Looking for any ideas to try, as I attempt to diagnose.
System Setup:
Garmin system.
Pilot and copilot pitch trim buttons on each control stick.
Buttons connect to Garmin GAD27 control unit.
GAD27 connects to a GSA28 pitch servo.
GSA28 pitch servo connects to the standard Vans-provided Ray Allen trim servo.
Scenario:
I was flying along at around 7500ft a few weekends ago, with the autopilot on, and noticed a G3X message asking me to trim nose down. That was pretty unusual, since the system is hooked into my electric elevator trim, and generally does small trim corrections by itself while cruising on AP. So I disconnected the autopilot and observed that the elevator trim was not functional. I could see that the G3X received my trim-up and trim-down commands from the stick (as it turns the trim display a different color when you press a trim button), but the control surface was not moving. Aileron trim was working fine. I didn't sense I was in any immediate danger, as it was stuck only slightly out of trim, and it wasn't running away in either direction, so I continued my flight and descended to my destination. Once I got to pattern altitude and started my pre-landing checklist, I noticed that the elevator trim was working normally again. Once on the ground I verified that it worked exactly as expected and the trim tab had correct and full range of motion.
A couple of things I ruled out:
Trim mechanism frozen? No. OAT never dropped below freezing temps.
Ground or power connection loose? No. Pitch trim power and grounds to the GAD27 unit are secure and have continuity.
Control stick trim button failure? No. The G3X display confirmed my buttons were working. Plus, the AP itself was unable to adjust the trim, regardless of button input.
Next step for me: The trim +/- signal comes from the GAD27, passes through the GSA28 servo, through two Deutsch connectors, then to the trim motor itself. I will be checking every connection for a bad crimp or other failure.
Another step, later: My pre-takeoff checklist has me verifying I am trimmed for takeoff, but it does not include testing trim function on the ground in the case that the plane is already trimmed for takeoff. I'll be adding that to the checklist.
Anything else you'd suggest trying? Preferably on the ground, as I don't intend to fly with unreliable trim control.
System Setup:
Garmin system.
Pilot and copilot pitch trim buttons on each control stick.
Buttons connect to Garmin GAD27 control unit.
GAD27 connects to a GSA28 pitch servo.
GSA28 pitch servo connects to the standard Vans-provided Ray Allen trim servo.
Scenario:
I was flying along at around 7500ft a few weekends ago, with the autopilot on, and noticed a G3X message asking me to trim nose down. That was pretty unusual, since the system is hooked into my electric elevator trim, and generally does small trim corrections by itself while cruising on AP. So I disconnected the autopilot and observed that the elevator trim was not functional. I could see that the G3X received my trim-up and trim-down commands from the stick (as it turns the trim display a different color when you press a trim button), but the control surface was not moving. Aileron trim was working fine. I didn't sense I was in any immediate danger, as it was stuck only slightly out of trim, and it wasn't running away in either direction, so I continued my flight and descended to my destination. Once I got to pattern altitude and started my pre-landing checklist, I noticed that the elevator trim was working normally again. Once on the ground I verified that it worked exactly as expected and the trim tab had correct and full range of motion.
A couple of things I ruled out:
Trim mechanism frozen? No. OAT never dropped below freezing temps.
Ground or power connection loose? No. Pitch trim power and grounds to the GAD27 unit are secure and have continuity.
Control stick trim button failure? No. The G3X display confirmed my buttons were working. Plus, the AP itself was unable to adjust the trim, regardless of button input.
Next step for me: The trim +/- signal comes from the GAD27, passes through the GSA28 servo, through two Deutsch connectors, then to the trim motor itself. I will be checking every connection for a bad crimp or other failure.
Another step, later: My pre-takeoff checklist has me verifying I am trimmed for takeoff, but it does not include testing trim function on the ground in the case that the plane is already trimmed for takeoff. I'll be adding that to the checklist.
Anything else you'd suggest trying? Preferably on the ground, as I don't intend to fly with unreliable trim control.

