Hi All,
I'm in the process of wiring my panel and all was going well until today. I had planned on having a trim reverse switch on my panel in case of trim runaway to bring the trim back in to a neutral position to ease stick forces. The idea is if the trim is running away, just reverse it towards neutral and then switch it off.
I have a Ray Allen trim motor wired into a GSA 28 AP server for auto-trim. From the servo it goes to the GAD 27 J272 pins 11 & 12 (manual calls these 'Pitch Trim Out 1&2').
From the GAD 27 (J272 pins 1 & 2) it goes to a DPDT ON-OFF-(ON) switch and then from the switch it goes to the Circuit breaker and ground.
So the overall connections are like this...
Battery -> Circuit Breaker -> Trim Rev Switch -> GAD 27 -> GSA 28 AutoPilot Pitch Servo -> RA Trim Servo
The switch is wired as follows:
Pin 1 +12v from CB
Pin 4 Ground
Pin 2 & 5 output to GAD 27
Pin 3 is connected to Pin 4 above
Pin 6 is connected to Pin 1 above
With the J272 connector disconnected from the GAD and testing with a multi meter the trim switch works a dream. I can connect the meter to pins 1 & 2 (trim input) of the J272 plug and the voltage from the circuit breaker reverses as expected when the switch is moved from the ON to the momentary ON position.
However, when the connector is attached to the GAD 27 the trim works perfectly only in the ON position. As soon as it is moved to the momentary position the Circuit Breaker trips.
To rule out the CB I hooked up an inline fuse and that pops in the same test so that confirms the breaker is working correctly.
I have already set a 1 second maximum trim run time in the G3X settings. So, this switch is really a final line of defence.
Does anyone else have a trim reverse switch in their GAD 27 system and seen a similar issue?
If this is a bad idea, I can obviously remove the switch, but is there a way to reverse the trim from the PFD during flight?
Or, is there another reason why this is tripping the CB that I might have missed at all?
Thank you in advance for any help or suggestions.
Abe
I'm in the process of wiring my panel and all was going well until today. I had planned on having a trim reverse switch on my panel in case of trim runaway to bring the trim back in to a neutral position to ease stick forces. The idea is if the trim is running away, just reverse it towards neutral and then switch it off.
I have a Ray Allen trim motor wired into a GSA 28 AP server for auto-trim. From the servo it goes to the GAD 27 J272 pins 11 & 12 (manual calls these 'Pitch Trim Out 1&2').
From the GAD 27 (J272 pins 1 & 2) it goes to a DPDT ON-OFF-(ON) switch and then from the switch it goes to the Circuit breaker and ground.
So the overall connections are like this...
Battery -> Circuit Breaker -> Trim Rev Switch -> GAD 27 -> GSA 28 AutoPilot Pitch Servo -> RA Trim Servo
The switch is wired as follows:
Pin 1 +12v from CB
Pin 4 Ground
Pin 2 & 5 output to GAD 27
Pin 3 is connected to Pin 4 above
Pin 6 is connected to Pin 1 above
With the J272 connector disconnected from the GAD and testing with a multi meter the trim switch works a dream. I can connect the meter to pins 1 & 2 (trim input) of the J272 plug and the voltage from the circuit breaker reverses as expected when the switch is moved from the ON to the momentary ON position.
However, when the connector is attached to the GAD 27 the trim works perfectly only in the ON position. As soon as it is moved to the momentary position the Circuit Breaker trips.
To rule out the CB I hooked up an inline fuse and that pops in the same test so that confirms the breaker is working correctly.
I have already set a 1 second maximum trim run time in the G3X settings. So, this switch is really a final line of defence.
Does anyone else have a trim reverse switch in their GAD 27 system and seen a similar issue?
If this is a bad idea, I can obviously remove the switch, but is there a way to reverse the trim from the PFD during flight?
Or, is there another reason why this is tripping the CB that I might have missed at all?
Thank you in advance for any help or suggestions.
Abe
