As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT ELEV, FRONT SPAR CRACKED THROUGH BOTH LAYERS OF SKIN AT LIGHTENING HOLE, JUST INBD OF NR 8 ELEV HINGE. REMOVED REPAIR SECTION OF WEB, FABRICATED NEW WEB PIECES, INSTALLED NEW WEB SECTION. REPAIRED FRONT SPAR CRACK PER SRM 55-21-00 PG 804. INSTALLED LWR SKIN.