Doors — Main Deck Cargo Door Actuator Bearing Fittings — Inspection
- Published
- Effective
- Deadline
- Replaces
- 2024-0092
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must not exceed a 70-degree opening angle for the main deck cargo door on affected parts that have surpassed 13,000 flight cycles, except during the automatic closing sequence. Detailed visual inspections of the actuator bearing fittings must be performed before 13,000 flight cycles or within 330 flight cycles after 26 April 2024, and then every 640 flight cycles thereafter. If any cracks are found, both affected parts must be replaced with new serviceable parts before the next flight.
Summary
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.
What changed
This revision of EASA AD 2024-0092 clarifies that during the automatic closing sequence of the main deck cargo door, the door opening angle may temporarily exceed the 70-degree operational limitation without constituting a violation. The AD remains an interim measure requiring repetitive inspections and operational limitations, with further regulatory actions possible in the future.
Why it matters
This directive is critical for aviation professionals as it addresses a fatigue-related cracking issue that could lead to uncontrolled cargo door movement, posing safety risks to ground personnel. Operators and maintenance organizations must comply with inspection intervals and operational limits to ensure continued airworthiness and prevent potential injuries or damage during cargo loading and unloading.
More for Airbus A300
All 42- EASA AD 2026-0007Landing Gear — Component Life Limit — ImplementationJan 14, 2026
- EASA AD 2019-0011R2Fuselage — Aft Fitting of Frame 40 — InspectionAug 8, 2025
- EASA AD 2025-0170Main Landing Gear — ReplacementAug 4, 2025
- EASA AD 2014-0272R1Wings — Frame 40 Lower Junction Fastener Holes — Inspection / RepairJul 31, 2025
- EASA AD 2024-0198Oxygen — Chemical Oxygen Generators — ReplacementOct 18, 2024
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