What was found
AFTER REMOVAL OF SKIN STRINGER BS380 STR38R, FOUND CRACK AT 1EA FASTENER HOLE APPROX 1/8 INCH RUNNING UP AND 3/16 RUNNING DOWN. STRINGER REPAIRED PER SRM 53-10-03 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF SKIN STRINGER BS380 STR38R, FOUND CRACK AT 1EA FASTENER HOLE APPROX 1/8 INCH RUNNING UP AND 3/16 RUNNING DOWN. STRINGER REPAIRED PER SRM 53-10-03 FIG 1.