Mike applying the expanding foam to the base of the back wall of the hangar. The treated area can be seen on the left.
Mike laying out a nice bead of expanding foam along the back wall of the hangar.
After the expanding foam was applied, the shop was straightened out once again and I decided to use the big air compressor for the first time. Plugged it in, turned it on … and it barely began to turn. What? Decided to try another outlet that I know is on another circuit and the air compressor turned a little faster … but still no dice. Bummer. Scotty, I need more power!
Got to thinking about it and it is a 13 amp compressor so it takes more than a little power to get it moving. The circuit is only 12 gauge wire and the wire run goes to the breaker panel at the far end of the hangar row which wire distance is likely around an easy 200 feet. The 12 gauge wire has much more voltage loss than optimum … but one thing is certain … the air compressor will NOT be running on house power.
Guess it is time to go shopping for a small portable generator …that sucks but shy of running a #6 wire, just don’t think there is anything that can be done.
Even though my exuberance was squashed due to the anemic electrical outlets in the hangar, decided to suck it up and make something happen on the RV-12 … so moved the tail cone in close proximity behind the fuselage so the wiring to and from the tail cone could be installed, along with pulling the pitot tube through the fuselage’s center section. My method for doing this is a departure from the Van’s plans which would have the builder doing this with the side skins on … but there is a method to the madness, so to speak. The plan is to install a backup altimeter and airspeed indicator in the RV-12’s instrument panel which will require running a static air tube up to the instrument panel plus there is the angle of attack indicator tubing which needs to be run back to the tail cone. The wire grommets are getting really full and I know there is room for the trim wires and pitot tube … but just in case the static air or AOA tubing won’t fit, by having the side skins off, it will offer options for routing in case the wire grommets get maxed out.
Routing the pitot tube in through the center tunnel wire grommets.
After the pitot tube was routed, up through the center tunnel, the wire that goes to the pitch trim motor was pulled in through the wire grommets in the center tunnel.
Routing the pitch trim motor wire through the center channel wire grommets.
Finished for now the pitot tube and pitch trim motor wire successfully run through the center tunnel wire grommets.
A test piece of the static line was able to fit into the aft grommet on the fuselage which is great news … however, the center channel grommet has one more 18 gauge wire in it so it may not be a piece of cake getting it pulled in through the center tunnel. Hopefully, will give it a go tomorrow if other obligations get fulfilled in the morning.