10 May 2025, 19:35 [ UTC - 5; DST ]
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Post subject: Spa Day Induced Alternator Failure Posted: 23 Jun 2020, 16:38 |
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Joined: 08/10/12 Posts: 328 Post Likes: +263 Location: KTKV KBKV
Aircraft: C23
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Dropped my wife and 3 of her friends off 45 minutes from our place to spend the night at a spa. On descent on my return to home base my right alternator light flickered a few times, the left alternator amps started fluctuating and the autopilot disconnected. The right ALT light never illuminated again but the amp meter showed zero amps. I couldn’t get it to reset. I was VMC so no big deal. I just replaced this alternator 5 hours ago so I thought what the heck? It’s new. Attachment: EC3055AD-9F69-4683-98EA-A654766B4F31.jpeg Guessing that was an impressive arc going on in there for a few seconds. The stud-end inside the alternator failed. Infant mortality. Poor quality control at Hartzell strikes again. I’m guessing the warranty doesn’t cover labor. Grateful there wasn’t a source of fuel near the arcing alternator. The spa trip just cost me some more AMUs! Kirk
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Post subject: Re: Spa Day Induced Alternator Failure Posted: 23 Jun 2020, 23:12 |
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Joined: 01/18/12 Posts: 84 Post Likes: +52
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Have your mechanic complete FAA form Malfunction and Defect report documenting the failure. This gets the early failure into the FAA tracking system and enough similar failures warrants FAA investigation. Username Protected wrote: Dropped my wife and 3 of her friends off 45 minutes from our place to spend the night at a spa. On descent on my return to home base my right alternator light flickered a few times, the left alternator amps started fluctuating and the autopilot disconnected. The right ALT light never illuminated again but the amp meter showed zero amps. I couldn’t get it to reset. I was VMC so no big deal. I just replaced this alternator 5 hours ago so I thought what the heck? It’s new. Attachment: EC3055AD-9F69-4683-98EA-A654766B4F31.jpeg Guessing that was an impressive arc going on in there for a few seconds. The stud-end inside the alternator failed. Infant mortality. Poor quality control at Hartzell strikes again. I’m guessing the warranty doesn’t cover labor. Grateful there wasn’t a source of fuel near the arcing alternator. The spa trip just cost me some more AMUs! Kirk
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Post subject: Re: Spa Day Induced Alternator Failure Posted: 24 Jun 2020, 01:09 |
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Joined: 06/17/14 Posts: 5856 Post Likes: +2629 Location: KJYO
Aircraft: C-182, GA-7
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Where are they built? Ford used to build some amazing alternators for Piper years ago. They were built Ford Tough! A TriPacer that I flew had one that lasted for over 40 years!
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Post subject: Re: Spa Day Induced Alternator Failure Posted: 26 Jun 2020, 17:19 |
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Joined: 08/10/12 Posts: 328 Post Likes: +263 Location: KTKV KBKV
Aircraft: C23
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Username Protected wrote: Really hard to tell from the posted picture, but if the stud remnant in the alternator case is not loose, I'd say this was an installation failure, not an alternator failure.
Also if the stud is not loose and there is arc evidence in the perimeter of the hole in the cable end lug, I'd again lean toward installation error not alternator fault.
IE the cable was not tightend correctly, or over tightened and stripped the nut or stud. Attachment: 9FB1EC98-629F-4C3B-9D09-73BF8B074844.jpeg Here’s a better pic. Mechanic said it was definitely an internal issue. (Not the same mechanic or shop that installed it). We’ll see what Hartzell says when they see it. Kirk
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Post subject: Re: Spa Day Induced Alternator Failure Posted: 26 Jun 2020, 20:07 |
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Joined: 12/10/07 Posts: 34665 Post Likes: +13287 Location: Minneapolis, MN (KFCM)
Aircraft: 1970 Baron B55
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Username Protected wrote: Here’s a better pic. Mechanic said it was definitely an internal issue. (Not the same mechanic or shop that installed it). We’ll see what Hartzell says when they see it. Looks like an internal assembly error to me. You'd have to really wrench on the top nut to break that stud and even then it would be more likely to fracture on the outside. Is the wire lug still tightly attached to the remaining portion of the stud (under the boot)?
_________________ -lance
It's easier to fool people than to convince them that they have been fooled.
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Post subject: Re: Spa Day Induced Alternator Failure Posted: 26 Jun 2020, 21:40 |
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Joined: 08/10/12 Posts: 328 Post Likes: +263 Location: KTKV KBKV
Aircraft: C23
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Hi Lance - Yes, still attached.
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Post subject: Re: Spa Day Induced Alternator Failure Posted: 27 Jun 2020, 19:50 |
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Joined: 12/10/07 Posts: 34665 Post Likes: +13287 Location: Minneapolis, MN (KFCM)
Aircraft: 1970 Baron B55
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Username Protected wrote: Hi Lance - Yes, still attached. Then unless the stud was fractured by over torquing the outer nut (which I think is unlikely) the alternator came to you with a problem waiting to happen. From what I saw in your pictures I'd guess that the internal connection to that stud was loose enough to generate a small resistance. With resistance in the alternator output, the VR would just crank up the field current until that peaked or the alternator was putting out enough extra voltage to bring the bus up to the setpoint. 40A through a 1Ω resistance dissipates 1600 W, definitely enough to fry the stud. That would also mean the alternator was actually putting out an extra 40V but given enough RPM they will easily do that as long as the diodes survive.
_________________ -lance
It's easier to fool people than to convince them that they have been fooled.
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Post subject: Re: Spa Day Induced Alternator Failure Posted: 30 Jun 2020, 08:44 |
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Joined: 04/26/13 Posts: 21601 Post Likes: +22126 Location: Columbus , IN (KBAK)
Aircraft: 1968 Baron D55
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Username Protected wrote: The spa trip just cost me some more AMUs! Don't feel bad Kirk, those AMUs were going to be spent either way. Just be glad it didn't happen on a passenger leg.
_________________ My last name rhymes with 'geese'.
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