Fuselage — Aft Fitting of Frame 40 — Inspection
- Published
- Effective
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Affected operators and maintenance teams should perform the specified inspections on the aft fitting of Frame 40 according to the procedures outlined in the document. They must adhere to any inspection intervals or deadlines provided to maintain airworthiness.
Summary
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.
What changed
This document introduces inspection procedures for the aft fitting of Frame 40 on Airbus A300 and A300-600 aircraft. It establishes new inspection criteria or intervals to detect potential structural issues in this critical fuselage area.
Why it matters
This inspection requirement is important for aviation professionals as it helps maintain the structural safety of Airbus A300 series aircraft. Operators and maintenance organizations must comply to prevent possible structural failures, ensuring safe operation and regulatory compliance.
More for Airbus A300
All 42- EASA AD 2026-0007Landing Gear — Component Life Limit — ImplementationJan 14, 2026
- 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
- EASA AD 2024-0169Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitations Items — Amendment
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