Bombardier_Challenger_Global_00-Engine_Failure_on_Takeoff
<P>Bombardier_Challenger_Global_00-Engine_Failure_on_Takeoff</P><P> </P>
<P>**** Hidden Message *****</P> ROPAT<BR>Sep 13/2004 Flight Crew Operating Manual Volume 1<BR>REV 1 CSP 100-6 09-14-5<BR>CL300_SOP_004<BR>PF<BR>PNF<BR>“ ” CALL RESPONSE<BR>Initial climb<BR>• V 2 speed<BR>takeoff<BR>flaps<BR>V R rotate<BR>airplane<BR>to command<BR>bar noseup<BR>pitch attitude<BR>V 1 release<BR>thrust levers<BR>“V 1 ”<BR>“POSITIVE RATE”<BR>(when a positive rate of climb is established)<BR>Clear of obstacles<BR>Initial takeoff roll<BR>(standing or rolling<BR>takeoff procedures)<BR>“GEAR UP”<BR>(pitchup to<BR>maintain<BR>V 2 speed)<BR>• Continue climb at<BR>170 KIAS, if necessary<BR>• Reduce thrust to CLB<BR>Clear of obstacles<BR>• Accelerate airplane to<BR>V 2 + 15 kt (min) flaps 10<BR>V 2 + 25 kt flaps 20<BR>Engine Failure (Above V 1 Speed)<BR>Takeoff Continued<BR>Engine<BR>failure<BR>Rudder and ailerons<BR>as required for<BR>directional control<BR>NOTE:<BR>Directional control improves<BR>if nosewheel is kept on the<BR>runway (with forward pressure<BR>on the control wheel) until V R<BR>• “FLAPS 0”<BR>• “ENGINE FAILURE<BR>ABOVE V 1<BR>SPEED<BR>CHECKLIST”<BR>“V 2 + 25”<BR>Keep skid indicator<BR>centered using<BR>rudder or rudder trim<BR>“ROTATE”<BR>(V R )<BR>HDG & FLC<BR>Engine Failure Above V1 Speed<BR>Figure 09-14-02<BR>
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MANUAL 8 MANUAL 8 MANUAL 8 MANUAL 8 MANUAL 8 MANUAL 8 <P>好好学习</P><P>thank you</P> 庞巴迪挑战者动力装置
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