
The wiring in the airplane over the years is; well, let's just call it interesting. I can see why so many folks rewire their airplanes. If it doesn't end up happening by the time the airplane gets back up in the air, it will probably occur shortly thereafter. Lots of scary stuff behind the panel that's being addressed.
I am in the middle of trying to figure out the situation with the rheostat. After some calculating and digging, the Ohmite Model H 25W 100Ω that I purchased will not work well in the system. I am not confident that the rheostat that was pulled out of the airplane was the original one, nor am I confident that the rheostat that I checked on the 49 A model that's been living on the field for the last several months is either. After being told that I need to change out the original equipment 1816 bulbs, as well as do a hold host of other complicated things to the airplane to make the lights work, I called a time out and did some digging. The bulbs in the A model are all 1816s, but the rheostat was a 5W 30Ω versus some unknown wattage and presumably 50Ω one that came from our airplane. Doing some calculations, the 0-15Ω Ohmite rheostat that Aircraft Spruce sells will do the trick for the purposes of getting all of the original-style lights (plus compass light, plus radio lights) working safely and properly. First lesson learned: don't reinvent the wheel.
Next, while trying to figure out what the second wire soldered to the center terminal of the rheostat is going to, I noticed a visibly cut, original wire that had been taped up. Luckily it had the number printed on it, "C28".
Great! I'll just consult the IPC to determine the home for this wire!
WRONG.
C28 does not exist in the wiring diagram. Pulling the wire loose, I trace it through a grommet going through the main panel behind the front kick panel upholstery and running up the front of the doorpost out into never-never land. After pulling it loose from the bundle to the top of the door post, I notice it doesn't have any resistance. I flick of the wrist tugs the wire free from the bundle, and the plot thickens.
Originally, I thought that maybe I was reading the wire wrong somehow and it was "C82", which goes to the stall warning horn. The stall warning horn works, and has the original wire running to it. The airplane has never (to my knowledge) had a heated pitot tube, Kohlsman or otherwise. All of the lights have worked at annual, so not a nav light or a landing/taxi light. The wiring diagrams in the IPC appear to be very complete, often referencing optional wiring, but there are some visible jumps in wire numbers. Was this to accommodate optional equipment? Did Cessna provide labeled wire for any service kit installations? Would this be documented in any of the service kits? I have checked the A model IPC and couldn't find anything referencing that wire number...figuring that since this is a relatively early B model (S/N 20408) that perhaps it was a holdover from older wiring.
No dice. Not super critical, but I am curious.
Lastly (two-part question), there is a second (newer Tefzel) wire that is/was soldered to the center terminal of the rheostat. The only wire going to center terminal should be coming from the fuse. After pulling my hair out, my IA just walked in and mentioned that the only two wires routing from under the panel, and up the front of the doorpost on the starboard side should be to the dome light or the nav light. He told me to pull the fuse for the dome light and see if it still worked, but then back pedaled and said that since I have already unsoldered the rheostat again that it it would be difficult. I replied that by process of elimination, I would find out what that wire went to, because when I turned the master switch on, either the nav light wouldn't work, or the dome light. Dome light was the winner, but that opens up another can of worms - the dome light SHOULD be on the same fuse as the landing light and cigarette lighter. I'm not in any risk of overloading the current fuse that it's on (on the rheostat, puts it on the panel lights and (optional, not installed) Stewart-Warner heater), but should I put it back to the proper/placarded fuse? Also, since the load on the fuse with the panel lights is so small with no heater, is it safer to put a 5A fuse rather than the 15A one that's in there? If there is a problem with the panel lights, the airplane will burn up before the fuse burns. Seems like a poor decision.
Eventually, circuit breakers will be retrofitted, but that will probably not happen until a rewire occurs. We're working with what we have now, just making safer and functional.
I appreciate any leads.