What was found
HEAVY CHECK COE & MAJOR REPAIR. INTERIOR FUSELAGE SKIN HAS AREAS OF LEVEL 2 CORROSION, 11.2" FWD OF FRAME 22 AT STRINGER 11-11A. REPAIR IAW SRAS CE-5345 15 9684 DATED 10 23 15.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HEAVY CHECK COE & MAJOR REPAIR. INTERIOR FUSELAGE SKIN HAS AREAS OF LEVEL 2 CORROSION, 11.2" FWD OF FRAME 22 AT STRINGER 11-11A. REPAIR IAW SRAS CE-5345 15 9684 DATED 10 23 15.