What was found
DURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND CRACKED AT STR 1, BS 430. R&R PER IAW SRM 53-30-3 FIG 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND CRACKED AT STR 1, BS 430. R&R PER IAW SRM 53-30-3 FIG 4.