What was found
DURING A LTC INSPECTION, IT WAS DISCOVERED THAT CORROSION ON LEFT 1070 FRAME INBOARD CHORD AT STRINGER 10L. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1070 STRINGER 10L IAW B727 SRM 53-10-4 FIG 2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A LTC INSPECTION, IT WAS DISCOVERED THAT CORROSION ON LEFT 1070 FRAME INBOARD CHORD AT STRINGER 10L. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1070 STRINGER 10L IAW B727 SRM 53-10-4 FIG 2. (M)