by pappas » Sun Dec 22, 2024 4:18 pm
2 more pictures would be helpful. One each from the left and right side of the fitting and from a bit farther away as to show more of the surrounding area. I also don't know what part of the fitting is rotating exactly. However, I can tell you that The blue/red fitting in your image should not rotate at all. If the Blue female nut is rotating on the red male hose end, then it is not tight enough. If the hose clamp is not tight enough on the lower hose, then the hose could rotate on the female hose end fitting, (less likely due to the friction of the hose on the barbed fitting end). Still, the clamp needs to be tight.
It is difficult to see exactly how the upper hose is attached to the blue female nut.
(Sidenote- Is the upper blue female nut attached to a metal threaded elbow that threads into the turbo body?) If so, that can be a source of the leak as well. If you are saying that the upper blue female nut is attached to a metal elbow, and, it is that elbow that rotates where it threads into the turbo...that would likely be your leak. If the elbow threads into the turbo body it has to be tight and should have an appropriate thread sealant on those threads as well. It is best to tie the plane down, turn on the cooling pump, and run it with a safety pilot in the cabin and you can watch the fittings under varying RPM settings to see if you can spot the leak occurring. You might be able to get away with just running the cooling pump and not running the engine. Try that first, you can do that alone.
Remember, a lot of leaks start somewhere else, follow the pull of gravity or the direction of the airflow, and manifest themselves in another location.
These aluminum hose fittings can be a source of the leak and should be inspected to make sure they are not loose nor too close to anything that gets hot enough to melt a hose. Sometimes you just have to take them apart, inspect, repair, replace, or re-route them to a better spot.
At worst case, you do not need to remove the engine. The turbo can be unbolted from the manifolds and linkages, and removed by itself so you can re-think the attachment fittings or the clocking of the turbo. (Read about "clocking the turbo in the install manual. If you are lucky, re-clocking the turbo may be all you need to get the fitting off the firewall.) I was never very happy about how close the turbo was to the firewall on my Waiex, but there is room there for just enough clearance to keep everything from rubbing if the positioning of the components is well thought out.
Nothing on the engine should be contacting the firewall. The in-flight vibration and start-up/shut-down vibration will cause you problems later. I don't think you have a major issue here, just a slightly pain-in-the-butt maintenance issue.
Lou Pappas
Phoenix, AZ
RV-7A Flying (2024)
Waiex B Turbo (2016)
RV-8 (2009)
Waiex Legacy 3300 (2007)
Hiperlight SNS-9 (1991)
Falcon Ultralight (1989)