Brief Description: hose connections, EIS connections
Installed the clamps size 7, to hold the braided hose that connects to the manifold to take the fuel pressure there.
Installed the manifold pressure box in the compartment under the foward baggage area.
Attached the fuel hose from the fuel injector body to the spider. Considered with Dick Isherwood how to install the fuel flow sensor in that line. I later found the installation instructions that came with the fuel flow transducer that indicates that it should be installed between the mechanical fuel pump and the fuel injector body, which is inconsistent with what I have read widely elsewhere.
Realized that the fuel pressure unit that I bought from Vans and installed, will not work the the GRT EIS. I removed the one from Vans and installed the uit supplied by GRT.
Dick and I measured the runs for the AWG 2 cables for ground and the AWG 6 cable for the alternator.
It took us a while to determine where the alternator cable will terminate in the airplane.
We still don't know where, if anywhere, to install the ammeter shunt. We cannot tell where the amp guage will be....if I will have one.
