As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H STABILIZER RIB 92.7, VERTICAL STIFFNERS NR 2 AND 3 CRACKED 1 INCH ABOVE LOWER FLANGE. SKIN WAS CUT TO OBTAIN ACCESS TO REPAIR VERITCAL STIFFNERS, SKIN CUT OUT REPAIRED PER SRM 55-10-01 REPAIR 11 TABLE 204 INCORPORATING PREVIOUS REPAIR ON LP 9626841. NEW DOUBLER LOCATION: STA 88 TO 111, 7 TO 43 INCHES AFT OF FRONT SPAR. STIFFNERS REPAIRED PER SRM 55-10-09 REPAIR 4 .