What was found
AFTER TAKEOFF, SLATS FAILED TO RETRACT. JETTISONED FUEL TO SAFE LANDING WEIGHT, RETURNED TO FIELD AND MADE A SAFE LANDING. PERFORMED FRICTION BRAKE INSPECTION/CHECK IAW A300 AMM 27-81-47 PG 601. TORQUE IS UNDER 27 FOOT POUNDS, WITHIN LIMITS. SLAT/FLAP OPS CHECKED GOOD IAW AMM 27-80-00 PG 501. AIRCRAFT RELEASED TO SERVICE.