What was found
ENROUTE FUEL LEAK UNDER RIGHT WING. FUEL MISCOMPARE CAS FOLLOWED BY FUEL IMBALANCE CAS. VISUAL CHECK OUT THE AFT CABIN WINDOW VERIFIED FUEL VENTING OVERBOARD AT A HIGH RATE. DECENDED AND BEGAN OUT DIVERSION THE FUEL LEAK SUBSIDED. ACFT WALKAROUND PERFORMED IAW AMP BD700-A-J12-00-00-02AAA-39BA-A REV 42 & NO FUEL LEAKAGE FOUND. INNER WING TANK PRESSURE RELIEF VALVES OPS TEST PERFORMED IAW AMP BD700-A-J28-11-03-00AAA-320A-A REV 42 & FOUND GOOD. NACA SCOOP GENERAL VISUAL INSP PERFORMED IAW AMP BD700-A-J28-13-19-00AAA-3118-A REV 42 & FOUND GOOD. WING TO WING MANUAL TRANSFER SYS OPS TEST PERFORMED IAW AMP BD700-A-J28-22-00-02AM-320A-A REV 42 & FOUND GOOD. OPS TEST OF FUEL QTY COMPUTER PERFORMED IAW AMP BD700-A-J28-41-03-00AAA-320A-A REV 42 & FOUND GOOD. NOT ABLE TO REPRODUCE FAULT ON GROUND.RECOMMENDED TO INCOPORATE SERVICE BULLETIN SB700-57-7527. REFER TO ADVISORY WIRE AW 700-28-0951 REV 1FOR DETAILS.