As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING JACKING OF DATUM AIRPLANE, MX DAMAGED THE FUSELAGE SKIN SECTION 48 - BS2594.5 AT S-26R (ABOVE THE TAIL JACK PAD). MEASURING 2.5 IN. D AND 0.437 IN DEPTH. THE DAMAGE IS LOCATED APPROX 3.5 IN FWD OF BS 2598 BUTT JOINT. "INTERIM REPAIR PERFORMED AS DESCRIBED IN PART 1 WORK INSTRUCTIONS IAW SRM 53-30-03 FIG 1. (SHEETS 1-9)" EO4753B233.