319, A320, and A321 aircraft models, including the newly certified A321-253NY. The directive mandates the replacement of affected THSA parts identified by serial numbers to ensure continued safe operation of the flight controls. It applies to all manufacturer serial numbers of the specified aircraft models.
EASA AD 2024-0204
EASA Airworthiness Directive 2024-0204 is issued for Airbus A319 and A320 aeroplanes, specifically models A319-112, A319-132, A320-214, A320-232, A320-233, A320-251N, and A320-271N. This directive mandates inspection of rivet holes at frame 64 of the fuselage to detect and correct potential fatigue damage. The directive applies to all manufacturer serial numbers listed in the AD's appendix.
EASA AD 2024-0198
EASA Airworthiness Directive 2024-0198 is an official regulatory document addressing the replacement of chemical oxygen generators in various Airbus aeroplanes, including models A310, A300, A318, A319, A320, A321, A330, and A340. The directive targets specific oxygen generators with part numbers E63320-00, E63340-00, and E63440-00 that have known activation failures. It mandates replacement of these affected parts to ensure continued airworthiness and safety.
EASA AD 2024-0197
EASA Airworthiness Directive 2024-0197 is issued for Airbus A318, A319, A320, A321, A330, and A340 aeroplanes concerning the SafeLav gaseous oxygen container (SLGOC). The directive addresses a production deficiency in certain SLGOC batches that may cause oxygen flow activation failure due to a missing heat treatment on the actuation pin. This AD applies to specific part numbers and serial numbers of SLGOCs installed on these aircraft models.
EASA AD 2024-0196
EASA Airworthiness Directive 2024-0196 is an airworthiness directive addressing the inspection of pneumatic overheat detection system sensing elements on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific part numbers of continuous fire detectors produced before January 31, 2021, which may fail to detect thermal bleed leak events properly. The directive mandates inspection and, if necessary, replacement of affected parts to ensure continued airworthiness.
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 2020-0104R1-CN
EASA Airworthiness Directive Cancellation Notice 2020-0104R1-CN cancels the previous AD 2020-0104R1 concerning the inspection and replacement of oxygen supply solenoid valves on Airbus A318, A319, A320, and A321 aircraft. The affected parts are specific solenoid valves with part numbers DVE90-06 or DVE90-07 manufactured up to 2016. This cancellation applies to all manufacturer serial numbers of these aircraft models.
EASA AD 2024-0147R1
EASA Airworthiness Directive 2024-0147R1 is an updated regulatory requirement addressing inspection and reinforcement of the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aircraft. It mandates repetitive inspections for fatigue damage at frame 35 (or 35.8 for A321) and requires modification to reinforce the bulkhead to ensure structural integrity. This directive applies to all serial numbers except those with specific Airbus modifications embodied in production or service.
EASA AD 2019-0069R2
EASA Airworthiness Directive 2019-0069R2 is a regulatory document addressing the modification of overhead stowage compartments (OHSC) and pivoting OHSC (POHSC) on Airbus A318, A319, A320, and A321 aircraft. The directive mandates modifications to improve the robustness of these compartments to prevent detachment caused by loose or missing screws. This AD applies specifically to various Airbus A320 family models as listed in the applicable service bulletins.