Doors – Aft Cargo Door Frame Forks – Inspection
Superseded. Comply with 2023-0117, which replaces this document.
- Published
- Effective
- Deadline
- Replaces
- 2015-0152R1
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must perform detailed clearance checks, inspections for wear, and high frequency eddy current inspections on the aft cargo door frame forks within specified compliance times based on flight cycles. Any discrepancies or cracks found must be corrected before further flight by adjustment, repair, replacement, or reinforcement as per Airbus service bulletins. Inspections must be repeated at intervals defined by the AD, with no terminating action provided by corrective measures alone.
Summary
EASA Airworthiness Directive 2018-0266 is an airworthiness directive issued for Airbus A300F4-605R and A300F4-622R aeroplanes equipped with Airbus modification 12046. It addresses the inspection and maintenance of aft cargo door frame forks to detect cracks and prevent structural integrity issues. The directive mandates specific inspections and corrective actions to ensure continued airworthiness of affected aircraft.
What changed
EASA Airworthiness Directive 2018-0266 supersedes the previous AD 2015-0152R1 and introduces new inspection thresholds and intervals based on the frame fork configuration. It updates the inspection procedures and intervals for high frequency eddy current inspections and clarifies corrective actions for detected wear or cracks. The directive also incorporates revised Airbus service bulletins for inspection and modification.
Why it matters
This directive is critical for aviation professionals as it ensures the structural integrity of the aft cargo door on affected Airbus A300 models, preventing potential in-flight failures. Operators and maintenance organizations must comply to avoid unsafe conditions that could lead to cargo door frame rupture. Compliance helps maintain aircraft safety and regulatory conformity, reducing risk and potential operational disruptions.
More for Airbus A300-600
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- EASA PAD 26-013Fuselage — Door Frames Holes — InspectionJan 26, 2026
- EASA AD 2018-0229R1Wings — Centre Wing Box Frame 47 Angle Fittings — Inspection / ModificationNov 20, 2025
- EASA AD 2025-0255Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitations Items — AmendmentNov 19, 2025
- EASA AD 2025-0236
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New ADs and bulletins for Airbus A300-600, A300F4-605R and A300F4-622R, summarized like this page, every Monday.