What was found
INSPECTION FOUND FUSELAGE FRAME CORRODED ON FORWARD SIDE AT STA 372 BETWEEN STRINGER 17R AND 20R. THE CORRODED SECTION WAS REMOVED AND A FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE FRAME CORRODED ON FORWARD SIDE AT STA 372 BETWEEN STRINGER 17R AND 20R. THE CORRODED SECTION WAS REMOVED AND A FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2.