What was found
SWELLING ON UPPER FUSELAGE SKIN LT SIDE STA 1760 AREA AT STRINGER 3. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, INSTALLED NEW RIVET PER SRM 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SWELLING ON UPPER FUSELAGE SKIN LT SIDE STA 1760 AREA AT STRINGER 3. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, INSTALLED NEW RIVET PER SRM 51-30-02.