What was found
RIGHT UPPER FUSELAGE SKIN WAS CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, THE CRACK WAS APPROXIMATELY 1 INCH LONG . PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01, FIG 219
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT UPPER FUSELAGE SKIN WAS CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, THE CRACK WAS APPROXIMATELY 1 INCH LONG . PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01, FIG 219