What was found
EXTERNAL FUSELAGE SKIN STA 1520-1540 BETWEEN STR 22R TO STR 23R HAS DENT. FOUND OUT LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. CUT-OUT DAMAGE AREA 1.100" LONG X 0.800" WIDE AT STA 1522 BETWEEN STR 22R- STR 23R IAW SRM 53-00-01 REPAIR 16. PERFORMED SURFACE HFEC INSP OF CUT OUT IAW NTM 51-00-19, PT 6 WITH NO CRACKS NOTED. PERFORMED HFEC ROTARY PROBE INSP OF ALL HOLES IAW NTM 51-00-16, PT 6 WITH NO CRACK INDICATIONS NOTED. FABRICATED REPAIR DOUBLE, LOCATED & DRILLED AND INSTALLED REPAIR IAW SRM 53-00-01, REPAIR 16. THIS IS A CATEGORY "B" REPAIR, INSP THRESHOLD FLIGHT CYCLES IS REQ- IAW SRM 53-00-01, REPAIR 16 PAGE 206 TABLE V, MAJOR REPAIR.