What was found
(CAN) PRODUCTION FLIGHT TEST 1 (2002-12-21) UNABLE TO AIRSTART RT ENGINE EITHER WINDMILL OR WITH AIR TURBINE START. N2 REMAINED AT 0 PERCENT EVEN WITH ATS ENGAGED. RNC (RAPPORT DE NON CONFORMANCE) C302087572 RAISED. PILOTS TO CARRIED OUT DISPOSITION OF RNC AS PER PROPULSION ENGINEERING ON NEXT FLIGHT. PRODUCTION FLIGHT TEST 2 (2002-12-23) REPEAT OF SNAG FLIGHT NR 1. RT ENGINE N2 TURNED FREELY AFTER LANDING DURING MOTORING ON APU BLEED. ON NEXT FLIGHT, BREAK-IN PROCEDURE CARRIED OUT PRIOR TO RESTART ATTEMPT. AFTER BREAK-KN PROCEDURE REPEAT WINDMILL RELIGHT PROCEDURE PER PROPULSION ENGINEERING DISPOSITION. PRODUCTION FLIGHT TEST #3 (2002-12-23) WINDMILL PORTION OF WEAR IN PROCEDURE UNSUCCESSFUL. ATS RELIGHT AFT