What was found
DURING ROUTINE INSP, THE FUSELAGE SKIN FOUND CORRODED BEYOND ALLOWED LIMITS BETWEEN SKIN LAP AT BS 1338, STR 10L. REMOVED AND REPLACED, FAB DOUBLER AND FILLER PER IAW B727 SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSP, THE FUSELAGE SKIN FOUND CORRODED BEYOND ALLOWED LIMITS BETWEEN SKIN LAP AT BS 1338, STR 10L. REMOVED AND REPLACED, FAB DOUBLER AND FILLER PER IAW B727 SRM 53-30-3.