As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN AT RIB STA 111.10 AT 28" AFT OF FRONT SPAR SHOWS A CRACK. SKIN REPAIRED IAW SRM 55-10-01 REP 11 WITH 1 COMMON DOUBLER. INITIAL INSPECTION TO BE PERFORMED AT 56,000 TOTAL COMPONENT FLT CYCLES FOLLOWED BY REPEAT INSPECTION AT EA 9000 FLT CYCLES IAW STEP 5A, TABLE 204.