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Posted

Hi Guys, help me out here. I've never had a manifold pressure gauge. I understand how it operates and I understand what it's reading but I don't know my best settings.

 

Manifoldpressure.thumb.jpg.b5b533330d033066ea6a9c2e2e73c589.jpg

 

When I'm cruising I have to adjust my propeller to a high pitch to prevent the engine running over maximum revs. 

 

What I don't understand is where my best/least fuel consumption comes from when matching RPM to Manifold Pressure while maintaining cruising speed.

 

Lets say I want to keep the Rotax 912ULS spinning at 5000 revs while getting my best economical cruise speed. Do I control this with manifold pressure?

Posted

To make use of your manifold pressure gauge you would need a power chart. Such charts for say a Lycoming O-360A1A will include altitude, rpm, manifold pressure and show fuel flow for each setting. 23-23 @3500 feet is not the same power as 23-23 @5500 feet.

 

Rotax do not seem to publish such charts, good luck finding one.

 

 

Posted

Rotax do publish the manifold pressure/expected fuel flow/ altitude/ engine rpm charts;

 

Join Rotax Owners Forum for all the Manuals/Service letters/etc https://www.rotax-owner.com/en/rotax-forum

 

I strongly advise you read the Rotax 912 ULS Operators Manual file:///C:/Users/User/Downloads/OM_912%20Series_Ed4_Rev2%20(3).pdf

 

Some downloads that may interest you;

 

https://legacy.rotaxowner.com/si_tb_info/serviceletter/sl-912-016-r1.pdf

https://aquila-aviation.de/wp-content/uploads/2021/06/SL_912_016R2_914_014R2_Rotax_Notes_engine_handling.pdf

 

A couple of excerpts;

 

525310675_1434904198081866_8151254740180424223_n.jpg?stp=dst-jpg_s590x590_tt6&_nc_cat=109&ccb=1-7&_nc_sid=e06c5d&_nc_ohc=WooZuqFD2iQQ7kNvwGxZhQx&_nc_oc=AdnFfWGjaHAup8oAKhuiSmID9VjSBcgfcq7P0XhhgyZhURAokvSkYyu2BbUsjhLdUu4uihhxG08zxYuuVuuO0ytz&_nc_zt=23&_nc_ht=scontent-syd2-1.xx&_nc_gid=bhVuobNFsGzAtl2GGIrAYQ&_nc_ss=8&oh=00_AftXOVu77SRXkfgdN1_lB0bVcLA6ZsqCKff0deD8fBiGrg&oe=69A7E8E0525443668_1434904124748540_1480718517832446089_n.jpg?stp=dst-jpg_s590x590_tt6&_nc_cat=105&ccb=1-7&_nc_sid=e06c5d&_nc_ohc=cTdpXktyBxQQ7kNvwF-hgjG&_nc_oc=AdnhKeSN7FIDegv-tHtNGJuxLN18eT4l3GdwkYJnILKPrqR3fZZxJiVT0buiuwdcMAx8tvrIyqmKuFi10zUGvtn6&_nc_zt=23&_nc_ht=scontent-syd2-1.xx&_nc_gid=bhVuobNFsGzAtl2GGIrAYQ&_nc_ss=8&oh=00_AfsWT9tYRpnGGJIHniz9Wg3DCmickfy-f0I9PPrWbY38vA&oe=69A7EB23

 

 

image.jpeg.194664b6020b02ec4b9fd45496d229cf.jpegimage.jpeg.194664b6020b02ec4b9fd45496d229cf.jpeg

 

 

Note: The figures given are nominal ie will differ due to many factors eg airframe😈

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