What was found
STIFF FLIGHT CONTROLS AIRPLANE ROLLS LEFT WHEN CONFIGURING FOR FLAPS. STIFF AILERONS ONCE FLAPS WERE SELECTED AIRPLANE ROLLED LEFT AND WORSENED WITH GREATER FLAP DEGREE SETTINGS. RIGGED RT AND LT FLAP CONTROL SURFACE SYS IAW AMM 27-54-00-830-801. OPERATIONAL TEST GOOD. ALL SYSTEMS ARE IN TOLERANCE AND FUNCTIONING AS REQUIRED. REFER TO NON-ROUTINE TALLEY CARDS N23584, AND N23585 FOR FURTHER DETAILS.