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EASA Regulations for Airbus A300

42 airworthiness directives and regulations affecting Airbus A300.

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New ADs and bulletins for Airbus A300, summarized like the ones below, every Monday.

EASA AD 2026-0007

Landing Gear — Component Life Limit — Implementation

EASA Airworthiness Directive 2026-0007 is an airworthiness directive affecting Airbus A300 B4-203, A300 B4-2C, A300 C4-203, and A300 F4-203 aeroplanes. It mandates the implementation of updated and more restrictive life limits for landing gear components to ensure continued airworthiness. The directive requires operators to comply with Airbus Service Bulletin A300-32-0471 and revise their Aircraft Maintenance Programme accordingly.

Airworthiness Directive

Airbus A300

EASA AD 2019-0011R2

Fuselage — Aft Fitting of Frame 40 — Inspection

Fuselage — Aft Fitting of Frame 40 — Inspection is a regulatory document concerning the inspection requirements for the aft fitting of Frame 40 on Airbus A300 and A300-600 aircraft. It addresses structural integrity checks specific to this fuselage component to ensure continued airworthiness of these aircraft models.

Airworthiness Directive

Airbus A300600

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.

Airworthiness Directive

Airbus A300600600ST (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.

Airworthiness Directive

Airbus A300600

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.

Airworthiness Directive

Airbus A310
Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A340
Airbus A300600600ST (Beluga)

EASA AD 2024-0169

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

EASA Airworthiness Directive 2024-0169 is an amendment addressing the Airbus A300 series, including models B4-2C, B4-103, B4-120, B4-203, B4-220, C4-203, and F4-203. This directive updates the Airworthiness Limitations Section Part 2 related to Damage Tolerant Airworthiness Limitations Items. It mandates new and more restrictive maintenance tasks to ensure continued airworthiness of these aircraft.

Airworthiness Directive

Airbus A300
Airbus A300 B4-2C
Airbus A300 B4-103
Airbus A300 B4-120
Airbus A300 B4-203
Airbus A300 B4-220
Airbus A300 C4-203
Airbus A300 F4-203

EASA AD 2017-0204R1

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

EASA Airworthiness Directive 2017-0204R1 is an amendment concerning Airbus A300 aeroplanes, all certified models and serial numbers. It addresses time limits and maintenance checks related to Safe Life Airworthiness Limitation Items as specified in the Airbus A300 Airworthiness Limitations Section Part 1 Revision 02. The directive ensures mandatory compliance with updated airworthiness limitations to maintain continued airworthiness and safety of the affected aircraft.

Airworthiness Directive

Airbus A300

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.

Airworthiness Directive

Airbus A300600600ST (Beluga)
Airbus A300B4-203
Airbus A300B4-2C
Airbus A300C4-203
Airbus A300F4-203
Airbus A300B4-603
Airbus A300B4-605R
Airbus A300B4-622
Airbus A300B4-622R
Airbus A300C4-620
Airbus A300F4-605R
Airbus 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.

Airworthiness Directive

Airbus A300600600ST (Beluga)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.

Airworthiness Directive

Airbus A300600
Airbus 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.

Airworthiness Directive

Airbus A300600600ST (Beluga)
Airbus A310
Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A340
Airbus A350
Airbus A380

EASA AD 2024-0008

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

EASA Airworthiness Directive 2024-0008 is an amendment concerning the Airbus A300 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 Airbus A300 models and serial numbers.

Airworthiness Directive

Airbus A300

EASA AD 2023-0209

Oxygen – Chemical Oxygen Generators – Replacement

EASA Airworthiness Directive 2023-0209 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing chemical oxygen generators installed on various Airbus aircraft models including A310, A300, A318, A319, A320, A321, A330, and A340 series. The directive targets specific part numbers of chemical oxygen generators that have shown failures to activate, potentially reducing oxygen availability in emergencies. It mandates replacement of affected oxygen generators to ensure continued airworthiness and safety.

