What was found
CRACK ON LT RING PAN FWD UPPER CORNER STA Y= 674-693 AT INTERNAL FUSELAGE STRUCTURE. REMOVE FASTENERS AND DAMAGE, REPAIR PARTS WERE FABRICATED, TREATED PAIN PAINTED, NDT CHECKED, REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-5, 51-30-2, 51-10-3 PAR 21, 14 ERA 493648-14MA, REV ORIGINAL.