What was found
ENGINE NOSE COWL UPPER FWD EDGE OF COMPOSIT PANEL HAS DAMAGE IN TWO AREAS. REMOVED DAMAGE AND APPLIED REPAIR IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE NOSE COWL UPPER FWD EDGE OF COMPOSIT PANEL HAS DAMAGE IN TWO AREAS. REMOVED DAMAGE AND APPLIED REPAIR IAW SRM.