Airworthiness DirectiveSuperseded

Airbus A310
Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A340
Airbus A300600600ST (Beluga)

EASA AD 2023-0196

Electrical Power — Nickel-Cadmium Rechargeable Batteries — Replacement

EASA Airworthiness Directive 2023-0196 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing the replacement of Nickel-Cadmium rechargeable batteries on various Airbus aircraft models including the A318, A319, A320, A321, A300, A310, A330, A340, A350, and A380. The directive mandates the replacement of affected Ni-Cd batteries with serviceable parts to ensure continued airworthiness and electrical power reliability. It applies to specific battery part numbers and sets time limits for on-wing battery storage to prevent capacity degradation.

Airworthiness Directive

Airbus A300600600ST (Beluga)
Airbus A310
Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A340
Airbus A350
Airbus A380

EASA AD 2021-0180-CN

CANCELLED: Oxygen — Crew and Passenger Oxygen Cylinders — Inspection / Replacement

EASA Airworthiness Directive 2021-0180-CN is a cancellation notice that officially cancels the previous directive EASA AD 2021-0180R2 concerning inspection and replacement of crew and passenger oxygen cylinders on various Airbus aircraft models. The affected aircraft include Airbus A300, A300-600, A310, A300F4-608ST, A318, A319, A320, A321, A330 (except A330-223F and A330-243F), and A340 series. The directive addressed oxygen cylinders with specific part numbers that had a manufacturing defect potentially causing oxygen leakage and fire risk.

Airworthiness Directive

Airbus A300600600ST (Beluga)
Airbus A310
Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A340
Airbus A300F4-608ST

EASA AD 2007-0243R1

Wings - Wing / Pylon Thrust- & Sideload Fitting (Spigot) - Inspection / Replacement

EASA Airworthiness Directive 2007-0243R1 is a regulatory document addressing inspection and replacement requirements for the wing and pylon thrust- and sideload fitting (spigot) on Airbus A300, A310, A300-600, and A300-600ST aeroplanes. The directive mandates detailed visual inspections and corrective actions to prevent structural integrity issues that could lead to engine loss. It applies to specific manufacturer serial numbers within these aircraft families.

Airworthiness Directive

Airbus A300600600ST (Beluga)600ST
Airbus A310

EASA AD 2023-0104

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

EASA Airworthiness Directive 2023-0104 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all certified models and serial numbers of Airbus A300 aeroplanes. It mandates compliance with updated airworthiness limitation tasks and maintenance program publication triggers as specified in Airbus A300 Airworthiness Limitations Section Part 2 Damage Tolerant Airworthiness Limitation Items Revision 03, Variation 3.4. This directive ensures continued structural integrity and safety of the affected aircraft.

Airworthiness DirectiveSuperseded

Airbus A300

EASA AD 2022-0171

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1 / Safe Life Airworthiness Limitations Items — Amendment

The document titled 'Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1 / Safe Life Airworthiness Limitations Items — Amendment' is an amendment concerning the Airbus A300 aircraft. It addresses updates to the airworthiness limitations related to time limits and maintenance checks, specifically focusing on safe life airworthiness limitation items. This amendment ensures continued compliance with safety standards for the Airbus A300 fleet.

Airbus A300

EASA AD 2022-0116

Hydraulic Power — Hydraulic System Reservoirs Pressurization — Functional Check

EASA Airworthiness Directive 2022-0116 is an airworthiness directive addressing hydraulic system reservoir pressurization on Airbus A300B2-203, A300B2K-3C, A300B4-203, A300B4-2C, A300C4-203, and A300F4-203 aeroplanes. It mandates functional checks of the hydraulic system reservoirs to detect air leakage and ensure proper pressurization. The directive aims to prevent potential loss of hydraulic systems due to contamination and air pressurization line rupture.

Airworthiness Directive

Airbus A300
Airbus A300B2-203
Airbus A300B2K-3C
Airbus A300B4-203
Airbus A300B4-2C
Airbus A300C4-203
Airbus A300F4-203

EASA AD 2022-0058

Windows — Windshields — Inspection

EASA Airworthiness Directive 2022-0058 is an airworthiness directive addressing inspection requirements for SAINT-GOBAIN SULLY front windshields installed on Airbus A300, A300-600, A310, and A300-600ST aeroplanes. It mandates repetitive detailed inspections and electrical test measurements of affected windshield parts to ensure structural integrity and prevent in-flight windshield failure. The directive applies to all certified models and manufacturer serial numbers of these Airbus aircraft.

Airworthiness Directive

Airbus A300600600ST (Beluga)600ST
Airbus A310