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		Dave Saylor
 
 
  Joined: 11 Jan 2015 Posts: 210 Location: GILROY, CA
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				 Posted: Wed Oct 07, 2020 7:17 pm    Post subject: Breaker then pump failure | 
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				I just had the Tyco switch/breaker for my boost pump fail.  It made a bad smell, then became intermittent, then failed completely in the span of a few minutes.  I replaced it with the same make and model.
 
 2.5 flight hours later my boost pump failed.  The new breaker never tripped.  The pump just stopped running.  The pump circuit has no resistance and I get full bus voltage at the pump, even with the pump still connected.  So it's open inside.  The new switch is working fine.
 The pump is from Airflow Performance.  They're common in RVs.  The pump and the switch had almost 2000 airframe hours since installed.  I use it for take-off and landing, so the powered time is a fraction of the total time.
 The airplane had been sitting for almost a year, then flown about 15 hours in the last two weeks.
 Does anyone have an understanding of any relationship between these two failures?  They seem too similar to be completely unrelated.  My guess is that a faulty pump somehow overloaded a faulty breaker, then failed completely.  I couldn't say that I noticed any particular fuel pressure issues before the failure.  Everything was in the green.
 Thoughts?
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Thu Oct 08, 2020 8:34 am    Post subject: Breaker then pump failure | 
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				At 10:14 PM 10/7/2020, you wrote:
  I just had the Tyco switch/breaker for my boost pump fail.  It made a bad smell, then became intermittent, then failed completely in the span of a few minutes.  I replaced it with the same make and model.
 
  
    Do you still have the carcass? I'd like to have
    it . . .
 
  2.5 flight hours later my boost pump failed.  The new breaker never tripped.  The pump just stopped running.  The pump circuit has no resistance and I get full bus voltage at the pump, even with the pump still connected.  So it's open inside.  The new switch is working fine.
 
    Agreed 
   
 
  The pump is from Airflow Performance.  They're common in RVs.  The pump and the switch had almost 2000 airframe hours since installed.  I use it for take-off and landing, so the powered time is a fraction of the total time.
 
    I think that pump has a PM motor with brushes.
    It's not uncommon for such devices to suffer
    as much degradation from idle time as from
    service life. In any case, I'm betting that
    the pathway through the armature is open for
    reasons we do not yet know. Does the pump
    have a 'cure' value? If not, I'd be pleased
    to do a autopsy on it too.
 
  The airplane had been sitting for almost a year, then flown about 15 hours in the last two weeks.
 
  
  Does anyone have an understanding of any relationship between these two failures?  They seem too similar to be completely unrelated.  My guess is that a faulty pump somehow overloaded a faulty breaker, then failed completely.  I couldn't say that I noticed any particular fuel pressure issues before the failure.  Everything was in the green.
 
  Thoughts?
 
    I suspect they are not related. In theory, you
    can't damage a breaker by 'overloading' it . . . after
    all, its core mission in life is to protect from
    the consequences of such conditions including self
    destruction. Getting a look at the carcasses might
    offer more clues.
 
  
  
    Bob . . .
 
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		ceengland7(at)gmail.com Guest
 
 
 
 
 
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				 Posted: Thu Oct 08, 2020 9:05 am    Post subject: Breaker then pump failure | 
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				On Thu, Oct 8, 2020 at 11:42 AM Robert L. Nuckolls, III <nuckolls.bob(at)aeroelectric.com (nuckolls.bob(at)aeroelectric.com)> wrote:
 
  	  | Quote: | 	 		    At 10:14 PM 10/7/2020, you wrote:
  snipped .
 
  2.5 flight hours later my boost pump failed.  The new breaker never tripped.  The pump just stopped running.  The pump circuit has no resistance and I get full bus voltage at the pump, even with the pump still connected.  So it's open inside.  The new switch is working fine.
 
    Agreed 
   
 
  The pump is from Airflow Performance.  They're common in RVs.  The pump and the switch had almost 2000 airframe hours since installed.  I use it for take-off and landing, so the powered time is a fraction of the total time.
 
