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  #1  
Unread 11-21-21, 08:41 PM
Kim Geyer Kim Geyer is offline
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Look at the connector for the voltage regulator one of the pins has 2 wires on it. One of those is the alt restart. I’ve had that connection get janked up and cause problems
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  #2  
Unread 11-21-21, 11:24 PM
Rick Erwin Rick Erwin is offline
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Thank you for the tip, Kim. I’ll check that tomorrow also.

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  #3  
Unread 11-23-21, 07:17 PM
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Learjetter Learjetter is offline
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Rick,
I found the "droids you were looking for!" :-)

Here's a photo of my ALT RESTART switch, as removed from my panel yesterday. A previous owner removed the ALT RESTART battery pack years ago, so during this recent annual, I opted to remove the switch, and will document the removal in the logbook.
Hope this helps!
-LJ

--Upon further reflection, the ALT RESTART switch is going back in the panel. Turns out, there is a no-kidding emergency checklist called TOTAL LOSS OF ELECTRICAL POWER that calls for pressing that button. I guess I'll add the battery pack back in too...but I'll be very reluctant to press that button unless the checklist calls for it (for all the reasons described in other threads).
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File Type: jpg ALT RESTART SW AND DIODES1.jpg (207.5 KB, 587 views)
File Type: jpg ALT RESTART SW AND DIODES2.jpg (205.5 KB, 559 views)

Last edited by Learjetter : 11-28-21 at 08:13 AM. Reason: added update.
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  #4  
Unread 11-25-21, 08:47 AM
Rick Erwin Rick Erwin is offline
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Quote:
Originally Posted by Learjetter View Post
Rick,
I found the "droids you were looking for!" :-)

Here's a photo of my ALT RESTART switch, as removed from my panel yesterday. A previous owner removed the ALT RESTART battery pack years ago, so during this recent annual, I opted to remove the switch, and will document the removal in the logbook.
Hope this helps!
-LJ
Learjetter, thank you for posting the pictures.

I did get access to the resistor and the diodes and checked them; they are good.

Even after bypassing the resistor, the switch, and the diodes, (by running a test wire from the dry cell batteries directly to the field terminal on the alternator) the same problem exists. As soon as the wire from the batteries touches the alternator's field terminal, the voltage drops to zero. There must be something in the alternator that's causing this behavior. BTW, the alternators work fine.

I'll tackle this problem again on Monday, and report back when I have anything significant to report.
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  #5  
Unread 11-25-21, 12:24 PM
Timcote1960 Timcote1960 is offline
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Been reading this thread with interest. I myself have never tried the alternator restart system, and feel a bit guilty about it because the POH says to test it on a regular basis. I am wondering how other 337 pilots have managed this---is it all that important? What about the high voltage and the high voltage test system? I haven't run those either, but there they are recommended, mostly as a procedure to do while aloft.

When I was taught to fly the 337, the CFI told me "Just treat it like a really big, heavy 182." While I respect the aircraft's complexity, I guess I have glossed over some of the finer point. The electrical system has been one of them.

What say---do you run these checks as prescribed in the POH? Do they work? Is it worth it?

Tim
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  #6  
Unread 11-25-21, 04:16 PM
Rick Erwin Rick Erwin is offline
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Quote:
Originally Posted by Timcote1960 View Post
What say---do you run these checks as prescribed in the POH? Do they work? Is it worth it?

Tim
Hi Tim,

In addition to your three questions to the group, I am also interested in knowing:

Has anyone here ever had the "need" to actually "use" the Alternator Restart system inflight? If so, what was your experience with the system?

*****

For reference, my airplane is a FT337GP. Same as a P337G.

There are two checks we should be performing.

1. The POH alludes to the need to do a "functional check" of the electrical system as part of the "Before Takeoff" check. While this functional check is not delineated in the "Before Takeoff" checklist (Page 4-8), it is delineated in the "Before Takeoff-Amplified Procedures" (Page 4-15). I suppose the obvious place for this functional check to occur would be at item (6).d. "Alternators -- CHECK", in the "Before Takeoff" checklist.

2. The POH, on Page 7-44, indicates that every 25 hours we should be accomplishing an operational check of the "Alternator Restart" system. This check is to be accomplished during Day-VFR-Cruise flight, with a heavy load on the electrical system.

