Today's Message Index:
----------------------
 
     1. 12:40 AM - You'll Cry Pip Pins (Tony Renshaw)
     2. 12:57 AM - Re: You'll Cry Pip Pins (David Joyce)
     3. 01:07 AM - Re: You'll Cry Pip Pins (Frans Veldman)
     4. 01:27 AM - Scottish trip - advice? (gtagr)
     5. 02:42 AM - Re: You'll Cry Pip Pins (GRAHAM SINGLETON)
     6. 02:56 AM - Re: You'll Cry Pip Pins (Bob Harrison)
     7. 03:08 AM - Re: Scottish trip - advice? (Bob Harrison)
     8. 06:45 AM - Re: You'll Cry Pip Pins (William Daniell)
     9. 06:51 AM - Re: You'll Cry Pip Pins (houlihan)
    10. 06:52 AM - Re: Scottish trip - advice? (David Joyce)
    11. 06:59 AM - Spar pin (was You'll cry..) ()
    12. 08:37 AM - Re: Spar pin (was You'll cry..) (gtagr)
    13. 08:48 AM - Contact of Europa now at Wombleton .... (Bob Harrison)
    14. 08:57 AM - Re: You'll Cry Pip Pins (Pete)
    15. 08:59 AM - Re: Scottish trip - advice? (gtagr)
    16. 08:59 AM - Re: Contact of Europa now at Wombleton .... (Donald Cameron)
    17. 09:00 AM - Re: Spar pin (was You'll cry..) (Pete)
    18. 09:01 AM - Re: Re: Spar pin (was You'll cry..) (Pete)
    19. 09:03 AM - Re: Contact of Europa now at Wombleton .... (John Heykoop)
    20. 09:54 AM - Re: Re: Scottish trip - advice? (Bob Harrison)
    21. 10:02 AM - Re: You'll Cry Pip Pins (GRAHAM SINGLETON)
    22. 10:06 AM - Re: You'll Cry Pip Pins (William Daniell)
    23. 01:02 PM - Re: Scottish trip - advice? (graeme bird)
    24. 01:15 PM - Re: You'll Cry Pip Pins (GRAHAM SINGLETON)
    25. 01:48 PM - Re: You'll Cry Pip Pins (William Daniell)
    26. 03:13 PM - Re: You'll Cry Pip Pins (GRAHAM SINGLETON)
    27. 03:20 PM - Re: Contact of Europa now at Wombleton .... (Trevpond)
    28. 03:57 PM - Re: Contact of Europa now at Wombleton .... (Bob Harrison)
 
 
 
Message 1
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  | 
      
      
| Subject:  | You'll Cry Pip Pins | 
      
      
      Hi Fred and co,
      Isn't the width of the spars and seat back the depth of the shank of the pip pin?
      
      Don't have it with me to measure.
       Talking about pip pins, does anyone see any merit in using two of the Port pip
      pins, another for the Std spar too?
      
      Regards
      Tony Renshaw
      
      
      Sent from my iPad
      
      On 07/06/2013, at 4:01 PM, Europa-List Digest Server <europa-list@matronics.com>
      wrote:
      
      > 1  _____________________________________
      > 
      
      
Message 2
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| Subject:  | Re: You'll Cry Pip Pins | 
      
      
      Tony, I opted to have 2 pippinned spar pins on the logic 
      that it confines the ends of the spars both sides and 
      almost certainly improves the strength of he combination, 
      which tend to twist and depart from the straight and 
      narrow under high load. It also looks neater! Regards, 
      David Joyce, GXSDJ
      
      
      On Fri, 7 Jun 2013 16:40:13 +0900
        Tony Renshaw <tonyrenshaw268@gmail.com> wrote:
      ><tonyrenshaw268@gmail.com>
      > 
      > Hi Fred and co,
      > Isn't the width of the spars and seat back the depth of 
      >the shank of the pip pin? 
      > Don't have it with me to measure.
      > Talking about pip pins, does anyone see any merit in 
      >using two of the Port pip pins, another for the Std spar 
      >too?
      > 
      > Regards
      > Tony Renshaw
      > 
      > 
      > Sent from my iPad
      > 
      > On 07/06/2013, at 4:01 PM, Europa-List Digest Server 
      ><europa-list@matronics.com> wrote:
      > 
      >> 1  _____________________________________
      >> 
      > 
      > 
      >Un/Subscription,
      >Forums!
      >Admin.
      > 
      > 
      > 
      
      
Message 3
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  | 
      
      
| Subject:  | Re: You'll Cry Pip Pins | 
      
      
      On 06/07/2013 09:40 AM, Tony Renshaw wrote:
      
      >  Talking about pip pins, does anyone see any merit in using two of the Port pip
      pins, another for the Std spar too?
      
      If I recall correctly, there was some technical reason why both pip pins
      are different. I forgot the details, but this discussion has been held
      before and someone with insight argued why using a pip pin on the
      starboard side was not such a good idea. It had something to do with the
      different arrangement and thus different torsional loads on the
      starboard side because the spars overlay "the other way around". The pin
      had to be longer there to allow some movement, and because it needs to
      have some play a pip pin can not be used (unless you make it longer than
      it should be but then you need an additional retaining mechanism which
      of course negates the whole idea of using a pip pin in the first place.)
      
