EASA Regulations & Airworthiness Directives

Browse 285 EASA regulations with AI-powered summaries.

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Filtered by: Airbus A320Clear filter

EASA AD 2025-0166

Jul 30, 2025

Fuselage — Inner Cap and Frame Flange at Frame 68 Stringer 22 — Inspections

The document titled 'Fuselage — Inner Cap and Frame Flange at Frame 68 Stringer 22 — Inspections' is a regulatory directive applicable to Airbus S.A.S. aircraft models A318, A319, A320, and A321. It addresses inspection requirements focused on the fuselage structure, specifically the inner cap and frame flange at frame 68 stringer 22. The directive aims to ensure structural integrity and continued airworthiness of these aircraft types.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0210R1

Jul 22, 2025

Superseded by EASA AD 2025-0166

EASA Airworthiness Directive 2025-0166 supersedes the previous directive affecting Airbus S.A.S. aircraft models A318, A319, A320, and A321. This directive addresses updated safety and maintenance requirements for these aircraft types to ensure continued airworthiness. It provides revised instructions and compliance measures relevant to operators and maintenance organizations.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA PAD 25-104

Jul 16, 2025

Fuselage — Centre Fuselage Forward Pressure Bulkhead — Inspection

EASA Airworthiness Directive Proposal 25-104 is a regulatory document addressing inspection requirements for the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various serial numbers except those with specific Airbus modifications embodied in production or service. The directive mandates repetitive rototest inspections of the forward pressure bulkhead hole C1 and provides an optional terminating modification.

Proposed AD
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0118R1

Jul 15, 2025

Aircraft Flight Manual — Amendment / Communications — Digital Radio and Audio Integrating Management System — Modification

The document titled 'Aircraft Flight Manual — Amendment / Communications — Digital Radio and Audio Integrating Management System — Modification' applies to AIRBUS S.A.S. aircraft models A319, A320, and A321. It addresses updates to the Aircraft Flight Manual related to the integration and modification of the digital radio and audio management systems on these aircraft types. The amendment ensures that the flight manual reflects the latest system capabilities and operational procedures.

Other
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2021-0177R3

Jul 15, 2025

Hydraulic Power — Pylon / Engine Interface Rods — Inspection / Replacement

EASA Airworthiness Directive 2021-0177R3 is a regulatory update addressing inspection and replacement requirements for hydraulic power pylon/engine interface rods installed on Airbus A319, A320, and A321 aircraft models. The directive applies to specific part numbers of interface rods and mandates repetitive detailed inspections and corrective actions to prevent potential fuel or hydraulic leaks caused by rod end damage. It also introduces optional terminating actions through modification to enhance safety and compliance.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2017-0098R2

Jun 25, 2025

Fuselage — Potable Water and Waste Water Service Panels — Reinforcement

EASA Airworthiness Directive 2017-0098R2 addresses reinforcement requirements for the potable water and wastewater service panels on Airbus A319, A320, and A321 aeroplanes. This directive applies to various models except those already modified with Airbus production modifications 160055 or 160056, or certain corporate jet variants. It mandates structural reinforcements to prevent fatigue cracks that could compromise aircraft integrity.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0120

May 26, 2025

Cabin Systems — Antenna Adapter Plate — Inspection

EASA Airworthiness Directive 2025-0120 is an airworthiness directive addressing inspection requirements for the antenna adapter plate and related parts installed on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates repetitive general visual inspections of affected broadband antenna adapter plates to detect corrosion and cracks that could compromise aircraft safety. It applies to all manufacturer serial numbers of the specified Airbus models.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A350
  • Airbus A380

EASA AD 2025-0111

May 14, 2025

Fuselage — Service Door Stop Fitting Hole — Inspection / Repair

EASA Airworthiness Directive 2025-0111 is issued for Airbus A318, A319, A320, and A321 aeroplanes, addressing inspection and repair requirements for the fuselage service door stop fitting holes at fuselage frames 16 and 20. This directive mandates repetitive rototest inspections and corrective actions to detect and repair cracks that could compromise structural integrity. It applies to both Current Engine Option (CEO) and New Engine Option (NEO) variants with specific applicability exceptions.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0096

