Final Testing


Dynamic Prop Balance

I rented a Dynavibe Classic from Viking Aircraft Engines for $200. With a few Kitplanes Articles (Propeller Balancing & Good Vibes) and some video help – it looked like something I could handle myself. My buddy Alan also needed to do his RV-4, so we made it a team effort. The process is actually dirt simple. The system is three components. First, you have the optical sensor that is used to track the propeller RPM through a reflective sticker on one of the prop blades. There are some constraints here regarding hub distance vs RPM vs sticker size. But again, read the chart and you’re good to go. The second component is an accelerometer. This device will measure the vibration produced. And lastly you have the control unit that allows you to get the outputs of your testing. Both the optical sensor and accelerometer bold directly to the engine. Make sure the optical sensor has a good line of sight to the master blade (the one with the sticker), and make sure the accelerometer is positioned perpendicular to the plane of travel for the cylinders (straight up and down works well for our horizontally opposed Lycomings) and as far forward as possible. Now decide on your target RPM. Your best options are cruise or take off RPMs. I chose to balance at 2500 RPM. Now run up your plane, average out the values, and see where you are at.

Run one for me showed a value of 0.21 IPS at 352°, which as starting points go, is pretty good! Now, here is the only thing that you have to keep straight in your head. First, the degrees given is where the HEAVY side is. In other words, to balance the system you need to add 180° from the value given. Second. The degrees stated are from the master prop (one with the sticker) IN THE DIRECTION OF TRAVEL. If you remember DIRECTION OF TRAVEL – its easy to remember what way you are looking both from the back or the front of the prop!

Adding weight with the standard Lycoming flywheel is easy. There are a number of holes all the way around, that enable the easy addition of weight. It took a couple more runs to fine tune. The second run gave a value of 0.16 IPS @ 121°. Basically we had a little too much weight, and were slightly off on the location. Run three, we moved that bolt one location over in the direction of the light side and got a value of 0.07 IPS @ 92°. Now we just removed a little weight and the final run gave a value of 0.01 IPS @ 146°. Anything under 0.07 is considered excellent, and 0.01 is awesome! Very happy with the results.

My buddy Curtis stopped by the hangar as we finished doing the balance to tell us “Oh, I have a DynaVibe classic you could have used for free!” Thanks Curtis for the timely announcement! 😀

We also balanced the wooden fixed pitch prop on Alan’s RV-4. As we had already done my prop, we were quite quick in doing his. His values started out at 0.61 IPS 29°.  After 3 runs, and three bolts, we arrived at a 0.05 IPS @ 216 degrees. I was not able to notice a difference between my 0.21 and 0.01 – but unlike Alan I am not yet attuned to the vibrations and sounds of my engine. I speculated that Alan would be able to feel a difference between 0.61 and 0.05. Sure enough he said on the taxi back to his hangar he could notice a definite reduction in vibration. I’m curious to hear his flight observations!


ELT Testing & Data Plate Installation

Accomplished a few things tonight. First I had my data plate engraved locally, and needed to install that. I primed the area first. I used simple pop rivets to hold the data plate in place. I’m using the standard EAA data plate. It is the smallest and most discrete of the ones I could find. Here you can see where I positioned it under the horizontal stab – which seems to be the favorite location of most builders.

I had never done an ELT test yet, so I wanted to make sure that was working. At the top of the hour I ran the self test and used a hand held radio to confirm transmission. It all checked out ok. There is one gripe – currently it is not receiving GPS data via RS-232. You have to connect a diode and a resister to the test lead on the ELT in order to check this functionality. A quick review of my wiring diagram made me realize where I think my boneheaded mistake is… I believe I tied the RS-232 in at the G5… or I may have not tied it in at all. I’ll need to open that bundle up to see exactly where I placed that lead. Either way, I’m quite sure I have an extra RS-232 output on the GDU… which would be the easiest place. Regardless, I do not need GPS connection via RS-232 to be in compliance within the USA at the current time. So this project was added to my “After flying” to do list!!!


Magnetometer and AHARS Calibration

Tonight I worked to calibrate the magnetometer and the AHARS. It was rather windy when i got to the airport, and you need good GPS data to calibrate both, so i had to wait until the storms passed. First up was the AHARS calibration. This was pretty easy. Basically level the aircraft in flight attitude and let the G3x figure out pitch and roll offset. I also needed to do a vibration test on the AHARS once the engine was running. Next I did a magnetic interference test. Basically you start and turn off all the various electrical gizmos that could cause interference and manipulate the controls etc. You do this in 10 second increments. The magnetometer (which is in the left wing tip) passed the interference test.

I taxied to an open part of the airport and used my compass to ensure I was facing due north. I guess you can do the magnetometer calibration with the engine running and just taxi it. But I chose to shut down and just push the tail around. Basically all you have to do it rotate the plane 360 degrees and 30 degree segments. The display tells you what to do and when. Dirt simple. And I got a successful calibration.

Now with the aircraft warmed up, I taxied back to the hangar, tied her to my truck and did a full power run-up for the AHARS vibration test. This also passed. So now I have a fully tested and calibrated AHARS and magnetometer.  I also setup all the airspeed marking limitations tonight in the EFIS.