As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF UNTIL APPROX 10 TO 15 SECONDS AFTER GEAR RETRACTION ABNORMAL RIGHT ROLLING TENDENCY, REQUIRING APPROX 30 DEGREES YOKE DEFLECTION. DURING FLAP EXTENSION ON GROUND TOOK SEVERAL CYCLES OF FLAPS TO EXTINGUISH, SLAT NR 3 AND 4 AMBER LIGHTS ON OVERHEAD PANEL, AMBER LIGHT ON FWD PANEL. ADJUSTED NR 3 L/E SLAT ACTUATOR ROD END PER MM.