As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACKING IN FRAME ANGLE WHICH MOUNTS INSTRUMENT PANEL TO FUSELAGE AND CRACKS IN ADJACENT CHANNEL AND FUSELAGE SKIN. SUSPECT CRACKING BECAUSE OF LANDINGS MADE IN TRAINING AIRCRAFT. SUGGEST CLOSE INSPECTION OF STRUCTURE MOUNTING INSTRUMENT PANEL EVERY 100 HOURS OR ANNUALLY.