In answer to the tip tank stress question, a full finite element analysis was carried out by the same company that provide such information to Airbus and the tip tanks and screw mounting system I described meet the standard JAR criteria ie an unplanned 9G impact. I do have reservations about the gear as well, hence my point about monitoring the 1800lb recommended MTOW and I have set myself a MLW of 1750lbs except in emergencies and in every event I use my well calibrated ACS AOA to ensure a min speed min ROD arrival.
The non return valve is an Andair product bulkhead mounting CK375 I think, in any event Andy Phillips at Andair will help (best to telephone) I also think Aircraft Spruce sell them. You will also need to modify the vent system to create a higher head and I would recommend specifying your check valve to be made with a tiny bleed so that when the main is filled to capacity via the gravity feeding tip tank you dont empty it out through the main vent. There are a number of other little things to do. I can tell you about them if you choose to proceed. Oh and if the main is full via the tips dont open the main tank fuel cap unless you want to see a blue geyser.
I have only fitted this system for as part of a long distance record breaking suite ( I still have to fit a 60 gallon tank in the right seat and footwell) You have to give some thought to the whole process before proceeding not least the potential performance and structural penalties that can occur. I have thought long and hard as to why I need 12.5 hours endurance. The aircraft can do it but she loses a little of her heart and soul if you know what I mean and as soon as I have done what I need to do the 60 gallon Fuselage tank is out and in the future when I am touring I will do it at the lightest fuel load that is safe for the journey. I have flown an RV6 with a little over 100 gallons on board and while it flew okay it bore little resemblance to the RV6 that we all know and love. Perfectly flyable but you need concentration rather than pure joy to fly if you get what I mean.
Happiness is a lightweight RV,it may be worth considering a nicely tuned 180 hp (Barrett) Lycoming (from memory about 20lbs lighter than a counterweight engine) with a well set up engine monitoring system lots of gap sealing and a stringent minimalist approach to weight. I think 180KTAS would be entirely possible for nearly 4 hours with VFR reserves.
Steve