As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN HAS CORROSION AT THE FORWARD SERVICE SCUFF PLATE ATTACH FASTENER HOLE 15OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 020-0001:5331-01297- 01B/001 00134 COMPLY WITH PRI 626480-14 REV 0, 1 AND ERA 626480-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 020-0001:5331-01297-01B/001 00134 COM PLIED WITH PRI 626480-14 REV 0, 1 AND ERA 626480-14 REV ORIGINAL. (LP# 1018223)