What was found
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT UNDER, FOUND LT AFT FUSELAGE INTERIOR OVERHEAD STIFFENER CRACKED AT FS 935 LBL 15. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-07.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT UNDER, FOUND LT AFT FUSELAGE INTERIOR OVERHEAD STIFFENER CRACKED AT FS 935 LBL 15. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-07.