What was found
RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R. CRACK IS APPROX. 3/8" LONG, PERFORMED A REPAIR IAW SRM 53-31-01 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R. CRACK IS APPROX. 3/8" LONG, PERFORMED A REPAIR IAW SRM 53-31-01 AND 51-40-02.