What was found
RIGHT WING OUTBOARD L/E UPPER INNER SURFACE - RIB CRACKED .250 AT STA 660.000. STOP DRILLED CRACK IAW SRM 57-2-0 FIG 2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING OUTBOARD L/E UPPER INNER SURFACE - RIB CRACKED .250 AT STA 660.000. STOP DRILLED CRACK IAW SRM 57-2-0 FIG 2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.