What was found
HEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL FWD OF FRAME 21, BETWEEN STRINGER 8 - 10. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.
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 FWD OF FRAME 21, BETWEEN STRINGER 8 - 10. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.