What was found
DURING INSPECTION FOUND FUSELAGE SKIN BULGED AT BS 360 +8", S-26L. MAINTENANCE REPAIRED CORRODED STR 8'S, BS 360+8", S-26L IAW PRI 549078-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION FOUND FUSELAGE SKIN BULGED AT BS 360 +8", S-26L. MAINTENANCE REPAIRED CORRODED STR 8'S, BS 360+8", S-26L IAW PRI 549078-14.