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Dave's RV-10 Build Log
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Date:  3-13-2017
Number of Hours:  7.75
Manual Reference:  
Brief Description:  Avionics Wiring In Fuselage

Determined avionics wires to be run in conduits from panel to mid-fuselage and to right wing, from mid-fuselage to tail cone, and from panel to tail cone. Determined wire lengths required for each wire to be run in the fuselage (excluding wiring within the panel).

Installed additional wires in the right wing for the magnetometer (3 conductor shielded and a 2 conductor shielded cable), and for the outside air temperature (OAT) probe (3 conductor shielded) to be installed near the second inspection hatch from the wing root.

Looked at options for mounting the flap position transmitter. Will most likely install it at the right wing root on the outside of the fuselage, connected to the flap actuator arm.

Sanded one side of the cabin top front and placed Icing to smooth out the surface. After allowing about an hour to cure, started sanding the icing to get the shape and form desired.
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