What was found
RT DRAG ANGLE (EMPENAGE-VERTICAL) APPEARS CRACKED. PERFORMED ET INSPECTION OF SUSPECT CRACK IAW NDTM 51-20-006. FOUND ANGLE TO BE CRACKED. MARKED END OF CRACK. (B)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT DRAG ANGLE (EMPENAGE-VERTICAL) APPEARS CRACKED. PERFORMED ET INSPECTION OF SUSPECT CRACK IAW NDTM 51-20-006. FOUND ANGLE TO BE CRACKED. MARKED END OF CRACK. (B)