What was found
DURING NDT INSPECTION, FWD SERVICE DOOR JAMB CORNER, FOUND ONE CRACK ON UPPER FWD CORNER ON OUTER LAYER OF SKIN. CUT OUT DAMAGE AREA AND REPAIRED IAW SRM 53-05, FIG 112, VIEW D AND ER/A 45.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING NDT INSPECTION, FWD SERVICE DOOR JAMB CORNER, FOUND ONE CRACK ON UPPER FWD CORNER ON OUTER LAYER OF SKIN. CUT OUT DAMAGE AREA AND REPAIRED IAW SRM 53-05, FIG 112, VIEW D AND ER/A 45.