What was found
DURING CONTROL CHECK CAP`S YOKE TURNED RT, THEN LT, THEN BACK TO CENTER, COPILOTS YOKE STAYED IN A FULL LT TURN WHEN CAPS WAS BROUGHT BACK TO CENTER. DURING TAXI BACK, WAS A NOTICEABLE CLICKING SOUND ANYTIME YOKE MOVED. DUPLICATED SQK. PER ENGINEERING, CHKD GAP AT DISCONNECT SECTOR STOP & GAP BETWEEN UPPER & LOWER SECTOR HALVES. GAP FOUND TO BE .072" BOTH CASES. PILOT'S WHEEL IS TURNED LT, BOTH GAPS GET TIGHTER, TO .060", & WHEN TURNED RT, EXPAND TO .080". REPLACED AILERON DISCONNECT SECT IAW MM 27-13-00. ACCOMPLISHED AILERON CONTROL CABLE RIGGING, & CABLE TENSION GOOD IAW MM 27-10-00. R & R LT AILERON ATTACH HARDWARE IAW MM 57-60-05, REV 7. ACCOMP CONTROL SURFACE & TRIM TRAVEL CHECK, 0.9:1 RATIO IAW MM 27-10-00, REV 19. CONTROL SURFACE TRAVEL CHKD GOOD AT 0.9:1 RATIO. ACCOMP ROLL SPOILER/SPEEDBRAKE TRAVEL CHECKS IAW MM 27-65-00. ACCOMP AILERON CONTROL SURFACE CHECK, 0.6:1 RATIO IAW MM 27-10-00. ACCOMP AUTOTHROTTLE OPS CHK IAW MM 22-30-00. VERIFIED ROLL SPOILER, SPEEDBRAKE CHECKS . VERIFIED AILERON CONTROL CHECK, 0.6:1 RATIO. ORIGINAL SUBMISSION DATE: 11/04/2024.