What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS Ñ2 IN CENTER FUSELAGE ON FRAME36. CRACK DEPTH 0.118 INCH . CRACK DIRECTION 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623119 WO 2025 278/1 ACCOMPLISHED REPAIR ON HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS #2 IN CENTER FUSELAGE ON FRAME 36. IN ACCORDANCE WITH AEROMAN #EA 57-0108-25 REV. 0 (COVER- PARTS 1-3) AND AIRBUS RDAF 81679714/004/2025 ISSUE A I.A.W EC NO. A25-1124-01. THIS REPAIR IS CATEGORY A NO REQUIRED FURTHER INSPECTION.