What was found
CRACK ON LT RING PAN FWD LOWER CORNER, STA Y= 598 AND Y= 889 AT CABIN PASSENGER LEFT SIDE, S/N 00207. DAMAGE WAS REMOVED IAW SRM 56-20-02 REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=598 AND 889 AT CABIN PASSENGER LT SIDE. NO CRACKS WERE FOUND. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 56-20-02, REPAIR 1, FIG 202, AND SRM 51-41-02, AND 51-41-05.