• Welcome aboard HomebuiltAirplanes.com, your destination for connecting with a thriving community of more than 10,000 active members, all passionate about home-built aviation. Dive into our comprehensive repository of knowledge, exchange technical insights, arrange get-togethers, and trade aircrafts/parts with like-minded enthusiasts. Unearth a wide-ranging collection of general and kit plane aviation subjects, enriched with engaging imagery, in-depth technical manuals, and rare archives.

    For a nominal fee of $99.99/year or $12.99/month, you can immerse yourself in this dynamic community and unparalleled treasure-trove of aviation knowledge.

    Embark on your journey now!

    Click Here to Become a Premium Member and Experience Homebuilt Airplanes to the Fullest!

Rotax 912ULS fuel system question

This site may earn a commission from merchant affiliate links, including eBay, Amazon, and others.

flyvulcan

Well-Known Member
Joined
Aug 6, 2007
Messages
524
Location
Adelaide, Australia
We are installing a Rotax 912ULS into our Lightning Bug and we note that in the Rotax installation manual that between the fuel pump and the carbies is a fuel manifold that splits the single fuel line into two which go to the individual carbies. This manifold also has a fitting for a fuel pressure sensor, as well as a return line to the tank with a restrictor in it (items 13-25 in the attached wrongly oriented diagram).

image.jpg

My question is whether this component (including fuel return line) is a requirement to be fitted or is it optional?

The reason that I ask is that we have seen some 912 installations that do not appear to include this fitting in their fuel systems. We wonder whether these installations are incorrect or whether the use of this component is optional. If so, under what conditions should it be used, or not used?

Of course I will be consulting the Rotax agents, but I'd appreciate some feedback from Rotax 912 experienced forumites.

Thanks,

Dave
 
Last edited:
Back
Top