I have had a persistent issue with Baro Alt after a transponder failure and subsequent repair. The aircraft is a RV-7A with a GRT HX dual EFIS, Garmin 530W, Tru-Trak 385, and GTX-345.
To begin, I experienced a complete GTX-345 transponder failure in flight this last year. This resulted in a complete loss of ADS-B In/out, and necessitated removal and factory service of the transponder by Garmin. Upon reinstallation it appeared to have no issues, with restoration of ADS-B in/out and an appropriate pressure altitude being displayed on the GTX. I did notice however that the autopilot (coupled to the 530W) was not receiving altitude guidance from the EFIS, although it would track GPS course. I don't think I connected that this would indicate a altitude source fault at the time.
I am a VFR pilot, and at that time did not realize I could verify ADS-B performance at that time with a PAPR report.
I then relocated to the aircraft a much busier Class D airport. It was noted by ATC that while ADS-B in/out performance would give my position, I was missing Baro Alt output. I then checked the PAPR report, and it demonstrated a 100% Baro Alt fault. The aircraft was due for its pitot/static check as well as transponder check. When this was conducted, faults were noted when undergoing this. On my next flight outbound, it unfortunately again demonstrated a Baro Alt fault, which could be seen on the PAPR as well the Flightaware tracing. However the Baro Alt fault corrected itself on the return flight, with an accurate altitude tracing.
I am unfortunately not the original builder of the RV, although I have done some very significant maintenance (engine removal and IRAN for a case seam oil leak, tire/brake work, baffle repairs, etc). I have not done any avionics work to it, and will admit that I have little to no familiarity with this.
In terms of troubleshooting further, my understanding is that altitude out signal is from the GRT EFIS via serial to the Tru-trak and GTX, in lieu of a stand-alone encoder. I am not really sure where to go from here in terms of next steps, although I suspect this is either an issue with the GRT or the wiring from which it provides altitude out. My home avionics shop would do the pitot/static/transponder check, but they really only work on certified aircraft and were not helpful beyond this. If not, would anyone be able to suggest an avionics shop in OH that would be able to assist with this?
To begin, I experienced a complete GTX-345 transponder failure in flight this last year. This resulted in a complete loss of ADS-B In/out, and necessitated removal and factory service of the transponder by Garmin. Upon reinstallation it appeared to have no issues, with restoration of ADS-B in/out and an appropriate pressure altitude being displayed on the GTX. I did notice however that the autopilot (coupled to the 530W) was not receiving altitude guidance from the EFIS, although it would track GPS course. I don't think I connected that this would indicate a altitude source fault at the time.
I am a VFR pilot, and at that time did not realize I could verify ADS-B performance at that time with a PAPR report.
I then relocated to the aircraft a much busier Class D airport. It was noted by ATC that while ADS-B in/out performance would give my position, I was missing Baro Alt output. I then checked the PAPR report, and it demonstrated a 100% Baro Alt fault. The aircraft was due for its pitot/static check as well as transponder check. When this was conducted, faults were noted when undergoing this. On my next flight outbound, it unfortunately again demonstrated a Baro Alt fault, which could be seen on the PAPR as well the Flightaware tracing. However the Baro Alt fault corrected itself on the return flight, with an accurate altitude tracing.
I am unfortunately not the original builder of the RV, although I have done some very significant maintenance (engine removal and IRAN for a case seam oil leak, tire/brake work, baffle repairs, etc). I have not done any avionics work to it, and will admit that I have little to no familiarity with this.
In terms of troubleshooting further, my understanding is that altitude out signal is from the GRT EFIS via serial to the Tru-trak and GTX, in lieu of a stand-alone encoder. I am not really sure where to go from here in terms of next steps, although I suspect this is either an issue with the GRT or the wiring from which it provides altitude out. My home avionics shop would do the pitot/static/transponder check, but they really only work on certified aircraft and were not helpful beyond this. If not, would anyone be able to suggest an avionics shop in OH that would be able to assist with this?