What was found
LEFT WING, OTBD FLAP, TOP SURFACE CHAFED AT 2 PLACES. FLAP TOP SKIN BLENDED IAW RD8-57-1022 AT STAX 403.0 0.023" MATERIAL REMAINING HFEC AND UT THICKNESS INSPECTION DONE. NO CRACK FOUND.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING, OTBD FLAP, TOP SURFACE CHAFED AT 2 PLACES. FLAP TOP SKIN BLENDED IAW RD8-57-1022 AT STAX 403.0 0.023" MATERIAL REMAINING HFEC AND UT THICKNESS INSPECTION DONE. NO CRACK FOUND.