    I think that pump has a PM motor with brushes.
    It's not uncommon for such devices to suffer
    as much degradation from idle time as from
    service life. In any case, I'm betting that
    the pathway through the armature is open for
    reasons we do not yet know. Does the pump
    have a 'cure' value? If not, I'd be pleased
    to do a autopsy on it too.
 
  The airplane had been sitting for almost a year, then flown about 15 hours in the last two weeks.
 
  
  Does anyone have an understanding of any relationship between these two failures?  They seem too similar to be completely unrelated.  My guess is that a faulty pump somehow overloaded a faulty breaker, then failed completely.  I couldn't say that I noticed any particular fuel pressure issues before the failure.  Everything was in the green.
 
  Thoughts?
 
    I suspect they are not related. In theory, you
    can't damage a breaker by 'overloading' it . . . after
    all, its core mission in life is to protect from
    the consequences of such conditions including self
    destruction. Getting a look at the carcasses might
    offer more clues.
 
  
  
    Bob . . .
  | 	  The core pump in the AFP pumps I'm familiar with are Airtex brand in-line fuel injection pumps, available online for between $60 & $100. Like this?
 https://www.amazon.com/Airtex-E2000-Electric-Fuel-Pump/dp/B000C1KHJG/ref=sr_1_7?dchild=1&keywords=airtex+fep2000+fuel+pump&qid=1602176199&sr=8-7
 Either E2000 or FEP2000. Note that the hose barb shown on one end screws off, allowing various other adapters.
 If the OP wishes, I can measure my FEP2000 to verify dimensions. 
 
 Charlie
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Thu Oct 08, 2020 11:13 am    Post subject: Breaker then pump failure | 
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    Interesting. The specs speak to commutators and
    brushes. I also deduce that this style of pump
    is used on a lot of medium pressure EFI systems.
 
    It will be interesting to see if we can open
    Dave's dead one for a closer looksee.
 
  
  
    Bob . . .
 
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		Kellym
 
 
  Joined: 10 Jan 2006 Posts: 1706 Location: Sun Lakes AZ
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				 Posted: Thu Oct 08, 2020 3:58 pm    Post subject: Breaker then pump failure | 
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				I believe Airflow Performance with do a rebuild at reasonable price.
 Might not get the diagnosis desired, but could be cheaper than alternatives.
 
 On 10/8/2020 12:08 PM, Robert L. Nuckolls, III wrote:
  	  | Quote: | 	 		  >
 > The core pump in the AFP pumps I'm familiar with are Airtex brand 
 > in-line fuel injection pumps, available online for between $60 & $100. 
 > Like this?
 > https://www.amazon.com/Airtex-E2000-Electric-Fuel-Pump/dp/B000C1KHJG/ref=sr_1_7?dchild=1&keywords=airtex+fep2000+fuel+pump&qid=1602176199&sr=8-7 
 >
 > Either E2000 or FEP2000. Note that the hose barb shown on one end 
 > screws off, allowing various other adapters.
 > If the OP wishes, I can measure my FEP2000Â to verify dimensions.Â
 >
 > Charlie
  
     Interesting. The specs speak to commutators and
     brushes. I also deduce that this style of pump
     is used on a lot of medium pressure EFI systems.
  
     It will be interesting to see if we can open
     Dave's dead one for a closer looksee.
  
  
     Bob . . .
  
  | 	 
 
 
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		Dave Saylor
 
 
  Joined: 11 Jan 2015 Posts: 210 Location: GILROY, CA
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				 Posted: Thu Oct 08, 2020 9:18 pm    Post subject: Breaker then pump failure | 
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				Charlie wrote:
  
 
 
 Between Amazon and the Airtex web site, my pump seems most like an E8445.  There are a lot of models and I haven't ID'd it exactly.  The E2000 looks the same but it puts out almost three times the pressure that I see.
 I sent my pump assy to AFP where they replaced the pump for a little more than the Amazon price.  They did a great job, shipping back the repaired assembly within hours of receiving it.
 Bob, if I get the old pump back, I'll send it to you along with the breaker.
 BTW, I just became aware of an AD from 2008 to replace this type of CB switch in Beechcraft products.
 --Dave
 
