As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ANNUAL INSPECTION AND AD 94-20-04 PARA (B) COMPLIANCE FOUND BEECH KIT 35-4016-3 (STAB REINFORCEMENT) LEADING EDGE CUFF ATTACH RIVETS FAULTY. FOUND LT CUFF ON THE RT SIDE AND RT CUFF ON LT SIDE. REVERSAL CAUSED A MISFIT OF CONTOUR AND INADQUATE RIVETING.