      Although I have modified my aircraft quite a lot, this is an area where
      I am shy to deviate from the build plan, as it is one of the most
      critical structural area's. As all of the other pins are pip pins my bet
      is that there must have been a reason why to use a different arrangement
      on this specific pin. Surely it can't be because it was cheaper or so,
      or the designer was short of one pip pin and decided to work around it...
      
      Regards,
      Frans
      
      
Message 4
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| Subject:  | Scottish trip - advice? | 
      
      
      Fellow Europa flyers,
      
      I'm planning to fly to Lerwick in the Shetlands and back, 6-13 July departing Wellesbourne.
      Any thoughts/advice/recommends on fuel availability/routes/accommodation
      please from those that have done a similar trip or who live in the localities?
      
      
      Clive Sutton, G-TAGR
       :)
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=402187#402187
      
      
Message 5
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| Subject:  | Re: You'll Cry Pip Pins | 
      
      Frans=0AThe pip pin on the port side is there to prevent the starboard spar
       from twisting away from the =0Aport spar under high load. The starboard si
      de has no need of retention because the overlapping =0Aspar provides that f
      unction.=0AStrictly speaking the bush in the seat back bulkhead is of no va
      lue, in fact it increases the load on the spars.=0ABe better without it as 
      per the motor glider. (but DYOR)=0AGraham=0A=0A=0A=0A=0A___________________
      _____________=0A From: Frans Veldman <frans@privatepilots.nl>=0ATo: europa-
      list@matronics.com =0ASent: Friday, 7 June 2013, 9:07=0ASubject: Re: Europa
      s Veldman <frans@privatepilots.nl>=0A=0AOn 06/07/2013 09:40 AM, Tony Rensha
      w wrote:=0A=0A>- Talking about pip pins, does anyone see any merit in usi
      ng two of the Port pip pins, another for the Std spar too?=0A=0AIf I recall
       correctly, there was some technical reason why both pip pins=0Aare differe
      nt. I forgot the details, but this discussion has been held=0Abefore and so
      meone with insight argued why using a pip pin on the=0Astarboard side was n
      ot such a good idea. It had something to do with the=0Adifferent arrangemen
      t and thus different torsional loads on the=0Astarboard side because the sp
      ars overlay "the other way around". The pin=0Ahad to be longer there to all
      ow some movement, and because it needs to=0Ahave some play a pip pin can no
      t be used (unless you make it longer than=0Ait should be but then you need 
      an additional retaining mechanism which=0Aof course negates the whole idea 
      of using a pip pin in the first place.)=0A=0AAlthough I have modified my ai
      rcraft quite a lot, this is an area where=0AI am shy to deviate from the bu
      ild plan, as it is one of the most=0Acritical structural area's. As all of 
      the other pins are pip pins my bet=0Ais that there must have been a reason 
      why to use a different arrangement=0Aon this specific pin. Surely it can't 
      be because it was cheaper or so,=0Aor the designer was short of one pip pin
      =============
      
Message 6
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  | 
      
      
| Subject:  | You'll Cry Pip Pins | 
      
      
      Hi! Frans/all.
      I used two spar pip pins from the outset since it needs remembering by a
      novice helper as to which side is which. But my suggestion is that the last
      thing I would wish is for one spar to migrate off the end of the pin . This
      whole concept was protected somewhat by the installation of the "cuff"
      encompassing both spars which came later in the development. Perhaps Neville
      will elucidate somewhat, since he does helpfully monitor this forum? It is
      my opinion that the original Europa team did decide to go for the cheap
      option. Any end play on the pip pins has been taken up by stacking washers
      under the heads of the pins when first installing the seat back bushings.
      However it is critical to ensure that the pip pins have got right "home" to
      allow their safety balls to expand.
      
      -----Original Message-----
      From: owner-europa-list-server@matronics.com
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of Frans Veldman
      Sent: 07 June 2013 09:07
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      --> <frans@privatepilots.nl>
      
      On 06/07/2013 09:40 AM, Tony Renshaw wrote:
      
      >  Talking about pip pins, does anyone see any merit in using two of the
      Port pip pins, another for the Std spar too?
      
      If I recall correctly, there was some technical reason why both pip pins are
      different. I forgot the details, but this discussion has been held before
      and someone with insight argued why using a pip pin on the starboard side
      was not such a good idea. It had something to do with the different
      arrangement and thus different torsional loads on the starboard side because
      the spars overlay "the other way around". The pin had to be longer there to
      allow some movement, and because it needs to have some play a pip pin can
      not be used (unless you make it longer than it should be but then you need
      an additional retaining mechanism which of course negates the whole idea of
      using a pip pin in the first place.)
      
      Although I have modified my aircraft quite a lot, this is an area where I am
      shy to deviate from the build plan, as it is one of the most critical
      structural area's. As all of the other pins are pip pins my bet is that
      there must have been a reason why to use a different arrangement on this
      specific pin. Surely it can't be because it was cheaper or so, or the
      designer was short of one pip pin and decided to work around it...
      
