What was found
HEAVY CHECK COE & MAJOR REPAIR. INTERIOR FUSELAGE SKIN HAS AREA OF LEVEL 2 CORROSION, 2" AFT OF FRAME 23, 1.1" ABOVE STRINGER 10A. BLEND 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 AREA OF LEVEL 2 CORROSION, 2" AFT OF FRAME 23, 1.1" ABOVE STRINGER 10A. BLEND REPAIR IAW SRAS CE-5345 15 9684 DATED 10 23 15.