What was found
FUSELAGE SKIN IS GOUGED FWD EDGE OF C-1 DOOR BETWEEN DOOR CUT-OUT AND ALT STATIC PORT. REPAIRED AREA IAW SRM 53-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN IS GOUGED FWD EDGE OF C-1 DOOR BETWEEN DOOR CUT-OUT AND ALT STATIC PORT. REPAIRED AREA IAW SRM 53-00-01.