EASA AD 2007-0243R1
Wings - Wing / Pylon Thrust- & Sideload Fitting (Spigot) - Inspection / Replacement
Summary
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.
What Changed
This revision of EASA AD 2007-0243 adds the supersedure of DGAC France AD 1999-007-019 R1 and incorporates administrative and layout amendments to align with the latest EASA AD standards. The technical requirements remain unchanged, but the revision clarifies applicability and compliance instructions without altering inspection thresholds or intervals.
Why It Matters
This directive is critical for aviation professionals because it ensures the continued structural integrity of the wing-to-pylon attachment, preventing potential engine separation. Operators and maintenance organizations must comply to avoid unsafe conditions that could compromise flight safety. The AD also harmonizes compliance requirements across affected Airbus models, facilitating consistent maintenance practices.
What To Do
Operators of affected Airbus A300, A310, A300-600, and A300-600ST aeroplanes must perform detailed visual inspections of the wing/pylon spigot before exceeding specified flight cycle thresholds or within defined timeframes. If cracks are found, immediate replacement of the spigot is required before further flight. Inspections must be repeated at intervals not exceeding those specified in the directive, with adjustments for aircraft average flight time as applicable.
AI-generated summary from official EASA source document. Always verify against the original.