What was found
BLENDED CORRODED AREA OF THE EXTERIOR FUSELAGE LH SKIN FORWARD OF THE CABIN DOOR AT FS145 AND WL 107.7, PERFORMED NDT AND SUBMITTED FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED REPAIR AREAS PER TEXTRON FIELD REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BLENDED CORRODED AREA OF THE EXTERIOR FUSELAGE LH SKIN FORWARD OF THE CABIN DOOR AT FS145 AND WL 107.7, PERFORMED NDT AND SUBMITTED FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED REPAIR AREAS PER TEXTRON FIELD REPAIR.