During each of these two checks, the ENTIRE electrical system of the aircraft will be shutdown. Personally, I'd rather not do this in-flight, ... even if it is Day-VFR.

I am more inclined to start the engines, accomplish the functional check, and ... if due - load up the electrical system (without avionics), accomplish the "Alternator Restart" check, unload the electrical system ... then, turn on the avionics, and get going.

Does anybody here care to answer Tim's three, and my two, questions?

Rick
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  #7  
Unread 11-25-21, 07:16 PM
edasmus edasmus is offline
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My experience with this is limited but here it is. My plane has had overvoltage situations occur over the years and the system worked as designed in my case. I wrote a long post on this years ago and I'm sure it's somewhere on this site.

It has long since been resolved and the condition does not occur anymore but it took awhile to find the culprit of what was causing the overvoltage condition. It was a short in the circuit breaker box to the left of the pilot's knee. The main large thick wire that provides power to the the buss bar vibrated and wore a small hole through the plastic insulator box and allowed intermittent contact with the skin of the aircraft and caused arcing. It actually burned a small hole in the skin of the aircraft.

Anyway, voltage would exceed the limit (which I think is about 32.5 volts if memory serves) and the overvoltage sensor would trip the alternators offline. Turning everything off and then turning the master switch off for a few seconds and then turning the master back on would reset the overvoltage sensor. Turning the alternators back on and then the remainder of the electrical system and I'd be back in business until the next time it happened (which might be months later).

Anyway, occasionally turning the alternator switches back on after resetting the master switch would not bring the alternators back on line. A press of the alternator restart button would solve that.

Anyway, my alternator restart batteries get replaced at every annual inspection and realistically I test each system about once, maybe twice a year. I figure that's good enough for me. If my alternators quit for any reason, (which they never have once this aforementioned problem was resolved), I'll attempt to get them back online. If that fails, I'm unloading the electrical system, putting the gear down, and then deciding how long I care to fly without the electrical system. I fly day VFR so as long as the gear is down, not having the electrical system isn't a serious problem. You serious instrument pilot's obviously have more at stake.

It's kind of pain to test the overvoltage system which is why I do not do it all that often. If one is to test it, make it the very first thing you do after starting the engines and bringing the alternators on line. I would strongly suggest keeping all avionics out of the equation. They shouldn't "feel" anything which is the point of the entire system but no sense injuring your avionics while finding out the over voltage protection didn't work as designed. I share Rick's sentiment as I test this on the ground.

Further opinions appreciated. Interesting thread. Thanks for starting it Rick.

BTW Rick, I've been on the waiting list at Bowman KLOU for about 5 months now. Hoping for a hangar there by next year sometime.

Last edited by edasmus : 11-25-21 at 07:24 PM.
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  #8  
Unread 11-26-21, 09:15 AM
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Quote:
Originally Posted by Timcote1960 View Post
What say---do you run these checks as prescribed in the POH? Do they work? Is it worth it?
Tim, I’m a nerd and do all the tests, I can’t do the ALT restart as the system was removed at some point in the past and was not documented. The button is on the panel and with the panel upgrade this coming year, the restart kit is going back in. Years ago, while flying patrol in the 337, I actually used the button to restart the electrical system where other attempts failed.

I do the electrical system ops test on every flight after both engines are started, before the radio master switch is turned on. It looks at some very important stuff and takes seconds once you have done it a couple of times. The test actually caught one of the warning lights being out, one flight it was good, the next not. Individual lights are not replaced, the unit is pulled out and a new one is put in.
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File Type: png 2EADD57A-1809-4C86-9C49-2E21A04B6E8A.png (271.9 KB, 447 views)
File Type: png 0ECA7018-A5F9-4F9C-A972-4725C3800D6B.png (271.5 KB, 445 views)
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  #9  
Unread 11-26-21, 01:09 PM
edasmus edasmus is offline
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Thanks for all the info Rick...
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  #10  
Unread 11-25-21, 08:36 AM
Rick Erwin Rick Erwin is offline
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Quote:
Originally Posted by Kim Geyer View Post
Look at the connector for the voltage regulator one of the pins has 2 wires on it. One of those is the alt restart. I’ve had that connection get janked up and cause problems
Kim,

I looked at those Molex connectors, and one of the field connections did need some rehab, but unfortunately that wasn't the source of the problem. Thank you for leading me to look there though!
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