      Regards,
      Frans
      
      
Message 7
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| Subject:  | Scottish trip - advice? | 
      
      
      Hi! Clive
      I can offer a little advice in that Wick is of first class service  and
      eager to oblige. However my experience of Sumburgh if you should need to
      flight plan back was not a good one. They refused to accept a flight plan to
      Wick because it was closed on a Sunday, so it was necessary to land with a
      suspect problem with the engine!  Not unusual with the Jabiru anyway ! The
      manager at Wick went ballistic at the Sumburgh people for diverting business
      from him!
      Also there are extensive Military activities to watch out for and you are to
      be recommended to constantly speak to the Regional FIS .
      Regards
      Bob Harrison G-PTAG 
      
      -----Original Message-----
      From: owner-europa-list-server@matronics.com
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of gtagr
      Sent: 07 June 2013 09:27
      Subject: Europa-List: Scottish trip - advice?
      
      
      Fellow Europa flyers,
      
      I'm planning to fly to Lerwick in the Shetlands and back, 6-13 July
      departing Wellesbourne.  Any thoughts/advice/recommends on fuel
      availability/routes/accommodation please from those that have done a similar
      trip or who live in the localities?  
      
      Clive Sutton, G-TAGR
       :)
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=402187#402187
      
      
Message 8
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| Subject:  | You'll Cry Pip Pins | 
      
      Graham
      
      
      I am very interested by this statement ..so as I understand it the spars are
      the main load bearing structure in the airpcraft. if the seat back bush does
      not do the this what does?  How does the motorglider work?
      
      
      Will
      
      
      From: owner-europa-list-server@matronics.com
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of GRAHAM
      SINGLETON
      Sent: Friday, June 07, 2013 04:42
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      Frans
      The pip pin on the port side is there to prevent the starboard spar from
      twisting away from the 
      port spar under high load. The starboard side has no need of retention
      because the overlapping 
      spar provides that function. 
      Strictly speaking the bush in the seat back bulkhead is of no value, in fact
      it increases the load on the spars.
      Be better without it as per the motor glider. (but DYOR)
      Graham
      
      
        _____  
      
      From: Frans Veldman <frans@privatepilots.nl>
      Sent: Friday, 7 June 2013, 9:07
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      
      On 06/07/2013 09:40 AM, Tony Renshaw wrote:
      
      >  Talking about pip pins, does anyone see any merit in using two of the
      Port pip pins, another for the Std spar too?
      
      If I recall correctly, there was some technical reason why both pip pins
      are different. I forgot the details, but this discussion has been held
      before and someone with insight argued why using a pip pin on the
      starboard side was not such a good idea. It had something to do with the
      different arrangement and thus different torsional loads on the
      starboard side because the spars overlay "the other way around". The pin
      had to be longer there to allow some movement, and because it needs to
      have some play a pip pin can not be used (unless you make it longer than
      it should be but then you need an additional retaining mechanism which
      of course negates the whole idea of using a pip pin in the first place.)
      
      Although I have modified my aircraft quite a lot, this is an area where
      I am shy to deviate from the build plan, as it is one of the most
      critical structural area's. As all of the other pins are pip pins my bet
      is that there must have been a reason why to use a different arrangement
      on this specific pin. Surely it can't be because it was cheaper or so,
      or the designer was short of one pip pin and decided to wo=  -->
      http://www.matronics.com/Navigator?Europa-List
      _ref="http://forums.matronics.com/" target="_blank">http://forums.matronbsp;
      Thank you for your generous nbsp;             -Matt Dralle, List Admin.
      
      
Message 9
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  | 
      
      
| Subject:  | Re: You'll Cry Pip Pins | 
      
      Hi.
      I would guess that its the lift and drag pins on the fuselage side that "
      carries" the load.
      
      Tim
      
      
      On 7 June 2013 14:45, William Daniell <wdaniell.longport@gmail.com> wrote:
      