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		Dave Saylor
 
 
  Joined: 11 Jan 2015 Posts: 210 Location: GILROY, CA
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				 Posted: Thu Oct 08, 2020 9:53 pm    Post subject: Breaker then pump failure | 
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				Bob wrote:
  	  | Quote: | 	 		    Do you still have the carcass? I'd like to have
    it . . .
  | 	  
 
 Here's a picture for now.  I broke in before I sent my initial message.  Charred remains to follow.
 I'm almost certain that the braid broke when I opened it.
 The little barbequed U spring is missing most of its legs.  I wonder if one broke off and shorted something to start the failure. 
 The switch had lost it's "snap" after it quit.
 Here's a picture from a Beech website.  These are serviceable and very similar to what I have.
 [img]cid:ii_kg1tn0im1[/img]
 
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		finn.usa(at)gmail.com Guest
 
 
 
 
 
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				 Posted: Fri Oct 09, 2020 6:22 am    Post subject: Breaker then pump failure | 
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				NO. The braid is the weak point.     
 Where it's spot welded to the contact it's hardened. As the       switch is turned on/off the braid flexes. Same as what happens       when you have a soldered flexible wire that is not supported at a       point where the wire is still flexible (after the solder       penetration).     
 It's a glaring design failure. Easily fixed by two molded pins in       the plastic housing that would provide support where braid is       again flexible. Why they haven't done that after the extensive       failure history is beyond me.     
 Do not use these switch/breakers for flight-critical items!     
 Finn     
 [img]cid:part1.DBFBFD4E.1966774E(at)gmail.com[/img]     On 10/9/2020 1:50 AM, David Saylor wrote:
       	  | Quote: | 	 		                         
          
          Bob wrote:
                      	  | Quote: | 	 		    Do you               still have the carcass? I'd like to have
                  it . . .
               | 	             
            
            Here's a picture for now.  I broke in before I sent my             initial message.  Charred remains to follow.
            
            
            I'm almost certain that the braid broke when I opened it.
            
            
            The little barbequed U spring is missing most of its             legs.  I wonder if one broke off and shorted something to             start the failure. 
            
            
            The switch had lost it's "snap" after it quit.
            
            
            Here's a picture from a Beech website.  These are             serviceable and very similar to what I have.
            
            
                         
              
            
          
        
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      	           		Virus-free. www.avast.com 		 	 [url=#DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2] [/url]
 
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		Ceengland
 
 
  Joined: 11 Oct 2020 Posts: 394 Location: MS
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				 Posted: Mon Oct 12, 2020 5:44 am    Post subject: Breaker then pump failure | 
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				On Fri, Oct 9, 2020 at 12:24 AM David Saylor <saylor.dave(at)gmail.com (saylor.dave(at)gmail.com)> wrote:
 
  	  | Quote: | 	 		  Charlie wrote:
  
 
 
 Between Amazon and the Airtex web site, my pump seems most like an E8445.  There are a lot of models and I haven't ID'd it exactly.  The E2000 looks the same but it puts out almost three times the pressure that I see.
 I sent my pump assy to AFP where they replaced the pump for a little more than the Amazon price.  They did a great job, shipping back the repaired assembly within hours of receiving it.
 Bob, if I get the old pump back, I'll send it to you along with the breaker.
 BTW, I just became aware of an AD from 2008 to replace this type of CB switch in Beechcraft products.
 --Dave
 
 
  | 	  Congrats on the inexpensive repair! The reason I'd bet on the E2000 is that the E8445 appears to have a fixed hose barb output, while the E2000 has a threaded fitting on the output, allowing choice of fittings. Note that both pumps are capable of much higher pressure (and volume) than Bendix injection (or even automotive electronic injection) uses. Both types require a mechanical 'bypass' style pressure regulator to set pressure, and excess fuel is vented by the regulator. In the older cars where these pumps were used, the bypassed fuel returned to the fuel tank. With the AFP pump assembly, that extra block of metal in the assembly is the regulator and routes the bypassed fuel back to the pump inlet. In later models, the same device functions as a check valve, allowing the engine's mechanical pump to 'suck' fuel around the electric pump itself. Earlier models had a separate check valve, IIRC.
 Charlie
 
