What was found
FUSELAGE SKIN DENT L/H SIDE STA 807 + 3.5' 2' ABOVE S-22L GROUNDED - YES. REPAIRED FUSELAGE SKIN AT LH STA 807 + 3.5" ABOVE STR-22L IAW B737-800 SRM 53-00-01-2R-3, REPAIR IS CATERGORY B PERMANET REPAIR WITH INSPECTION THRESHOLD OF 50,000 CYCLES AFTER AIRCRAFT DELIVERY, REPEAT INSPECTIONS 4,500 CYCLES AFTER REPAIR INSTALLATION IAW B737-800 SRM 53-00-01-2R-3 TABLE 204. CAT B REPAIR SUBMITTED TO ENGINEERING FOR TRACKING, THIS CLOSES THE ORIGINAL DEFECT.