I am rebuilding my 46 BC12D and have purchased the Harer STC. My plane always had two wing tanks. I am perplexed about the redundant fuel vent system that is included in the plans. I will comply with the STC but have doubts about what was actually intended. I have the following observations from the STC plans and paperwork Any help with the following would be greatly appreciated.
1. Taylorcaft never used this extra vent system and relied on the vented fuel caps my airplane has always had. Why are they needed now?
2. The STC drawing G-133 has a “Schematic Layout _vent Line” in that drawing it has a note “See Dwg G-170. G-170 has been eliminated in the revision to the STC. That lists the drawings to be used in the conversion.
3. There is also a “vent kit” drawing in the Packet of plans I received form Mr. Harer. It clearly shows a main fuel tank that is different that the one on Dwg G-133. It appears to be used with a main tank that has a place for a different fuel gauge than the cork and wire that my plane had.
4. The plans also come with a drawing of how to modify fuel caps for the wing tank to make them vented. Dwg G-160.
5. G-133 shows both wing tanks installed in the wings with the original Taylorcraft style vents in the cap and NO additional vent lines installed.
My own interpretation of the above conflicts in the plans is this. Taylorcraft built and certified the wing tanks without this vent system. Most Cubs I know with 85 and 90 hp engines just use the plane old fuel cap with wire gauge and no addition vent other than caps. Since drawing G-170 was eliminated that had something to do with the fuel venting system. Is it possible that just vented wing caps were all that was intended unless you had the internal gauge in the main tank and a non vented main tank. In which case the venting system would be needed. I have seen at least one Main tank like this and it appears that with the Internal gauge a venting port was installed on the top of the tank.
Sorry for all the long detail, but I do not like the fuel vent system and not that keen on the Soldered fittings in the filler neck.
1. Taylorcaft never used this extra vent system and relied on the vented fuel caps my airplane has always had. Why are they needed now?
2. The STC drawing G-133 has a “Schematic Layout _vent Line” in that drawing it has a note “See Dwg G-170. G-170 has been eliminated in the revision to the STC. That lists the drawings to be used in the conversion.
3. There is also a “vent kit” drawing in the Packet of plans I received form Mr. Harer. It clearly shows a main fuel tank that is different that the one on Dwg G-133. It appears to be used with a main tank that has a place for a different fuel gauge than the cork and wire that my plane had.
4. The plans also come with a drawing of how to modify fuel caps for the wing tank to make them vented. Dwg G-160.
5. G-133 shows both wing tanks installed in the wings with the original Taylorcraft style vents in the cap and NO additional vent lines installed.
My own interpretation of the above conflicts in the plans is this. Taylorcraft built and certified the wing tanks without this vent system. Most Cubs I know with 85 and 90 hp engines just use the plane old fuel cap with wire gauge and no addition vent other than caps. Since drawing G-170 was eliminated that had something to do with the fuel venting system. Is it possible that just vented wing caps were all that was intended unless you had the internal gauge in the main tank and a non vented main tank. In which case the venting system would be needed. I have seen at least one Main tank like this and it appears that with the Internal gauge a venting port was installed on the top of the tank.
Sorry for all the long detail, but I do not like the fuel vent system and not that keen on the Soldered fittings in the filler neck.
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