gisurvey Posted July 18, 2012 Report Share Posted July 18, 2012 Hi all, Maybe a dumb question, but... Rotax912ULS What MAP do I have to expect for cruise flight, 5000rpm, 10000'DA? I know that in standard conditions ISA, sea level, for 5000rpm is expected to have 27.2inHg. Thanks, Alec Link to comment Share on other sites More sharing options...
coppercity Posted July 18, 2012 Report Share Posted July 18, 2012 Hi Alec, I usually see between 18-19 in/Hg at those DA's? Link to comment Share on other sites More sharing options...
Ed Cesnalis Posted July 18, 2012 Report Share Posted July 18, 2012 It depends on your prop pitch. Link to comment Share on other sites More sharing options...
gisurvey Posted July 18, 2012 Author Report Share Posted July 18, 2012 Thanks Eric & CT. I know that MAP depends by prop pitch. In fact, I have a variable pitch prop and I want to know what MAP is "ideal" (to be achieved/maintained) for another conditions than ISA. And I'm not quite agree with the rule of thumb to subtract the lapse rate of 1"inHg/1000' from MAP at ISA conditions. Link to comment Share on other sites More sharing options...
Roger Lee Posted July 19, 2012 Report Share Posted July 19, 2012 You should set your prop to see 5500-5600 rpm at your average altitude since you can't fly at that exact altitude all the time. The MAP isn't a great help with the 912 and is better suited for the 914 turbo or constant speed prop. Trying to use the MAP pressure to set the prop will have you chasing a pitch. Go fly (the best way) at your average altitude and fly it at WOT. This will help remove any guess work. Come back and I can tell you what how many degrees to add or remove. Since this is a normal aspirated engine MAP isn't real important. It will always be 1 - 1.5 in. lower. Link to comment Share on other sites More sharing options...
gisurvey Posted July 19, 2012 Author Report Share Posted July 19, 2012 ... I know that MAP depends by prop pitch. In fact, I have a variable pitch prop and I want to know what MAP is "ideal" (to be achieved/maintained) for another conditions than ISA. ... For clarification: is about variable "in-fly" pitch prop, european version CTLS. Link to comment Share on other sites More sharing options...
Ed Cesnalis Posted July 19, 2012 Report Share Posted July 19, 2012 The ideal mp at 10,000 feet is whatever you get pitched for 5,500 rpm and at wide open throttle. Ideal for realizing maximum power that is. If you want to fly around at 65% power or less at that altitude you would use a lower throttle setting and get a lower mp and it would be ideal for 65%. In other words the ideal mp depends on your mission. Most of us are in the US and have fixed pitch props so MP means nothing to us when flying our CTs. Link to comment Share on other sites More sharing options...
Roger Lee Posted July 19, 2012 Report Share Posted July 19, 2012 I'm with Charlie Tango. We have had this discussion and tested this back in early 2007. Ed flies out of high altitude and fly's between 9K'-13.5K' in normal everyday flight. He lives in Mammoth, CA. home to high altitude flying. He's been there and done that. So have the other 100 LSA aircraft owners that I have re-pitched there props. Just fly to 10K' (if that's where you normally fly) and you want to see 5500-5600 rpm WOT and you don't care what the MAP is. Link to comment Share on other sites More sharing options...
gisurvey Posted July 19, 2012 Author Report Share Posted July 19, 2012 ok, thanks for your answers. Link to comment Share on other sites More sharing options...
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