      > Graham****
      >
      > ** **
      >
      > I am very interested by this statement =85.so as I understand it the spar
      s
      > are the main load bearing structure in the airpcraft=85 if the seat back 
      bush
      > does not do the this what does?  How does the motorglider work?****
      >
      > ** **
      >
      > Will****
      >
      > ** **
      >
      > *From:* owner-europa-list-server@matronics.com [mailto:
      > owner-europa-list-server@matronics.com] *On Behalf Of *GRAHAM SINGLETON
      > *Sent:* Friday, June 07, 2013 04:42
      > *To:* europa-list@matronics.com
      > *Subject:* Re: Europa-List: You'll Cry Pip Pins****
      >
      > ** **
      >
      > Frans
      > The pip pin on the port side is there to prevent the starboard spar from
      > twisting away from the
      > port spar under high load. The starboard side has no need of retention
      > because the overlapping
      > spar provides that function.
      > Strictly speaking the bush in the seat back bulkhead is of no value, in
      > fact it increases the load on the spars.
      > Be better without it as per the motor glider. (but DYOR)
      > Graham****
      >
      > ** **
      >
      > ** **
      > ------------------------------
      >
      > *From:* Frans Veldman <frans@privatepilots.nl>
      > *To:* europa-list@matronics.com
      > *Sent:* Friday, 7 June 2013, 9:07
      > *Subject:* Re: Europa-List: You'll Cry Pip Pins****
      >
      >
      >
      > On 06/07/2013 09:40 AM, Tony Renshaw wrote:
      >
      > >  Talking about pip pins, does anyone see any merit in using two of the
      > Port pip pins, another for the Std spar too?
      >
      > If I recall correctly, there was some technical reason why both pip pins
      > are different. I forgot the details, but this discussion has been held
      > before and someone with insight argued why using a pip pin on the
      > starboard side was not such a good idea. It had something to do with the
      > different arrangement and thus different torsional loads on the
      > starboard side because the spars overlay "the other way around". The pin
      > had to be longer there to allow some movement, and because it needs to
      > have some play a pip pin can not be used (unless you make it longer than
      > it should be but then you need an additional retaining mechanism which
      > of course negates the whole idea of using a pip pin in the first place.)
      >
      > Although I have modified my aircraft quite a lot, this is an area where
      > I am shy to deviate from the build plan, as it is one of the most
      > critical structural area's. As all of the other pins are pip pins my bet
      > is that there must have been a reason why to use a different arrangement
      > on this specific pin. Surely it can't be because it was cheaper or so,
      > or the designer was short of one pip pin and decided to wo=  -->
      > http://www.matronics.com/Navigator?Europa-List
      > _ref="http://forums.matronics.com/" target="_blank">
      > http://forums.matronbsp; Thank you for your generous nbsp;
      > -Matt Dralle, List Admin.*
      >
      >
      > *
      >
      > * *
      >
      > * *
      >
      > **
      >
      > **
      >
      > **
      >
      > **
      >
      > **
      >
      > *http://www.matronics.com/Navigator?Europa-List*
      >
      > *<           - MATRONICS WEB FORUMS -*
      >
      > **
      >
      > *http://forums.matronics.com*
      >
      > **
      >
      > **
      >
      > **
      >
      > **
      >
      > *http://www.matronics.com/contribution*
      >
      > **
      >
      > * *
      >
      > *
      >
      ===========
      ===========
      ===========
      ===========
      > *
      >
      >
      
Message 10
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  | 
      
      
| Subject:  | Re: Scottish trip - advice? | 
      
      
      Clive, There is a nice hotel about 3/4 mile from the 
      airport and a friendly local taxi driver. The admin guy at 
      Lerwick was also very friendly and helpful. Regards, David 
      Joyce, G-XSDJ
      
      On Fri,  7 Jun 2013 01:27:03 -0700
        "gtagr" <clive.maf@googlemail.com> wrote:
      ><clive.maf@googlemail.com>
      > 
      >Fellow Europa flyers,
      > 
      > I'm planning to fly to Lerwick in the Shetlands and 
      >back, 6-13 July departing Wellesbourne.  Any 
      >thoughts/advice/recommends on fuel 
      >availability/routes/accommodation please from those that 
      >have done a similar trip or who live in the localities?  
      > 
      > Clive Sutton, G-TAGR
      > :)
      > 
      > 
      > 
      > 
      > Read this topic online here:
      > 
      > http://forums.matronics.com/viewtopic.php?p=402187#402187
      > 
      > 
      > 
      > 
      > 
      > 
      > 
      >Un/Subscription,
      >Forums!
      >Admin.
      > 
      > 
      > 
      
      
Message 11
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  | 
      
      
| Subject:  | Spar pin (was You'll cry..) | 
      
      Fred,
      
                  Wow, you hit a note there, that lines up with what I've come to
      believe. By leaning 'way back from the belly panel opening, I can see the
      pintle and believe that an extended hacksaw blade of about 30 inches would
      rest on it and begin sawing. The blade is attached to a speed-controlled
      scroll saw so we can start slowly and establish an early cut to follow. The
      route would be the same, near the back of the panel hole, up behind the
      pitch tube and behind the aileron bracket. I mean to guide it with the
      boroscope, with a buddy who has taken an interest at the hangar.
      
                  Due to a combination of lassitude and ignorance, I can't seem to
      achieve the Matronics graphic skills for a photo, but will send it directly.
      
      Cheers, Ferg
      
      
      Ferg...there is a space of 1.75" (45mm) between the face of my tank and 
      
      the aft edge of the 0.5" rod which connects to the aileron friction 
      
      plate. I'm suggesting that this gap would allow ample space for a 
      
      reciprocating saw blade of proper length to saw your pintle from 
      
      below...the trick will be to establish some reference points so that the 
      
      opening for the saw can be determined with some accuracy.
      
      
      My suggestion would be to use a hole saw to cut a hole in the bottom of 
      
      the fuselage...say about 2" in diameter...if you make hatch marks for 
      
      the center point extending beyond the circumference of the circle, they 
      
      would make it easy to align the cut-out circle when you go to patch it 
      
      in once the problem's solved and your wings are off.
      
      
      To locate the center point of your hole, perhaps starting from a 
      
      reference line drawn between the two fuel tank access holes would 
      
      do...?...if this sounds like a sensible approach to you (and to others 
      
      lurking on the list), I can give you a dimension fore and aft from that 
      
      line, and a second dimension off the centerline of the fuselage 
      
      bottom to locate the center point for the hole.
      
      
      Let me know if you would like me to determine those dimensions and 
      
      establish that point.
      
      
      My suggestions are based on the idea that a solution lies in finding a 
      
      way to cut off your "tapered pintle" which will then allow for you to 
      
      drive out the remaining portion which is now stuck in the spar holes.
      
