As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND TWO CRACKS ON AFT RT SIDE OF FUSELAGE. MAIN CRACK IS 3.4 INCH LONG. A SPLINTER CRACK OFF THE MAIN CRACK IS 1.9 INCH LONG. BOTH CRACKS ARE JUST AFT OF THE RT ELEVATOR ACCUMULATOR ACCESS PANEL, FS CANT 1474 LONG NR 21. NOTE ALREADY PERFORMED HFEC TO FIND END OF CRACKS. REPAIRED SKIN CRACKS IAW SRM 53-01 FIG 2 SHT 3.