Apr 28, 2025

Aircraft Flight Manual — Section Limitations — Amendment / Master Minimum Equipment List — Amendment / Pneumatic — High Pressure Bleed Valve — Replacement

The document titled 'Aircraft Flight Manual — Section Limitations — Amendment / Master Minimum Equipment List — Amendment / Pneumatic — High Pressure Bleed Valve — Replacement' applies to Airbus S.A.S. aircraft models A319, A320, and A321. It addresses updates to the Aircraft Flight Manual section limitations and the Master Minimum Equipment List, alongside the replacement procedure for the pneumatic high pressure bleed valve. These changes are specific to the Airbus A319/A320/A321 family.

Other
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0083

Apr 14, 2025

Equipment/Furnishings — Cargo Bulkhead Frame 24A Vertical Members — Inspection

EASA Airworthiness Directive 2025-0083 is an official regulatory document addressing inspection requirements for the cargo bulkhead frame 24A vertical members on Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive detailed inspections of the affected cargo bulkhead vertical member upper parts and fittings located behind the 80VU rack to ensure continued airworthiness. The directive applies to all manufacturer serial numbers of the specified Airbus models.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0078

Apr 9, 2025

Fuselage — Centre Fuselage Skin and Forward Pressure Bulkhead — Inspection

EASA Airworthiness Directive 2025-0078 is an airworthiness directive addressing inspection requirements for the centre fuselage skin and forward pressure bulkhead on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific serial numbers and configurations, focusing on potential fatigue issues in critical fuselage areas. The directive mandates repetitive inspections and corrective actions to ensure structural integrity.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0066

Mar 28, 2025

Fuselage — Pressure Panel at Centre Wing Box — Inspection

EASA Airworthiness Directive 2025-0066 is an airworthiness directive issued by EASA concerning Airbus A319, A320, and A321 aeroplanes with specific modifications embodied in production. It mandates inspections of the pressure panel at the centre wing box to detect potential fatigue-related cracks. The directive applies to various Airbus A319, A320, and A321 models up to manufacturer serial number 09287, excluding certain CEO aeroplanes with specific mods.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0068

Mar 28, 2025

Superseded by EASA AD 2026-0017

EASA Airworthiness Directive 2025-0068 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection and modification requirements for forward-facing galleys with specific part numbers to prevent damage-related failures that could compromise galley integrity during emergency landings. The directive mandates inspections and corrective actions to ensure galley safety and compliance.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0065

Mar 27, 2025

Fuselage — Angle Fitting Connection to Side Skin Panel and Transition Angle — Inspection

The document titled 'Fuselage — Angle Fitting Connection to Side Skin Panel and Transition Angle — Inspection' is an inspection directive applicable to the Airbus A320 aircraft. It addresses the structural integrity of the angle fitting connections between the side skin panel and the transition angle on the fuselage. The directive aims to ensure continued airworthiness by mandating specific inspection procedures.

Airworthiness Directive
  • Airbus A320

EASA AD 2025-0041

Feb 18, 2025

Flight Controls — Trimmable Horizontal Stabilizer Actuator — Modification

The Flight Controls — Trimmable Horizontal Stabilizer Actuator — Modification is an airworthiness directive issued by AIRBUS S.A.S. affecting multiple aircraft types including the A318, A319, A320, A321, A330, and A340. This document addresses modifications related to the trimmable horizontal stabilizer actuator system to ensure continued safe flight control operations. It applies specifically to the listed Airbus aircraft models equipped with the affected actuator components.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340

EASA AD 2025-0037

Feb 12, 2025

Superseded by EASA AD 2025-0118

EASA Airworthiness Directive 2025-0037 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes with specific Airbus modifications embodied. The directive addresses issues related to loss of synchronization between radio management panels, which can result in loss of radio communications, transponder functionality, and standby navigation. It requires amendments to the Aircraft Flight Manual to include procedures to manage these failures.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0031

Feb 10, 2025

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 3 — Certification Maintenance Requirements — Amendment

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.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0032

Feb 10, 2025

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

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.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0033

Feb 10, 2025

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 5 — Fuel Airworthiness Limitations — Amendment

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.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321