What was found
DURING C1 CHECK, PERFORMED DVI OF FUSELAGE SKIN INTERNALLY ON AREAS EXPOSED BY REMOVAL OF THE SIDE FRAME FITTING HAS CORROSION. REPAIR ACCOMPLISHED ON WORK ORDER# 47008ORD09. AIRCRAFT RETURNED TO SERVICE AFTER C1 CHECK COMPLETED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C1 CHECK, PERFORMED DVI OF FUSELAGE SKIN INTERNALLY ON AREAS EXPOSED BY REMOVAL OF THE SIDE FRAME FITTING HAS CORROSION. REPAIR ACCOMPLISHED ON WORK ORDER# 47008ORD09. AIRCRAFT RETURNED TO SERVICE AFTER C1 CHECK COMPLETED.