What was found
D-CHECK, FWD PIT CORROSION ON FUSELAGE SKIN S26L FS 720-FS 720A (BELOW TRANSITION PANEL). REMOVED CORROSION PER 51-10-6. MARKED AREA AND CUT OUT DAMAGED PORTION OF UPPER AND LOWER SKIN PER 727 SRM 53-30-3 FIG 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
D-CHECK, FWD PIT CORROSION ON FUSELAGE SKIN S26L FS 720-FS 720A (BELOW TRANSITION PANEL). REMOVED CORROSION PER 51-10-6. MARKED AREA AND CUT OUT DAMAGED PORTION OF UPPER AND LOWER SKIN PER 727 SRM 53-30-3 FIG 5.