EASA AD 26-013
Fuselage — Door Frames Holes — Inspection
EASA Airworthiness Directive 26-013 is a proposed directive addressing inspection requirements for door frame holes on Airbus A300-600 and A310 aeroplanes. It mandates repetitive high frequency eddy current inspections of specific seal retainer run out rivet holes at frames 56A, 57A, and 73A on both left-hand and right-hand sides. The directive applies to all manufacturer serial numbers of the affected aircraft models.