As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN HAS 2EA CRACKS ON VERTICAL FASTENER ROW MEASURING 1" LONG AND .250 LONG LOCATED AT LFS 1702, BETWEEN S-10L AND S-11L (VERI FIED WITH HFEC) REF AMES NR 165631-0300-0008 REMOVED DAMAGE. FABRICATED AND INST ALLED DOUBLER 1 AND FILLER 3 IAW SRM 53-00-01 REPAIR 29. TH IS IS A CATEGORY B REPAIR REQUIRING SUPPLEMENTAL INSPECTION AS G IVEN IN TABLE V FIG 201 SHEET 10 NO ADDITIONAL REMARKS.