What was found
CRACK IN FRAME HOLE AT UD STA 1160, LT SIDE. TENSION TIE INS STAGE 2. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED FRAME. HFEC IAW NTM, NO CRACK FOUND. MANUFACTURED AND INSTALLED REPAIR PARTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FRAME HOLE AT UD STA 1160, LT SIDE. TENSION TIE INS STAGE 2. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED FRAME. HFEC IAW NTM, NO CRACK FOUND. MANUFACTURED AND INSTALLED REPAIR PARTS.