What was found
RW INTERNAL HYDRO-PRESSED RIB TO STRINGER STA 686.50 STRINGER 2ND FRAME AFT IS CRACKED. STOPED DRILLED PER MM 57-13-00 FIG 801. REMOVED FUEL PROBE DRILLED NEW REPAIR DOUBLER PER MM 53-13 AND INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RW INTERNAL HYDRO-PRESSED RIB TO STRINGER STA 686.50 STRINGER 2ND FRAME AFT IS CRACKED. STOPED DRILLED PER MM 57-13-00 FIG 801. REMOVED FUEL PROBE DRILLED NEW REPAIR DOUBLER PER MM 53-13 AND INSTALLED.