Fennec Posted December 6, 2018 Report Share Posted December 6, 2018 I am trying to figure out single engine configuration of Bell helicopter if one engine is to shut down. The helicopter was flying in following conditions :- Weight - 10606 pounds Altitude - 7000 feet pressure altitude Temperature - 34 degree Celsius Air Speed - 70 KIAS According to the OEI performance graph of 11000 weight category given in Rotorcraft Flight Manual the Bell helicopter will get a rate of descend of 370 feet per minute. My query is that if pilot is flying the helicopter in weight configuration, OAT and altitude given above and has to shut down one engine then what will be the 'single engine configuration' in which pilot has to bring the helicopter before resorting to single engine ? Quote Link to comment Share on other sites More sharing options...
vaporlock Posted December 6, 2018 Report Share Posted December 6, 2018 Probably an airspeed that is conducive to single engine operations Quote Link to comment Share on other sites More sharing options...
hybrid Posted December 6, 2018 Report Share Posted December 6, 2018 2 hours ago, vaporlock said: Probably an airspeed that is conducive to single engine operations Exactly my thoughts, best rate of climb, and minimum rate of descent. Bell probably uses 70 KIAS as both, the charts should tell you that. Quote Link to comment Share on other sites More sharing options...
Blackmac Posted December 6, 2018 Report Share Posted December 6, 2018 At that altitude, weight and temperature, I would use the holy Shyte Graph and hopefully you have a level surface to land on!!!!!!😱 Have fun,Don. 1 3 Quote Link to comment Share on other sites More sharing options...
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