What was found
LEFT FUSELAGE UPPER LOBE INTERIOR AT BS 1280 BETWEEN STRINGERS 11 & 15L GOUGED. REMOVED DAMAGE IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. INSTALLED REPAIR IAW SRM 53-00-07 REPAIR 3 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FUSELAGE UPPER LOBE INTERIOR AT BS 1280 BETWEEN STRINGERS 11 & 15L GOUGED. REMOVED DAMAGE IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. INSTALLED REPAIR IAW SRM 53-00-07 REPAIR 3 FIG 201.