HI, ONE OF OUR 737-800 (WINGLETS), OPERATES DAILY TO THE DESERT. DURING LAST 12 MONTHS WE HAVE RECEIVED MANY PILOT REPORTS RELATED TO HEAVY CONTROL WHEEL FORCES IN ROLL AXIS, SUCH AS :
1) AILERON CONTROL WHEEL STIFFNESS, ESPECIALLY AT FULL RANGE TRAVEL
2) SPEEDBRAKE HANDLE STIFFNESS.
3) AILERON INPUTS ARE VERY HARD WITHOUT AUTO PILOT. DIFFERENCE IN AILERON TRIM UNIT IS ONE.
4) AILERON TRIM DISPLACED 1 UNIT TO THE RIGHT ON F/O CONTROL COLUMN WITHIN CAPT INDICATES ZERO CENTER.
5) FLT CONTROL STIFFNESS PERSISTS IN ROLL AXIS AND SPEED BRAKE HANDLE TO FLT DETENT.
NOTE: CAM FOLLOWER BEARING REPLACED AUG 2017, DEFECT PERSIST. SPOILER MIXER AND RATIO CHANGER REPLACED OCT 2017, DEFECT PERSIST.
6) LATEST REPORT 3 JULY 2018 AND TROUBLESHOOTING AS BELOW:
DURING PRE-FLIGHT CHK, FLIGHT CONTROLS NOTED TO BE STIFF IN THE ROLL AXIS WITH HYD SYS PRESSURIZED.
AILERON CENTERING MECHANISM CENTERING SPRING ADJUSTED, FORCE TEST C/OUT SATIS. DURING PREFLIGHT CHKS,
FOLLOWING WAS NOTED, AFTER HYD SYS PRESSUIRZED, CAPT FLIGHT CONTROL POSITION CENTERED/ F/O FLIGHT
CONTROL 1 DEGREE OFFSET. T/SHOOTING C/OUT BODY CABLE AA & AB FOUND SATIS. ROLL FORCE TRANSDUCER WIRE
BUNDLE CHECKED IF TOO TIGHT FOUND SATIS. AILERON TRANSFER MECHANISM INSPECTED FOR EXCESSIVE FRICTION.
FOUND SATIS. CONTROL COLUMN U JOINT & SUPPORT BEARING INSPECTED FOUND SATIS. TENSION CHECKED ON CABLES
ABSA & ABSB. FOUND SATIS, SAME ABOVE CABLES INSPECTED FOR CONDITION & BLOCKAGE. ALL FOUND SATIS. LEFT
AILERON DEFLECTED DOWN WHILE RIGHT IS FLUSH WITH HYD SYS PRESSURIZED. RIGHT WING SPOILER PANELS 8/9/10/11
DEFLECTED.
ANY RECOMMENDATIONS ARE APPRECIATED.
BRGDS