      
      But perhaps more experienced minds can find a better alternative.
      
      
      Fred
      
      
Message 12
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  | 
      
      
| Subject:  | Re: Spar pin (was You'll cry..) | 
      
      
      Gentlemen, if I may offer a late suggestion, a wire saw might bring something - here's a link: http://www.amazon.co.uk/Commando-Stainless-Steel-Cutter-Strong/dp/B000O6EL50
      
      These things have the advantage of not requiring a 'reciprocating gap' beyond the
      item being cut, and possibly quite a small entry and exit slot in the belly
      - though you'd need to thread it over the item to be cut somehow of course. 
      I'm sure the handle rings could be detached somehow to make this 'threading' operation
      easier . . .
      
      Like BCB's other products, worth carrying in the aircraft in a survival kit too.
      
      Clive. :)
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=402210#402210
      
      
Message 13
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  | 
      
      
| Subject:  | Contact of Europa now at Wombleton .... | 
      
      Hi! All you clever administrators ....
      
      Having been out of circulation in the Arctic recently  I noticed a message
      come through about Europa Spares moving out to Wombleton .  Does anyone who
      files such useful info have a new contact number I can get through to them
      please?
      
      Regards
      
      Bob H 
      
      
Message 14
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  | 
      
      
| Subject:  | Re: You'll Cry Pip Pins | 
      
      All the lifting loads are taken by the lift pins on the side of the fuse. Th
      e pip pins function only to tie the spars together and keep the wings from f
      olding up under G.
      
      The geometry is such that when the main spars are flexing under load, the pi
      p pin locations on the spars move downward relative to the lift pins at the s
      ide of the fuse (as the lift pins are further out along the radius of the fl
      exing spars), so the net result is that the pip pins actually push DOWNWARDS
       on the seat back under high positive G's.....totally counter productive.  T
      he seat back bushes should be clearance vertically IMHO to avoid this situat
      ion.
      
      The seat back bushes may however provide some (weak?) support in keeping the
       pip pins from twisting out of the spars under their asymmetrical twisting l
      oad.  Many gliders use fork-spar arrangements to avoid this.
      
      Cheers,
      Pete
      A239
      
      On Jun 7, 2013, at 9:45 AM, "William Daniell" <wdaniell.longport@gmail.com> w
      rote:
      
      > Graham
      >  
      > I am very interested by this statement .so as I understand it the
       spars are the main load bearing structure in the airpcraft if the s
      eat back bush does not do the this what does?  How does the motorglider work
      ?
      >  
      > Will
      >  
      > From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-ser
      ver@matronics.com] On Behalf Of GRAHAM SINGLETON
      > Sent: Friday, June 07, 2013 04:42
      > To: europa-list@matronics.com
      > Subject: Re: Europa-List: You'll Cry Pip Pins
      >  
      > Frans
      > The pip pin on the port side is there to prevent the starboard spar from t
      wisting away from the 
      > port spar under high load. The starboard side has no need of retention bec
      ause the overlapping 
      > spar provides that function. 
      > Strictly speaking the bush in the seat back bulkhead is of no value, in fa
      ct it increases the load on the spars.
      > Be better without it as per the motor glider. (but DYOR)
      > Graham
      >  
      >  
      > From: Frans Veldman <frans@privatepilots.nl>
      > To: europa-list@matronics.com 
      > Sent: Friday, 7 June 2013, 9:07
      > Subject: Re: Europa-List: You'll Cry Pip Pins
      > 
      > 
      > On 06/07/2013 09:40 AM, Tony Renshaw wrote:
      > 
      > >  Talking about pip pins, does anyone see any merit in using two of the P
      ort pip pins, another for the Std spar too?
      > 
      > If I recall correctly, there was some technical reason why both pip pins
      > are different. I forgot the details, but this discussion has been held
      > before and someone with insight argued why using a pip pin on the
      > starboard side was not such a good idea. It had something to do with the
      > different arrangement and thus different torsional loads on the
      > starboard side because the spars overlay "the other way around". The pin
      > had to be longer there to allow some movement, and because it needs to
      > have some play a pip pin can not be used (unless you make it longer than
      > it should be but then you need an additional retaining mechanism which
      > of course negates the whole idea of using a pip pin in the first place.)
      > 
      > Although I have modified my aircraft quite a lot, this is an area where
      > I am shy to deviate from the build plan, as it is one of the most
      > critical structural area's. As all of the other pins are pip pins my bet
      > is that there must have been a reason why to use a different arrangement
      > on this specific pin. Surely it can't be because it was cheaper or so,
      > or the designer was short of one pip pin and decided to wo=  --> http://
      www.matronics.com/Navigator?Europa-List
      > _ref="http://forums.matronics.com/" target="_blank">http://forums.matr
      onbsp; Thank you for your generous nbsp;             -Matt Dralle, List Admi
      n.
      > 
      > 
      > 
      > 
      > 
      >  
      >  
      > http://www.matronics.com/Navigator?Europa-List
      > <           - MATRONICS WEB FORUMS -
      > http://forums.matronics.com
      > http://www.matronics.com/contribution
      >  
      > 
      > 
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      > 
      
Message 15
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  | 
      
      
| Subject:  | Re: Scottish trip - advice? | 
      
      
      Thanks for the suggestions.  By way of a bit more detail to comment upon, my outline
      route at the moment is:
      
      Day 1: Wellesbourne to Fishburn.
      Day 2: Fishburn to Cumbernauld (an uncle lives nearby)
      Day 3: Cumbernauld to Wick via Aberdeen with the direct water crossing
      Day 4: Wick to Lerwick, overflying Kirkwall, Sanday, FairIsle and Sumburgh
      Day 5: Stay local to Lerwick, possibly fly around/to Fetlar and around Out Stack
      Day 6: Return to Inverness via Wick
      Day 7: Inverness to Islay
      Day 8: Islay to EGBW via Carlisle
      
      Further thoughts?
      
