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EASA Regulations for Airbus A300-600

59 airworthiness directives and regulations affecting Airbus A300-600.

EASA AD 26-013

Fuselage — Door Frames Holes — Inspection

EASA Airworthiness Directive 26-013 is a proposed directive addressing inspection requirements for door frame holes on Airbus A300-600 and A310 aeroplanes. It mandates repetitive high frequency eddy current inspections of specific seal retainer run out rivet holes at frames 56A, 57A, and 73A on both left-hand and right-hand sides. The directive applies to all manufacturer serial numbers of the affected aircraft models.

Jan 26, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A310

EASA AD 2018-0229R1

Wings — Centre Wing Box Frame 47 Angle Fittings — Inspection / Modification

EASA Airworthiness Directive 2018-0229R1 is a regulatory update addressing inspection and modification requirements for the centre wing box frame 47 angle fittings on Airbus A300-600 series aeroplanes. This directive applies to various A300-600 models except those already modified by Airbus Service Bulletin A300-57-6069. It mandates specific inspections and modifications to detect and correct cracks that could compromise the structural integrity of the aircraft's centre wing box.

Nov 20, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2025-0255

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitations Items — Amendment

EASA Airworthiness Directive 2025-0255 is an amendment addressing the Airbus A300-600 aeroplanes. It mandates compliance with the updated Airworthiness Limitations Section Part 2, specifically the Damage Tolerant Airworthiness Limitations Items as defined in Airbus A300-600 ALS Part 2 Revision 4 Variation 4.3. This directive ensures continued airworthiness by enforcing new and more restrictive maintenance tasks for these aircraft.

Nov 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2025-0236

Fuselage — Frame Base Fitting between Frames 41 and 46 — Inspection / Repair

EASA Airworthiness Directive 2025-0236 is an airworthiness directive affecting Airbus A300-600 series aeroplanes, specifically models A300 B4-603, B4-605R, B4-622, B4-622R, C4-605R variant F, F4 605R, and F4-622R. It addresses inspection and repair requirements for the fuselage frame base fitting located between frames 41 and 46. The directive mandates repetitive detailed inspections and corrective actions to ensure structural integrity of the frame foot areas.

Oct 23, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2019-0044R1

Wings — Centre Section Frame 40 Forward Fitting Radius at Tension Bolt Junction — Inspection / Repair

The document titled 'Wings — Centre Section Frame 40 Forward Fitting Radius at Tension Bolt Junction — Inspection / Repair' is an Airworthiness Directive issued by AIRBUS S.A.S. specifically for the Airbus A300-600 aircraft. It addresses inspection and repair requirements for the forward fitting radius at the tension bolt junction on the centre section frame 40 of the wing. The directive aims to ensure structural integrity and safety of the affected aircraft component.

Oct 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2025-0214

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Part 2 / Damage Tolerant Airworthiness Limitation Items — Amendment

The document titled 'Time Limits / Maintenance Checks — Airworthiness Limitations Section — Part 2 / Damage Tolerant Airworthiness Limitation Items — Amendment' is an amendment concerning the Airbus A300-600 aircraft. It addresses updates to the airworthiness limitations related to damage tolerant airworthiness limitation items, which are critical for maintaining the structural integrity of the aircraft over time.

Sep 30, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2017-0158R2

Wings — Fuselage Frame 40 Lower Outboard Radius — Inspection

EASA Airworthiness Directive 2017-0158R2 is an updated regulatory requirement for Airbus A300-600 series aeroplanes equipped with modification 10221. It mandates special detailed inspections of the fuselage frame 40 lower outboard radius and fastener areas to detect cracks that could compromise structural integrity. The directive applies to specific Airbus A300 B4-605R, B4-622R, C4-605R Variant F, F4-605R, and F4-622R models.

Sep 12, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2025-0170

Main Landing Gear — Replacement

The document titled 'Main Landing Gear — Replacement' is a regulatory communication concerning the Airbus A300, A300-600, and A300-600ST (Beluga) aircraft models. It addresses the replacement procedures or requirements related to the main landing gear components of these specific Airbus aircraft types. The document serves as a guideline or directive for maintenance and operational compliance.

Aug 4, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)

EASA AD 2014-0272R1

Wings — Frame 40 Lower Junction Fastener Holes — Inspection / Repair

EASA Airworthiness Directive 2014-0272R1 is an updated regulation addressing inspection and repair requirements for the frame 40 lower junction fastener holes on Airbus A300 and A300-600 aeroplanes. It mandates specific inspections to detect cracks in the fittings around these fastener holes to ensure structural integrity. The directive applies to all models and serial numbers of these aircraft types.

Jul 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600

EASA AD 2024-0238

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

EASA Airworthiness Directive 2024-0238 is an amendment addressing the Airbus A300-600 and A300-600ST aeroplanes. It mandates compliance with updated system equipment maintenance requirements as specified in Airbus A300-600 Airworthiness Limitations Section Part 4, Revision 03 Variation 3.4. This directive applies to all manufacturer serial numbers of affected Airbus A300 models including B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, C4-605R variant F, C4-620, F4-605R, F4-622R, and F4-608ST.

Dec 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A300-600ST (Beluga)

EASA AD 2024-0198

Oxygen — Chemical Oxygen Generators — Replacement

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.

