What was found
DURING INSPECTION OF FLIGHT CONTROL SYSTEM, DURING INITIAL 200 HOUR PHASE 1 INSPECTION, IAW SAFETY COMMUNIQUE NR 265, FOUND RUDDER CABLE TENSIONS, RUDDER TAB CABLE TENSIONS, AND ELEVATOR TAB CABLE TENSIONS BELOW APPLICABLE MM SERVICE LIMITS. NO OTHER FAULTS NOTED. A MANDATORY SB IS IN THE PROCESS OF BEING ISSUED ON THIS SUBJECT IAW THE TEXT OF SAFETY COMMUNIQUE NR 265. (K)