      
      Clive.
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=402218#402218
      
      
Message 16
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  | 
      
      
| Subject:  | Re: Contact of Europa now at Wombleton .... | 
      
      Hi 
      
      I believe the temporary contact details are as follow 01751 432 356 
      
      Or via email: 
      info@europa-aircraft.co.uk
      
      Hope these work as I got this from the news page on europa website. 
      
      Kind regards
      Donald
      
      
      Sent from my iPhone
      
      On 7 Jun 2013, at 16:46, "Bob Harrison" <ptag.dev@talktalk.net> wrote:
      
      > Hi! All you clever administrators ....
      > Having been out of circulation in the Arctic recently  I noticed a message
       come through about Europa Spares moving out to Wombleton .  Does anyone who
       files such useful info have a new contact number I can get through to them p
      lease?
      > Regards
      > Bob H
      > 
      > 
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      > 
      
Message 17
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  | 
      
      
| Subject:  | Re: Spar pin (was You'll cry..) | 
      
      No idea if this is of any value or not, but might a campers thin "rope saw" m
      ay be of use to get into a tight space? I guess threading it would be diffic
      ult tho.
      
      
      On Jun 7, 2013, at 10:02 AM, <f.kyle@sympatico.ca> wrote:
      
      > Fred,
      >             Wow, you hit a note there, that lines up with what I=99v
      e come to believe. By leaning =98way back from the belly panel opening
      , I can see the pintle and believe that an extended hacksaw blade of about 3
      0 inches would rest on it and begin sawing. The blade is attached to a speed
      -controlled scroll saw so we can start slowly and establish an early cut to f
      ollow. The route would be the same, near the back of the panel hole, up behi
      nd the pitch tube and behind the aileron bracket. I mean to guide it with th
      e boroscope, with a buddy who has taken an interest at the hangar.
      >             Due to a combination of lassitude and ignorance, I can=99
      t seem to achieve the Matronics graphic skills for a photo, but will send it
       directly.
      > Cheers, Ferg
      >  
      > Ferg...there is a space of 1.75" (45mm) between the face of my tank and
      > the aft edge of the 0.5" rod which connects to the aileron friction
      > plate. I'm suggesting that this gap would allow ample space for a
      > reciprocating saw blade of proper length to saw your pintle from
      > below...the trick will be to establish some reference points so that the
      > opening for the saw can be determined with some accuracy.
      >  
      > My suggestion would be to use a hole saw to cut a hole in the bottom of
      > the fuselage...say about 2" in diameter...if you make hatch marks for
      > the center point extending beyond the circumference of the circle, they
      > would make it easy to align the cut-out circle when you go to patch it
      > in once the problem's solved and your wings are off.
      >  
      > To locate the center point of your hole, perhaps starting from a
      > reference line drawn between the two fuel tank access holes would
      > do...?...if this sounds like a sensible approach to you (and to others
      > lurking on the list), I can give you a dimension fore and aft from that
      > line, and a second dimension off the centerline of the fuselage
      > bottom to locate the center point for the hole.
      >  
      > Let me know if you would like me to determine those dimensions and
      > establish that point.
      >  
      > My suggestions are based on the idea that a solution lies in finding a
      > way to cut off your "tapered pintle" which will then allow for you to
      > drive out the remaining portion which is now stuck in the spar holes.
      >  
      > But perhaps more experienced minds can find a better alternative.
      >  
      > Fred
      >  
      > 
      > 
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      > 
      
Message 18
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  | 
      
      
| Subject:  | Re: Spar pin (was You'll cry..) | 
      
      
      Oops.....collision, apologies for my duplicate post...
      
      Cheers,
      Pete
      
      On Jun 7, 2013, at 11:35 AM, "gtagr" <clive.maf@googlemail.com> wrote:
      
      > 
      > Gentlemen, if I may offer a late suggestion, a wire saw might bring something - here's a link: http://www.amazon.co.uk/Commando-Stainless-Steel-Cutter-Strong/dp/B000O6EL50
      > 
      > These things have the advantage of not requiring a 'reciprocating gap' beyond
      the item being cut, and possibly quite a small entry and exit slot in the belly
      - though you'd need to thread it over the item to be cut somehow of course.
      I'm sure the handle rings could be detached somehow to make this 'threading'
      operation easier . . .
      > 
      > Like BCB's other products, worth carrying in the aircraft in a survival kit too.
      > 
      > Clive. :)
      > 
      > 
      > 
      > 
      > Read this topic online here:
      > 
      > http://forums.matronics.com/viewtopic.php?p=402210#402210
      > 
      > 
      > 
      > 
      > 
      > 
      > 
      > 
      > 
      > 
      
      
Message 19
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  | 
      
      
| Subject:  | Re: Contact of Europa now at Wombleton .... | 
      
      Bob
      
      The Europa Aircraft website says that their temporary contact number is 0175
      1 432356. Alternatively you can contact them by email.
      
