AD/F2000/32 - Fuselage - LH Stringer 13 at Frame 8

Requires operators of Dassault Falcon 2000EX aircraft (serials 102–124) to inspect the left‑hand fuselage stringer 13 between frames 7 and 8, and to rework or replace the web if defects are found, following EASA AD 2008‑0143 and Dassault Service Bulletin F2000EX‑178. Compliance is mandatory before 3,750 total flight cycles or within 74 months of delivery, whichever is earlier; the operator bears inspection, repair and downtime costs to address the structural risk identified by the regulator.