What was found
LOWER FUSELAGE: STA 250 TO STA 260 FWD BULKHEAD R/H SIDE T-CHORD FOUND CRACKED.(<P >AT R/H NOSE W/W FWD BULKHEAD STA 250 TO STA 260, CRACKED T-CHORD REMOVED AND INSTALLED WITH NEW FABRICATED T-CHORD AS PER EN 3565-26 REV.0. REPAIR CLASSIFIED AS "MAJOR" REPAIR WITH FIRST AND SECOND STAGE APPROVAL. NO ADDITIONAL STRUCTURAL WORK REQUIRED. INSPECTION THRESHOLD OF 23,941 TOTAL FLIGHT CYCLES. TO BE COMPLIED WITH SUBSEQUENT TO FAA APPROVAL REQUIREMENTS BEFORE REACHING THE INSPECTION THRESHOLD. NO FURTHER DEFECTS NOTED.</P>)