Month: February 2025

Over the weekend I finished all of the wiring in the engine compartment, and added clamps to hold everything in position. I also modified the wiring behind the instrument panel, allowing a more direct path for the control cables, particular the prop control.

The last task remaining for engine compartment wiring is replacing the main battery wire which brings power from the battery solenoid to the V-PX. I’m upgrading from the Vans supplied #8 AWG wire to a large #6 AWG wire. I had to order new ring terminals from aircraft spruce, so I will finish that job once the terminals arrive.

Over the weekend I spent time working on the wiring around the engine. My goal was to get all of the electrical connections made this weekend, and this coming week to finish securing the wiring.

In other news, my interior arrived from Classic Aero. I didn’t unbox everything, just the seats, as I have more work to do in the cabin before it’s worth installing the interior. the seats look great, and it’ll be awesome to get it all fitted.

The wiring required finalizing routing of various wires, trimming to length, installing ring terminals, and then securing them.

Before starting, I powered up the G3X and confirmed the ignitions were deactivated. I can’t deactivate the starter switch, so I covered the push-to-start switch with a small red plastic cup and taped it into position. This is to prevent a scenario where someone accidentally bumps the start switch while the battery is turned on. This is the danger of the push-to-start switch; if the battery switch is on (as it might be for maintenance or just configuring stuff on the ground), depressing the start switch will spin the prop and cause serious injury to anyone within the prop arc. This is different from many aircraft which use a keyed ignition, requiring a fairly deliberate turning of the key through several positions before the starter will engage. Keyed systems can degrade over time and are more liable to cause an accident where the magnetos are not fully grounded. If this occurs, someone who rotates the prop by hand could cause the engine to fire, resulting in a nasty accident and potentially an unmanned aircraft with an engine running. Anyway, caution is needed.

The starter motor wiring required a little re-routing to ensure the wires ran clear of the engine block and the snorkel. I wired up the ignition switch, along with the start lamp wire which provides an input to the G3X to identify when the starter is engaged. Useful to identify a stuck-starter situation.

I connected the alternator field wire and removed the unnecessary alternator lamp wire. The Vertical Power unit will monitor the alternator and alert in the event of a failure. I added some silicone to the back side of the alternator plug to stabilize the wires.

The baggage light is connected to the battery (hot bus), bypassing the Vertical Power system, and requires an inline 3A fuse. I picked up a fuse holder from AutoZone so I can use an automotive blade-style fuse. I mounted the fuse holder between two adel clamps near the oil dipstick to make changing the fuse possible via the oil door, without having to remove the cowling, or diving under the panel somewhere.

Last night and today I worked on wiring the E-Mag electronic ignition system. The wiring was straightforward, I just followed the installation manual and connected the wires to the plugs, then installed the plugs into the magnetos. The time consuming part was routing the wires, and figuring out where to ground the mags. I ended up using the accessory pad studs as the ground, because items nearby, has easy access, and I’m not planning to install a backup alternator at this stage.

I made the ground wires, routed them, then routed the other wires (power, switch, and tach reading). Once I was happy with the wiring, I trimmed the wires, labeled them, and then installed them into the plug.

The E-Mag magneto uses electronics to time the spark, vs. just a static timing as a traditional mag does. The advantage is that the spark timing can be dynamically adjusted based on manifold pressure (which is determined by throttle position and altitude), for a more efficient fuel burn.

The original electronic magnetos needed a backup power supply to continue to operate in an electrical failure scenario. This model has a built in alternator in each magneto, so it will keep running even if all power is lost, and/or manifold pressure is lost. That makes it way simpler to install, and more reliable.

The wiring includes a power wire to power the electronics from the electrical bus, a switch wire to immobilize the unit when activated, and a complimentary tach output which serves as a tech reading for the Garmin system, then there is a ground wire for local ground to the engine block.

The two ignition switches on the panel each have an “off”, “on” and “test” position. They control the left and right magnetos independently. When “off” the switch grounds the “kill” (lt/rt mag sw) wire, which immobilizes the unit. In that condition it is still “awake” and drawing power from the electrical bus, as long as the battery switch is activated. When the ignition switch is set to “on” the kill wire is ungrounded and the ignition will fire. When set to “test”, the power wire is disconnected. The test is to ensure the unit’s internal alternator runs and provides power to the unit. One important note: the internal power has a minimum RPM setting, something around 1100 RPM, below which the internal power will not function. This has several important implications:

• The engine can’t be started without external (to the E-Mag) power.
• The “test” function before flight should be performed above 1100 RPM, ideally at 1700 RPM. The engine RPM will drop if a magneto is in “test” and RPM is below 1100. The engine will quit if both magnetos are in “test” and RPM is below 1100.
• In an emergency if the battery buss is no longer supplying electrical power, and the engine were to quit for any reason, a restart is only possible if the prop is windmilling above 1100 RPM. An example of this condition could be an alternator failure, followed by a fuel starvation event. If switching tanks were to remedy the fuel starvation, the prop needs to be >1100 RPM for the magnetos to fire.

The last few evenings I’ve been working on finalizing the wiring runs in the engine compartment. I looked at a few other aircraft blogs to get a few ideas, and ordered a few supplies. I started by working on the ignition leads and the EGT and CHT probe wiring. I switched out some of the adel clamps I had been using and went with -6 size clamps for all the ignition leads. The leads are slightly loose in this size clamp, but the -5 size is too tight. I wanted to be able to run zip ties through some of the clamps, and it’s helpful to have a little bit of play. The silicone cover on the leads sticks very well to the cushion clamps, so the -6 size seems to work well.

I also used some short (1/4 inch) lengths of rubber tube to create stand-off spacers for the wiring. Running zip ties around the wire bundles and through the tube keeps the wiring together but separated by 1/4 or 1/2 inch or so. Apparently it’s a good idea to have some spacing between the ignition wires and the other wiring runs to minimize interference.

Installing adel clamps is a pain, even with the clamping tool and using safety wire to hold the clamps shut. It’s just slow going.

It’s also slow going trying to visualize the wiring runs, and trying to figure out what wiring will go where. I had to redo work a couple of times, and can already tell I’ll be redoing things in the future. It feels like an iterative process to get everything worked out and squared away.

I’m using a fireproof abrasion protection sleeve on almost all of the wiring. This helps keep the wiring neat and tidy and I hope it will keep it cleaner. The sleeve can be slipped on around the wiring which makes it much easier to install and remove.