What was found
WITH SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT, SUBSTANTIALLY. TRIM REQUIRED IS 3 DEGREES LT OF THE TRIM REQUIRED WITH A CLEAN WING. DURING CRUISE THE REQUIRED TRIM IS LESS THAN 1 UNIT RIGHT BOTH RUDDER/AILERON WITH BALANCED POWER & FUEL. FLAP BUSS TENSIONS IN LIMITS IAW AMM 27-50 AT 550 LBS. FOUND FLAP ACTUATORS BYPASSING AT L1, R1, AND R3 POSITIONS. REMOVED L1, R1, R3 FLAP ACTUATORS IAW AMM 27-52. INSTALLED THE FLAP ACTUATORS IAW AMM 27-52. FINAL INSTALLATION SAFTIES, OPS AND LEAK CHECKED GOOD IAW AMM 27-52. (LP3517149)