What was found
R/W UPPER SURFACE 6" AFT OF FRONT SPAR AT FUEL PROBE NR 12 HAS A 1" CRACK AT FASTENER HOLE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57- 2-1 FIG 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
R/W UPPER SURFACE 6" AFT OF FRONT SPAR AT FUEL PROBE NR 12 HAS A 1" CRACK AT FASTENER HOLE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57- 2-1 FIG 10.