What was found
HEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 15 - 16, STRINGER 10 - 11. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 15 - 16, STRINGER 10 - 11. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 201.