What was found
AT C-CHECK, ENGINE NR 4 O/B TRANSLATING COWL INNER PANEL SECTION SHOWS CRACK DAMAGE TO INTERIOR SURFACE. STOP DRILLED END OF CRACK, FABRICATED REPAIR PER SRM 71-2-8, 3 X 3.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, ENGINE NR 4 O/B TRANSLATING COWL INNER PANEL SECTION SHOWS CRACK DAMAGE TO INTERIOR SURFACE. STOP DRILLED END OF CRACK, FABRICATED REPAIR PER SRM 71-2-8, 3 X 3.5.