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		Kellym
 
 
  Joined: 10 Jan 2006 Posts: 1706 Location: Sun Lakes AZ
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				 Posted: Mon Oct 12, 2020 6:01 am    Post subject: Breaker then pump failure | 
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				That AD is rather controversial, in that the exact same breaker is used 
 in many other plane models and brands, but the AD was only issued 
 against specific Beech models.
 Kelly
 
 On 10/12/2020 6:37 AM, Charlie England wrote:
  	  | Quote: | 	 		       BTW, I just became aware of an AD from 2008 to replace this type of
      CB switch in Beechcraft products.
  
      --Dave
  
  | 	 
 
 
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 _________________ Kelly McMullen
 
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		Dave Saylor
 
 
  Joined: 11 Jan 2015 Posts: 210 Location: GILROY, CA
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				 Posted: Mon Oct 12, 2020 7:31 am    Post subject: Breaker then pump failure | 
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				Charlie,
 The one that came back looked identical.  Same threaded inlet, same banjo outlet, same terminals.  It's marked "Delphi FD0011".  Delphi has a store on Amazon, and the description is for a solenoid pump.
 The new one sounds much different.  I suppose it's a healthier sound now but it seems much higher pitch.
 AFP didn't send the old one back.
 --Dave
  
  	  | Quote: | 	 		  
 
 Congrats on the inexpensive repair! The reason I'd bet on the E2000 is that the E8445 appears to have a fixed hose barb output, while the E2000 has a threaded fitting on the output, allowing choice of fittings. Note that both pumps are capable of much higher pressure (and volume) than Bendix injection (or even automotive electronic injection) uses. Both types require a mechanical 'bypass' style pressure regulator to set pressure, and excess fuel is vented by the regulator. In the older cars where these pumps were used, the bypassed fuel returned to the fuel tank. With the AFP pump assembly, that extra block of metal in the assembly is the regulator and routes the bypassed fuel back to the pump inlet. In later models, the same device functions as a check valve, allowing the engine's mechanical pump to 'suck' fuel around the electric pump itself. Earlier models had a separate check valve, IIRC.
 Charlie
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		Dave Saylor
 
 
  Joined: 11 Jan 2015 Posts: 210 Location: GILROY, CA
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				 Posted: Mon Oct 12, 2020 7:32 am    Post subject: Breaker then pump failure | 
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				Very interesting Finn.  That makes a lot of sense.
 
 On Fri, Oct 9, 2020 at 7:31 AM Finn Lassen <finn.usa(at)gmail.com (finn.usa(at)gmail.com)> wrote:
 
  	  | Quote: | 	 		                     
 NO. The braid is the weak point.     
 Where it's spot welded to the contact it's hardened. As the       switch is turned on/off the braid flexes. Same as what happens       when you have a soldered flexible wire that is not supported at a       point where the wire is still flexible (after the solder       penetration).
    | 	 
 
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Mon Oct 12, 2020 8:04 am    Post subject: Breaker then pump failure | 
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				At 08:58 AM 10/12/2020, you wrote:
   	  | Quote: | 	 		  --> AeroElectric-List message posted by: Kelly McMullen <kellym(at)aviating.com>
 
  That AD is rather controversial, in that the exact same breaker is used in many other plane models and brands, but the AD was only issued against specific Beech models.
  Kelly | 	  
    I was on the team that worked that issue at Beech.
    The failure mode that started the investigation
    involved switch-breakers subject to the highest of
    ship's loads, i.e. electric prop de-ice. I know that
    same s/b was used on some Cessna models . . . but
    perhaps only on lightly loaded circuits. 
 
    Root cause is a mechanical issue. The fine strand
    jumper wire starts to loose strands due to operational
    flexing of the jumper.
 
