What was found
FUSELAGE SKIN INTERIOR SURFACE HAD SURFACE CORROSION FROM LONGERON 26 RIGHT TO 26 LEFT AT AFT PRESSURE BULKHEAD TEE CAP AREA. REPAIRED SKIN IAW DC9 SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN INTERIOR SURFACE HAD SURFACE CORROSION FROM LONGERON 26 RIGHT TO 26 LEFT AT AFT PRESSURE BULKHEAD TEE CAP AREA. REPAIRED SKIN IAW DC9 SRM.