      Regards
      John
      
      On 7 Jun 2013, at 16:46, "Bob Harrison" <ptag.dev@talktalk.net> wrote:
      
      > Hi! All you clever administrators ....
      > Having been out of circulation in the Arctic recently  I noticed a message
       come through about Europa Spares moving out to Wombleton .  Does anyone who
       files such useful info have a new contact number I can get through to them p
      lease?
      > Regards
      > Bob H
      > 
      > 
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      > 
      
Message 20
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  | 
      
      
| Subject:  | Re: Scottish trip - advice? | 
      
      
      Hi! Clive,
      When you have paid for landing and services at Inverness you will think you
      own a piece of the airfield !
      There's a flying farmer up there ......I think James Austin  Just had new
      Torque tube clamps from me  I'm late for a dinner date so must shoot off
      o'wise I would research his e-mail for you he has his own landing strip .
      Regards
      Bob H 
      
      -----Original Message-----
      From: owner-europa-list-server@matronics.com
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of gtagr
      Sent: 07 June 2013 16:57
      Subject: Europa-List: Re: Scottish trip - advice?
      
      
      Thanks for the suggestions.  By way of a bit more detail to comment upon, my
      outline route at the moment is:
      
      Day 1: Wellesbourne to Fishburn.
      Day 2: Fishburn to Cumbernauld (an uncle lives nearby) Day 3: Cumbernauld to
      Wick via Aberdeen with the direct water crossing Day 4: Wick to Lerwick,
      overflying Kirkwall, Sanday, FairIsle and Sumburgh Day 5: Stay local to
      Lerwick, possibly fly around/to Fetlar and around Out Stack Day 6: Return to
      Inverness via Wick Day 7: Inverness to Islay Day 8: Islay to EGBW via
      Carlisle
      
      Further thoughts?
      
      
      Clive.
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=402218#402218
      
      
Message 21
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  | 
      
      
| Subject:  | Re: You'll Cry Pip Pins | 
      
      Pete=0Ayour explanation is correct. Thanks for expanding my criptic remarks
      !=0AGraham=0A=0A=0A=0A=0A________________________________=0A From: Pete <pe
      terz@zutrasoft.com>=0ATo: "europa-list@matronics.com" <europa-list@matronic
      s.com> =0ASent: Friday, 7 June 2013, 16:55=0ASubject: Re: Europa-List: You'
      ll Cry Pip Pins=0A =0A=0A=0AAll the lifting loads are taken by the lift pin
      s on the side of the fuse. The pip pins function only to tie the spars toge
      ther and keep the wings from folding up under G.=0A=0AThe geometry is such 
      that when the main spars are flexing under load, the pip pin locations on t
      he spars move downward relative to the lift pins at the side of the fuse (a
      s the lift pins are further out along the radius of the flexing spars), so 
      the net result is that the pip pins actually push DOWNWARDS on the seat bac
      k under high positive G's.....totally counter productive. =C2-The seat ba
      ck bushes should be clearance vertically IMHO to avoid this situation.=0A
      =0AThe seat back bushes may however provide some (weak?) support in keeping
       the pip pins from twisting out of the spars under their asymmetrical=C2-
      twisting load. =C2-Many gliders use fork-spar arrangements to avoid this.
      =0A=0ACheers,=0APete=0AA239=0A=0AOn Jun 7, 2013, at 9:45 AM, "William Danie
      ll" <wdaniell.longport@gmail.com> wrote:=0A=0A=0AGraham=0A>=C2-=0A>I am v
      ery interested by this statement .so as I understand it the spars 
      are the main load bearing structure in the airpcraft if the seat b
      ack bush does not do the this what does?=C2- How does the motorglider wor
      k?=0A>=C2-=0A>Will=0A>=C2-=0A>From:owner-europa-list-server@matronics.c
      om [mailto:owner-europa-list-server@matronics.com] On Behalf Of GRAHAM SING
      LETON=0A>Sent: Friday, June 07, 2013 04:42=0A>To: europa-list@matronics.com
      =0A>Subject: Re: Europa-List: You'll Cry Pip Pins=0A>=C2-=0A>Frans=0A>The
       pip pin on the port side is there to prevent the starboard spar from twist
      ing away from the =0A>port spar under high load. The starboard side has no 
      need of retention because the overlapping =0A>spar provides that function. 
      =0A>Strictly speaking the bush in the seat back bulkhead is of no value, in
       fact it increases the load on the spars.=0A>Be better without it as per th
      e motor glider. (but DYOR)=0A>Graham=0A>=C2-=0A>=C2-=0A>=0A>___________
      _____________________=0A>=0A>From:Frans Veldman <frans@privatepilots.nl>=0A
      >To: europa-list@matronics.com =0A>Sent: Friday, 7 June 2013, 9:07=0A>Subje
      ct: Re: Europa-List: You'll Cry Pip Pins=0A>=0A>--> Europa-List message pos
      ted by: Frans Veldman <frans@privatepilots.nl>=0A>=0A>On 06/07/2013 09:40 A
      M, Tony Renshaw wrote:=0A>=0A>>=C2- Talking about pip pins, does anyone s
      ee any merit in using two of the Port pip pins, another for the Std spar to
      o?=0A>=0A>If I recall correctly, there was some technical reason why both p
      ip pins=0A>are different. I forgot the details, but this discussion has bee
      n held=0A>before and someone with insight argued why using a pip pin on the
      =0A>starboard side was not such a good idea. It had something to do with th
      e=0A>different arrangement and thus different torsional loads on the=0A>sta
      rboard side because the spars overlay "the other way around". The pin=0A>ha
      d to be longer there to allow some movement, and because it needs to=0A>hav
      e some play a pip pin can not be used (unless you make it longer than=0A>it
       should be but then you need an additional retaining mechanism which=0A>of 
      course negates the whole idea of using a pip pin in the first place.)=0A>
      =0A>Although I have modified my aircraft quite a lot, this is an area where
      =0A>I am shy to deviate from the build plan, as it is one of the most=0A>cr
      itical structural area's. As all of the other pins are pip pins my bet=0A>i
      s that there must have been a reason why to use a different arrangement=0A>
      on this specific pin. Surely it can't be because it was cheaper or so,=0A>o
      r the designer was short of one pip pin and decided to wo==C2- --> http
      ://www.matronics.com/Navigator?Europa-List=0A>_ref="http://forums.matroni
      cs.com/" target="_blank">http://forums.matronbsp; Thank you for your gene
      rous nbsp; =C2- =C2- =C2- =C2- =C2- =C2- -Matt Dralle, List Adm
      in.=0A>=0A>=0A>=0A>=0A>=0A>=C2-=0A>=C2-=0A>http://www.matronics.com/Nav
      igator?Europa-List=0A><=C2-=C2-=C2-=C2-=C2-=C2-=C2-=C2-=C2
      -=C2-=C2-- MATRONICS WEB FORUMS -=0A>http://forums.matronics.com=0A>h
      ttp://www.matronics.com/contribution=0A>=C2-=0A>========
      ===0Atp://www.matronics.com/Navigator?Europa-List=0A======
      =====0Acs.com=0A=================
      ===================0Amatronics.com/cont
      ribution=0A=====================
      == 
      
