What was found
UPPER FUSELAGE CARGO CABIN FRAME FAIL SAFE CHORD WITH CORROSION AT BS 1166 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME FAIL SAFE CHORD SECTION AT BS 1166 BETWEEN S-16R AND S-18R DUE TO CORROSION IAW B727 SRM 51-40-3 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE CARGO CABIN FRAME FAIL SAFE CHORD WITH CORROSION AT BS 1166 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME FAIL SAFE CHORD SECTION AT BS 1166 BETWEEN S-16R AND S-18R DUE TO CORROSION IAW B727 SRM 51-40-3 FIG 1.