    In the incident switches, loss of that jumper caused
    system current to flow through the spring. For the
    smaller switches, 5-10A, there is no immediate
    indication of failure. For the higher current
    applications, the spring heats up causing
    smoke from the burning of the switch's housing.
    I read that the smoke rather jetted from around
    the switch's actuator handle.
 
    Here's my library of photos and illustrations
    generated to support my task at Beech along
    with documents speaking to field responses.
 
   https://tinyurl.com/y48y93rk
 
    I worked analysis of the carcasses while others
    researched affected aircraft . . . which was
    a whole lot! There was a potential for thousands
    of aircraft and tens of thousands of switches to be
    at risk.
 
    Cessna had a similar situation as cited in documents
    offered above.
 
    This was a tough one. Existence of the insulator
    did not stop mechanical failure of the braid . . .
    it only prevents smoke generation by the heavily
    loaded switches. With the insulator in place,
    the switch simply opens up.
 
    Replacing all the at-risk switches in all fielded
    aircraft was a really BIG deal. The Bonanza Society
    and AOPA did a survey of affected aircraft owners
    and came to the conclusion that the failures
    were rare, occurrences of spring failure and
    smoke were rarer still. They opined that these
    events were very low risk and that a more relaxed
    approach to dealing with the condition was 
    warranted. The FAA agreed.
 
  
  
    Bob . . .
 
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		Ceengland
 
 
  Joined: 11 Oct 2020 Posts: 394 Location: MS
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				 Posted: Mon Oct 12, 2020 8:26 am    Post subject: Breaker then pump failure | 
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				The 1st hit I got on Amazon shows what appears to be a clone of the E2000. (Or the E2000 is a clone of the Delphi; who knows?    ) The Amazon ad says 'solenoid style'. Not sure what they mean by that, other than it's a cylindrical container like the activator solenoid on a starter motor. The pump is an electric motor, driving either a gerotor or roller-vane pump, all inside that housing. The sound is a whir or whine, right? Not a clicking sound. The low pressure Facet 'cube pumps' used as carb boost pumps make a clicking/buzzing/rattling sound; they are effectively 'solenoid' pumps.
 Just to be sure you know...Try your best to be sure that the pump gets a prime (pumps fuel) quickly when you 1st run the pump, even if you have to open the output side so it pumps into an open container. Most pumps like these will self prime, but they will only survive for a few minutes without fuel flowing through them. Configured like the AFP 'system' with the regulator bypass back to the inlet, they sometimes *won't* self-prime because they pump air in a loop around the pump instead of sucking fuel. That can kill the pump in a few minutes.
 Charlie
 On Mon, Oct 12, 2020 at 10:41 AM David Saylor <saylor.dave(at)gmail.com (saylor.dave(at)gmail.com)> wrote:
 
  	  | Quote: | 	 		  Charlie,
 The one that came back looked identical.  Same threaded inlet, same banjo outlet, same terminals.  It's marked "Delphi FD0011".  Delphi has a store on Amazon, and the description is for a solenoid pump.
 The new one sounds much different.  I suppose it's a healthier sound now but it seems much higher pitch.
 AFP didn't send the old one back.
 --Dave
  
  	  | Quote: | 	 		  
 
 Congrats on the inexpensive repair! The reason I'd bet on the E2000 is that the E8445 appears to have a fixed hose barb output, while the E2000 has a threaded fitting on the output, allowing choice of fittings. Note that both pumps are capable of much higher pressure (and volume) than Bendix injection (or even automotive electronic injection) uses. Both types require a mechanical 'bypass' style pressure regulator to set pressure, and excess fuel is vented by the regulator. In the older cars where these pumps were used, the bypassed fuel returned to the fuel tank. With the AFP pump assembly, that extra block of metal in the assembly is the regulator and routes the bypassed fuel back to the pump inlet. In later models, the same device functions as a check valve, allowing the engine's mechanical pump to 'suck' fuel around the electric pump itself. Earlier models had a separate check valve, IIRC.
 Charlie
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