What was found
F/O REPORTED ACFT REQUIRED "EXCESSIVE" ELEVATOR PRESSURE TO ROTATE ON T/O, WITH TRIM SET AT CALCULATED T/O POSITION. NOTED IN CRUISE, F/O'S YOKE CANTED 10-15 DEGREES TO RT, IN STRAIGHT & LEVEL FLT. VISUALLY INSPECTED ACFT FLIGHT CONTROLS. CHECKED AILERON, AILERON TRIM, ELEVATOR, ELEVATOR TRIM CABLE TENSIONS, & TRAVEL CHECKS. ALL WITHIN LIMITS. PERFORMED ELEVATOR CONTROL CIRCUIT STATIC FRICTION CHECK. CONTROL COLUMN LOADS WITHIN LIMITS. WITH ELEVATOR & AILERON CABLE SECTORS PINNED, CONTROL WHEELS NEUTRAL & FLIGHT CONTROLS STREAM LINED. VISUALLY INSPECTED FLT CONTROL CABLE RUNS. NO DEFECTS NOTED. ALL IAW MM 27-30-00-501 AND 27-10-00-501.