What was found
DURING C-CHECK FOUND GOUGE IN FUSELAGE (JUST FWD OF STA X531.5 BETWEEN STRINGERS 21S AND 22S). REPAIRED IAW REPAIR DOCUMENT 08-53-08 REV.1, DAMAGE TOLERANCE ANALYSIS BY MFG WITHIN ONE YEAR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK FOUND GOUGE IN FUSELAGE (JUST FWD OF STA X531.5 BETWEEN STRINGERS 21S AND 22S). REPAIRED IAW REPAIR DOCUMENT 08-53-08 REV.1, DAMAGE TOLERANCE ANALYSIS BY MFG WITHIN ONE YEAR.