What was found
DURING C-CHECK INSPECT, RT FWD FUSELAGE BELOW FWD STATIC PORT, DOUBLER THICKNESS RATIO EXCEEDED MAX ALLOWED, ALUMINUM RIVETS USED IN LONGERONS. REWORK REPAIR IAW TO BRING INTO CONFORMANCE, STA FS 195, L-35R. PERFORMED MAJOR REPAIR IAW FAA 8110-3 NR 05367 DATED 08-19-05, SEMAN DWG ED 4045 DATED 08-12-05 AND EO SEMAN NR 20051122 DATED 08-19-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PAGE 21. TRIMMED OUT DAMAGED AREA IAW SEMAN DWG ED 4045. PERFORMED NDT INSPECT IAW DC-8 NDT SPM, PART 06-10-01-001. FAB`D REPAIR DOUBLER, INTERNAL FINGER DOUBLER & FILLER IAW SEMAN DWG ED 4045, DC8 SRM 51-1-4 PAGE 1. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4045, DC-8 SRM 51-1-20D PG 9, DC8