I am well into my rebuild of the wings on my 1946 BC12-D. I have a question about the tubing used originally in the left wing for the pitot tube and the static line.
The plane is a 1946 BC12D sn 7700 with the Gilbarti/Harrer STC converting to an 85 HP BC12-D-4-85. The wings got hailed on a couple of years ago, and a hairline crack in the spar from under the root plywood sealed the deal on a complete rebuild.
The wing was certainly played with in 1973 when the STC was applied with the new spar root bushings and the modifications to the strut attach fittings. The aircraft was mostly dormant until the early 1990s when it was recovered with Stits. There is no history of any modifications to the static system. The static system seems to follow the factory drawing that I have showing both the pitot and static lines running up the left door post and into the nose of the left wing root rib. The static line just terminates at the first rib and the pitot continues out through rubber grommets in the nose ribs the the jury strut where the tubing connects with the pitot tube on the front jury strut.
My question concerns the tubing used for the pitot and static lines. The existing lines seem to be soft copper tubing with rubber tubing pieces held tight with wire ties serving as connectors between tubing pieces. The tubing is 0.190" outside diameter and about 0.085" internal diameter. My question is: What type of tubing was used on the original BC12-D? Is the soft copper original? What would be the best (approved!) tubing to be used today?
Any comments or suggestions are welcome, and any reference to real approved data will be met with shouts of glee!
Thanks loads in advance.
Skip Egdorf
TF #895
BC12D-4-85 N34237
The plane is a 1946 BC12D sn 7700 with the Gilbarti/Harrer STC converting to an 85 HP BC12-D-4-85. The wings got hailed on a couple of years ago, and a hairline crack in the spar from under the root plywood sealed the deal on a complete rebuild.
The wing was certainly played with in 1973 when the STC was applied with the new spar root bushings and the modifications to the strut attach fittings. The aircraft was mostly dormant until the early 1990s when it was recovered with Stits. There is no history of any modifications to the static system. The static system seems to follow the factory drawing that I have showing both the pitot and static lines running up the left door post and into the nose of the left wing root rib. The static line just terminates at the first rib and the pitot continues out through rubber grommets in the nose ribs the the jury strut where the tubing connects with the pitot tube on the front jury strut.
My question concerns the tubing used for the pitot and static lines. The existing lines seem to be soft copper tubing with rubber tubing pieces held tight with wire ties serving as connectors between tubing pieces. The tubing is 0.190" outside diameter and about 0.085" internal diameter. My question is: What type of tubing was used on the original BC12-D? Is the soft copper original? What would be the best (approved!) tubing to be used today?
Any comments or suggestions are welcome, and any reference to real approved data will be met with shouts of glee!
Thanks loads in advance.
Skip Egdorf
TF #895
BC12D-4-85 N34237
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