Bombardier_Learjet-Engine_Failure_onTakeoff起飞时一发失效
<P>Bombardier_Learjet-Engine_Failure_onTakeoff</P><P> </P>
<P>**** Hidden Message *****</P> Recommended Procedures/Techniques Learjet 40/45<BR>3-6 MP-132<BR>May 2004<BR>L40_SOP_004<BR>PF<BR>PNF<BR>“ ” CALL RESPONSE<BR>Initial climb<BR>• V2 speed<BR>takeoff<BR>flaps<BR>VR rotate<BR>airplane<BR>to specified<BR>noseup<BR>pitch attitude<BR>V1 release<BR>thrust levers<BR>“V1”<BR>“ROTATE”<BR>(VR)<BR>“POSITIVE RATE”<BR>(when a positive rate of climb is established)<BR>Clear of obstacles/1500 AGL<BR>Initial takeoff roll<BR>(standing or rolling<BR>takeoff procedures)<BR>“GEAR UP”<BR>(pitch to<BR>maintain<BR>specified<BR>attitude<BR>(V2 speed)<BR>• Continue climb at<BR>200 KIAS, if necessary<BR>1500 AGL and clear of • Reduce thrust to MCT<BR>obstacles<BR>• Accelerates airplane to<BR>V2 + 25 kt (minimum)<BR>Engine Failure (Above V1 Speed)<BR>Takeoff Continued<BR>Engine<BR>failure<BR>Rudder as<BR>required for<BR>directional<BR>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 VR<BR>• “FLAPS UP”<BR>• “ENGINE<BR>FAILURE<BR>ABOVE V1<BR>SPEED<BR>CHECKLIST”<BR>“V2 + 25”<BR>Keep the ball centered<BR>using rudder input<BR>Engine Failure Above V1 Speed<BR>Figure 3 - 2
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