Fuselage — Frame / Stringer Attachments — Inspection / Repair
- Published
- Effective
- Deadline
- Replaces
- 2014-0197
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of affected Airbus A330-223F and A330-243F aircraft must perform a one-time detailed inspection of specified fuselage zones before the aircraft reaches 72 months since its first flight. If discrepancies are found, adjacent areas must be inspected and corrective modifications or repairs applied before further flight, following the instructions in the referenced Airbus Service Bulletins. Contact Airbus for approved repair instructions if necessary.
Summary
EASA Airworthiness Directive 2014-0197R1 is an updated regulatory requirement addressing inspection and repair of fuselage frame and stringer attachments on Airbus A330-223F and A330-243F aircraft with specific manufacturer serial numbers. The directive mandates detailed inspections and corrective actions to ensure structural integrity due to missing fasteners found on some A330-200F aircraft during production. It references specific Airbus Service Bulletins for inspection and modification procedures.
What changed
This revision of EASA AD 2014-0197 corrects errors found in Appendix 1 (Table 3) of the original directive and updates editorial content to align with the latest AD writing standards. The changes do not affect the substantive requirements but clarify inspection zones and procedures. It replaces the original AD issued in September 2014.
Why it matters
This directive is critical for maintaining the structural safety of affected Airbus A330 freighter aircraft by preventing potential crack initiation and propagation caused by missing fasteners. Operators and maintenance organizations must comply to avoid reduced fuselage integrity, which could lead to serious safety risks. Compliance ensures continued airworthiness and regulatory conformity under EU aviation safety regulations.
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