chuckb Posted January 20, 2011 Share Posted January 20, 2011 Hey all, I'm trying to get a clear picture of what is happening when this occurs and what does the crew see when this happens. I understand the basics of the low pitch stop, but having never seen one that failed to extend, it's hard to get a clear idea of what all is going wrong. Thanks. Quote Link to comment Share on other sites More sharing options...
pjvr99 Posted January 20, 2011 Share Posted January 20, 2011 Difference in torque at FI when throttle is moved from GI to FI, and when moved from above FI back to FI. Difference should be a minimum of 500"lb (200"lb on some special variants). Sometimes a failure will be indicated by no difference, while the torq may hold for a few seconds when coming back to FI, before dropping off. Also in static operation, no hesitation at LPS angle is noted on protractor when unfeathering to GI or Reverse Quote Link to comment Share on other sites More sharing options...
galgany2009 Posted February 14, 2011 Share Posted February 14, 2011 MAKE SURE THAT YOUR FLIGHT IDLE ANGLE NOT LESS THAN 17.5 DEGREE.BECAUSE YOUR LOW PICH STOP WILL NEVER ENGAGED IF YOU DONOT GET 23.5.( 6 DEGREE U GET FROM LOW PICH STOP).FOR A NEW PROP MAY BE THE LOW PITCH STOP NEED TO BE ADJUSTED SCREW IN TO INCREASE.AS PER MM.RECORD YOUR TOP OF BETA TORQUE GO TO CROSSOVER AND COME BACK TO TOP OF BETA.TORQUE INCREASE OF 200INLB.MUST BE INDICATED MORE THAN THE RECORDED TORQUE IN TOP OF BETA.HESITATION MUST BE OBSERVED AS WELL. Quote Link to comment Share on other sites More sharing options...
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