Fuselage — Cockpit Lateral Window Frames — Inspection
- Published
- Effective
- Deadline
- Replaces
- 2019-0173
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must perform special detailed inspections of the affected vertical stiffeners within specified thresholds and intervals according to aircraft group classification, starting no later than 30 January 2023. Any cracks found must be repaired before the next flight following Airbus-approved instructions. Inspection results with findings must be reported to Airbus within 90 days. Compliance with the directive’s inspection and corrective action requirements is mandatory.
Summary
EASA Airworthiness Directive 2023-0009 mandates repetitive special detailed inspections of the cockpit lateral window frame vertical stiffeners on Airbus A318, A319, A320, and A321 aircraft, excluding certain modified configurations. The directive addresses potential cracks that could compromise fuselage structural integrity. It applies to all manufacturer serial numbers except those with specific Airbus modifications embodied in production or service.
What changed
This directive supersedes EASA AD 2019-0173 and reduces the compliance times for the required inspections. It retains the inspection requirements but mandates earlier and more frequent inspections based on updated analysis. The directive also clarifies group classifications for affected parts and updates inspection and corrective action procedures.
Why it matters
For operators and maintenance organizations, this directive ensures early detection and correction of cracks in critical cockpit window frame components, preventing potential structural failures. Compliance is essential to maintain airworthiness and avoid grounding of affected aircraft. The updated inspection intervals require careful planning and record-keeping to meet regulatory requirements.
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- EASA AD 2026-0142Wings – Main Landing Gear Support Rib 5 – InspectionsJul 20, 2026
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