What was found
CRACK ON VERTICAL STAB REAR SPAR FILLET CRACKED IN 2 PLACES RT SIDE ABOVE UPPER STRUT RIB 9/10. TRIMMES AFFECTED RIB FLANGES, FABRICATED SHEAR CLIP, FABRICATED FILLER, MATCH DRILLED AND INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON VERTICAL STAB REAR SPAR FILLET CRACKED IN 2 PLACES RT SIDE ABOVE UPPER STRUT RIB 9/10. TRIMMES AFFECTED RIB FLANGES, FABRICATED SHEAR CLIP, FABRICATED FILLER, MATCH DRILLED AND INSTALLED.