What was found
TWO WING DEICE LINES AND CLAMPS LOCATED AT FUSELAGE AND WING LEADING EDGE, CHAFE FUSELAGE SKIN. SUBMITTER STATED SHRINK WRAP AND THERMOPROTECTION TAPE SHOULD BE EXTENDED FORWARD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO WING DEICE LINES AND CLAMPS LOCATED AT FUSELAGE AND WING LEADING EDGE, CHAFE FUSELAGE SKIN. SUBMITTER STATED SHRINK WRAP AND THERMOPROTECTION TAPE SHOULD BE EXTENDED FORWARD.