What was found
FUSELAGE FRAME IS WORN AT LT SIDE 10:00 POSITION APPROXIMATELY 48 INCHES AFT OF AFT PRESSURE BULKHEAD. REPAIRED IAW SRM 53-10-02, FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME IS WORN AT LT SIDE 10:00 POSITION APPROXIMATELY 48 INCHES AFT OF AFT PRESSURE BULKHEAD. REPAIRED IAW SRM 53-10-02, FIG 2.