As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SKIN CRACKED APPROX 1.5 ON LWR SURFACE OF RT ELEV FWD AND I/B OF TAB CONTROL ROD. DYE CHECKED AND STOP DRILLED CRACKS, FABRICATED REPAIR PART PER SRM 55-20-3 FIG 5. OK TO INSTALL. INSTALLED DOUBLER, FASTENERS AND DOUBLE WEIGH 63G PER SRM 55-20-3 FIG 5.