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STAB TRIM FAULT TO/LAND A minor failure has occurred causing a loss of redundancy in the horizontal stabilizer trim sys-tem. The stabilizer trim will continue to function STALL PROTECT FAULT TO/LAND The Stall Protection Computer has automati-cally reverted to settings for flaps 30 L (R) STALL SHAKER FAIL TO/LAND The respective stall shaker has failed GND SPOILERS OFF The ground spoilers are selected OFF PITCH DISCONNECT The pitch disconnect has been selected. The pilots control column moves the left elevator. The copilot’s control column moves the right elevator. Autopilot will disengage and not re-engage ROLL DISCONNECT The roll disconnect has been selected. The pilot’s control wheel moves the aileron. The autopilot will disengage and not re-engage ROLL SPOILERS OFF The roll spoilers have been turned off and the roll disconnect has been activated RUD LIMITER IN TEST The rudder travel limiter system is conducting the manually activated system test SEC STAB TRIM ON The secondary channel of the horizontal stabi-lizer trim system is selected. The autopilot will be inoperative STAB TRIM OFF The STAB TRIM switch is in the off position. The autopilot will be inoperative STALL PUSHER OFF The stall pusher has been manually deacti-vated Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1 中国公务机网 www.gongwuji.com 公务机翻译 www.aviation.cn 本文链接地址：庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-飞行操纵(15) |
