What was found
DURING 100 HR INSPECTION, LT ANCHOR WAS WORN AT MASTER CYLINDER ATTACH, OBLONGED HOLE. BULKHEAD WAS BROKEN AT RUDDER BAR ATTACH RESULTING IN POOR BRAKING AND LIMITED LT RUDDER TRAVEL. REPAIR WITH NEW PARTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 100 HR INSPECTION, LT ANCHOR WAS WORN AT MASTER CYLINDER ATTACH, OBLONGED HOLE. BULKHEAD WAS BROKEN AT RUDDER BAR ATTACH RESULTING IN POOR BRAKING AND LIMITED LT RUDDER TRAVEL. REPAIR WITH NEW PARTS.