What was found
ON ARRIVAL DISCOVERED FUSELAGE SKIN TORN, ONE INCH LONG, BS 293 BETWEEN STRINGERS 21 - 22R. REPAIRED IAW AVO 125-17-04-04-01, STEP 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON ARRIVAL DISCOVERED FUSELAGE SKIN TORN, ONE INCH LONG, BS 293 BETWEEN STRINGERS 21 - 22R. REPAIRED IAW AVO 125-17-04-04-01, STEP 4.