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EASA Regulations & Airworthiness Directives

Browse 284 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 787114 Show all...

Filtered by: Airbus A321Clear filter

EASA AD 2025-0189

Fuselage — Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings — Inspection

Fuselage — Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings — Inspection is an airworthiness directive applicable to Airbus S.A.S. aircraft models A318, A319, A320, and A321. This document mandates inspections of the centre fuselage area focusing on the main landing gear door keel beam hinge and actuator fittings to ensure structural integrity and operational safety.

Airworthiness Directive

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD 2025-0167R1

Landing Gear — Main Landing Gear Aft Pintle Pin — Replacement

EASA Airworthiness Directive 2025-0167R1 is an updated safety directive addressing the replacement of the Main Landing Gear (MLG) Aft Pintle Pin on Airbus A318, A319, A320, and A321 aircraft. The directive applies to specific part numbers D3215600500600 and D3215303000800 identified as affected due to manufacturing defects. It mandates replacement of these parts to prevent potential corrosion and cracking that could lead to landing gear collapse.

Airworthiness Directive

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD 2025-0185

Wings — Pylon Spigot Fitting — Inspections

EASA Airworthiness Directive 2025-0185 is an airworthiness directive addressing inspections of the pylon spigot fitting on Airbus A318, A319, A320, and A321 aeroplanes. It targets slotted nuts with Part Number D57250182200 installed on these aircraft to detect severe corrosion that could compromise wing and pylon structural integrity. The directive mandates repetitive visual inspections and corrective actions as necessary to maintain safety.

Airworthiness Directive

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD 2025-0166

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

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 AD 2025-0075R1

Flight Controls / Landing Gear / Oxygen / Pneumatic - Part(s) Installation

Flight Controls / Landing Gear / Oxygen / Pneumatic - Part(s) Installation is a regulatory document concerning the installation of parts related to flight controls, landing gear, oxygen systems, and pneumatic systems on the Airbus A321 aircraft. The document addresses specific installation requirements to ensure airworthiness and safety compliance for this aircraft type.

Airworthiness Directive

Airbus A321

EASA PAD 25-104

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.

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD 2025-0118R1

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.

Airbus A319
Airbus A320
Airbus A321

EASA AD 2021-0177R3

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

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

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

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 2025-0107

Fuselage — Frame 35 / Slidebox Junction — Inspection

EASA Airworthiness Directive 2025-0107 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 aeroplanes. The directive mandates inspections of the fuselage frame 35 and slidebox junction areas to detect cracks that could compromise structural integrity. It applies to all serial numbers except those with Airbus modifications 161341 or 161511 incorporated during production.

Airworthiness Directive

Airbus A321

EASA AD 2025-0096

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.

Airbus A319
Airbus A320
Airbus A321

EASA AD 2025-0083

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

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 2025-0067

Fuselage — Centre Fuselage Frame Foot Joint — Inspection

EASA Airworthiness Directive 2025-0067 is an airworthiness directive addressing the Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes up to manufacturer serial number 09287 with Airbus modification 160286. It mandates inspections of the centre fuselage frame foot joint fastener holes to detect potential cracks that could affect structural integrity. The directive provides inspection intervals and corrective actions to maintain airworthiness.

Airworthiness Directive

Airbus A321

EASA AD 2025-0066

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

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 2025-0041

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