What was found
INSPECTION TYPE: 7C, FUSELAGE MAIN EQUIPMENT CENTER STA 246 LBL 40 FLOORBEAM FWD FACE STIFFENER FOUND CRACKED. REPAIRED IAW SRM 53-10-51-2R4, REPAIR 4, FIG 201, REV 52, ORIG MATL IS BAC1490-2793-7075T62, CRACK LENGTH: 1.1", WITH MATERIAL CLAD 7075T6-0063" AS REPAIR STIFFENER, CLAD 7075T6-0080" AS REPAIR DOUBLER & BAC1512-3347- 7075T6511 AS REPAIR FILLERS, REPEAT INSP AT 3,000 FLIGHT CYC OR 24 MONTHS WHICH EVER OCCURS FIRST IS REQUIRED IAW SRM 53-10-51-2R4.