Oct 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A300-600ST (Beluga)Airbus A310Airbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Airbus A300

EASA AD 2024-0170

Wing — Stringer Joint at Rib 18 — Inspection / Modification

EASA Airworthiness Directive 2024-0170 is an airworthiness directive addressing inspection and modification of the wing stringer joint at Rib 18 on Airbus A300-600 series aeroplanes, including models A300B4-603, A300B4-605R, A300B4-622, A300B4-622R, A300C4-605R variant F, A300C4-620, A300F4-605R, and A300F4-622R. It mandates detailed visual inspections and modifications to prevent widespread fatigue damage in the wing structure. The directive applies to all manufacturer serial numbers of these aircraft types.

Aug 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A300B4-603Airbus A300B4-605RAirbus A300B4-622Airbus A300B4-622RAirbus A300C4-605R variant FAirbus A300C4-620Airbus A300F4-605RAirbus A300F4-622R

EASA AD 2024-0164

Time Limits / Maintenance Checks — Safe Life Airworthiness Limitation Items — ALS Part 1 — Amendment

EASA Airworthiness Directive 2024-0164 is an amendment addressing the Airbus A300-600 and A300-600ST aeroplanes. It updates the Safe Life Airworthiness Limitation Items in the Airbus A300-600 Airworthiness Limitations Section Part 1, Revision 03. This directive mandates compliance with new and more restrictive maintenance limitations to ensure continued airworthiness.

Aug 21, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A300-600ST (Beluga)Airbus A300-600ST

EASA AD 2024-0162

Wings — Main Landing Gear Support Rib 5 — Inspection

EASA Airworthiness Directive 2024-0162 is an airworthiness directive addressing inspection requirements for the main landing gear support Rib 5 on Airbus A300 series aeroplanes, including models A300B4-203, A300B4-2C, A300C4-203, A300F4-203, A300B4-603, A300B4-605R, A300B4-622, A300B4-622R, A300C4-620, A300F4-605R, and A300F4-608ST. The directive mandates a one-time special detailed inspection of critical spotfaces on the main landing gear support Rib 5 lower flange to detect potential cracking issues. This AD applies to aircraft with specific modifications embodied in service or production and excludes certain part numbers and post-modification configurations.

Aug 20, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)Airbus A300B4-203Airbus A300B4-2CAirbus A300C4-203Airbus A300F4-203Airbus A300B4-603Airbus A300B4-605RAirbus A300B4-622Airbus A300B4-622RAirbus A300C4-620Airbus A300F4-605RAirbus A300F4-608ST

EASA AD 2024-0145

Wings — Main Landing Gear Support Rib 5 — Inspection

EASA Airworthiness Directive 2024-0145 is an airworthiness directive affecting Airbus A300, A300-600, and A300-600ST aeroplanes with specific manufacturer serial numbers. It mandates inspections of the main landing gear support Rib 5 lower flange for cracks, focusing on parts except those with certain part numbers. This directive updates previous requirements to include additional aircraft groups and inspection procedures.

Jul 23, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)Airbus A300-600ST

EASA AD 2024-0092R1

Doors — Main Deck Cargo Door Actuator Bearing Fittings — Inspection

EASA Airworthiness Directive 2024-0092R1 is an updated regulatory document addressing inspection requirements for the main deck cargo door actuator bearing fittings on Airbus A300, A300-600, and A310 freighter aircraft. The directive mandates inspections to detect cracks caused by fatigue in these actuator fittings to prevent potential unsafe conditions during cargo door operations. It applies to all affected aircraft serial numbers, including those modified by specific EASA Supplemental Type Certificates.

Jul 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A310

EASA AD US-2024-11-01

Electrical Power - Nickel-Cadmium Batteries during Aeroplane Parking or Storage - Replacement

The Electrical Power - Nickel-Cadmium Batteries during Aeroplane Parking or Storage - Replacement is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2024-11-01) that applies to various Airbus SAS airplane models including A300, A310, A318, A319, A320, A321, A330, A340, A350, and A380 series equipped with certain parts manufacturer approval (PMA) nickel-cadmium (Ni-Cd) batteries. This AD addresses the issue of reduced battery endurance performance during airplane parking or storage periods. It mandates replacement of affected PMA Ni-Cd batteries with serviceable parts to ensure electrical power reliability during abnormal or emergency conditions.

Jun 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)Airbus A310Airbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Airbus A350Airbus A380

EASA AD 2024-0083

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Part 2 / Damage Tolerant Airworthiness Limitation Items — Amendment

EASA Airworthiness Directive 2024-0083 is an amendment addressing the Airbus A300-600 aeroplanes equipped with Airbus modification 12046. It mandates compliance with new and more restrictive maintenance tasks introduced in the Airbus A300-600 Airworthiness Limitations Section Part 2 Revision 4 Variation 4.1. This directive ensures continued airworthiness by updating time limits and maintenance checks related to damage tolerant airworthiness limitation items.

Apr 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2024-0009

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitations Items — Amendment

EASA Airworthiness Directive 2024-0009 is an amendment concerning the Airbus A300-600 aeroplanes. It updates the Airworthiness Limitations Section Part 2 related to Damage Tolerant Airworthiness Limitations Items, ensuring continued airworthiness through revised maintenance tasks and limitations. This directive applies to all certified models and manufacturer serial numbers of the Airbus A300-600.

Jan 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600