The rest of the hardware was installed on top of the FW liner. The manifold for the fuel tank vents was reinstalled and the tubing reconnected. New tubing was routed down to the lower cowling flange on either side of the NACA duct inlet. A fole was drilled to allow the tubing to drain below the cowling. Enough length was left to allow for the tubing to be bent into the airstream to pressurize the tanks slightly. This will be adjusted during flight testing.
The fuel and oil pressure manifold and the fuel flow meter were both mounted. The EIS coil pack was installed, but will need to be rotated to avoid a conflict with the oil filter on the engine. The grounding forest of tabs was reinstalled. The ANL fuse holder for the alternator B lead was installed.
