What was found
THE FUSELAGE SKIN BETWEEN FS 586 TO 600 AND STR 27R TO 28R WAS CORRODED. REPAIRED PER B727 SRM 53-30-3, FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN BETWEEN FS 586 TO 600 AND STR 27R TO 28R WAS CORRODED. REPAIRED PER B727 SRM 53-30-3, FIG 3.