What was found
WEAR IN THE FUSELAGE SKIN, FROM RT STAB LOWER FAIRING PANEL AT BS 1862.7, STRINGER 16R. BOTH AREAS ARE BEYOND ALLOWABLE LIMITS OF SRM 53-00-02 DETAIL II. BOTH AREAS REPAIRED IAW SRM 53-80-01 RPR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WEAR IN THE FUSELAGE SKIN, FROM RT STAB LOWER FAIRING PANEL AT BS 1862.7, STRINGER 16R. BOTH AREAS ARE BEYOND ALLOWABLE LIMITS OF SRM 53-00-02 DETAIL II. BOTH AREAS REPAIRED IAW SRM 53-80-01 RPR 2.