What was found
FUSELAGE STRUCTURE, BENEATH OUTFLOW VLV, FRAME 66, STRINGER 31R, CORROSION. R & R STRINGER 31R, FROM FRAME 64 - 66 IAW SRM 51-42-11 PGS 25 - 26.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STRUCTURE, BENEATH OUTFLOW VLV, FRAME 66, STRINGER 31R, CORROSION. R & R STRINGER 31R, FROM FRAME 64 - 66 IAW SRM 51-42-11 PGS 25 - 26.