What was found
FOUND CRACK IN FUSELAGE FAIRING PANEL BETWEEN A/C BAYS AT FORWARD ADF PANEL, APPROX STA 1000. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC INSPECTED AND DETERMINED CRACK ENDS AT STOP DRILL IAW MM 51-00-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CRACK IN FUSELAGE FAIRING PANEL BETWEEN A/C BAYS AT FORWARD ADF PANEL, APPROX STA 1000. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC INSPECTED AND DETERMINED CRACK ENDS AT STOP DRILL IAW MM 51-00-00.