What was found
DURING PHASE 10 INSP FOUND THE HORIZ STAB FWD FACE OF THE MAIN SPAR BENT AND CRACKED IN THE CTR OF THE WEB AREA IN BETWEEN THE MAIN ATTACHMENT POINTS TO FUSELAGE STRUCTURE WITH THE STABILIZER REMOVED FROM THE ACFT TAILCONE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING PHASE 10 INSP FOUND THE HORIZ STAB FWD FACE OF THE MAIN SPAR BENT AND CRACKED IN THE CTR OF THE WEB AREA IN BETWEEN THE MAIN ATTACHMENT POINTS TO FUSELAGE STRUCTURE WITH THE STABILIZER REMOVED FROM THE ACFT TAILCONE.