Message 22
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  | 
      
      
| Subject:  | You'll Cry Pip Pins | 
      
      Well I damned, I=99d never have thought that.  Those thick spars 
      look like they should be supporting the aircraft but the weedy looking 
      fuze pins are actually do all the (lifting) work.  So the spars=99 
      main job is to prevent the wings folding forward or back?
      
      
      So the really important thing is to keep the spars together not tie the 
      spars into the fuze?
      
      
      I am woefully ignorant.
      
      
      Will
      
      
      From: Pete [mailto:peterz@zutrasoft.com] 
      Sent: Friday, June 07, 2013 10:56
      Cc: wdaniell.longport@gmail.com
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      All the lifting loads are taken by the lift pins on the side of the 
      fuse. The pip pins function only to tie the spars together and keep the 
      wings from folding up under G.
      
      
      The geometry is such that when the main spars are flexing under load, 
      the pip pin locations on the spars move downward relative to the lift 
      pins at the side of the fuse (as the lift pins are further out along the 
      radius of the flexing spars), so the net result is that the pip pins 
      actually push DOWNWARDS on the seat back under high positive 
      G's.....totally counter productive.  The seat back bushes should be 
      clearance vertically IMHO to avoid this situation.
      
      
      The seat back bushes may however provide some (weak?) support in keeping 
      the pip pins from twisting out of the spars under their asymmetrical 
      twisting load.  Many gliders use fork-spar arrangements to avoid this.
      
      
      Cheers,
      
      Pete
      
      A239
      
      
      On Jun 7, 2013, at 9:45 AM, "William Daniell" 
      <wdaniell.longport@gmail.com> wrote:
      
      Graham
      
      
      I am very interested by this statement .so as I understand it 
      the spars are the main load bearing structure in the airpcraft 
      if the seat back bush does not do the this what does?  How does the 
      motorglider work?
      
      
      Will
      
      
      From: owner-europa-list-server@matronics.com 
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of GRAHAM 
      SINGLETON
      Sent: Friday, June 07, 2013 04:42
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      Frans
      The pip pin on the port side is there to prevent the starboard spar from 
      twisting away from the 
      port spar under high load. The starboard side has no need of retention 
      because the overlapping 
      spar provides that function. 
      Strictly speaking the bush in the seat back bulkhead is of no value, in 
      fact it increases the load on the spars.
      Be better without it as per the motor glider. (but DYOR)
      Graham
      
      
        _____  
      
      
      From: Frans Veldman <frans@privatepilots.nl>
      Sent: Friday, 7 June 2013, 9:07
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      <frans@privatepilots.nl>
      
      On 06/07/2013 09:40 AM, Tony Renshaw wrote:
      
      >  Talking about pip pins, does anyone see any merit in using two of the 
      Port pip pins, another for the Std spar too?
      
      If I recall correctly, there was some technical reason why both pip pins
      are different. I forgot the details, but this discussion has been held
      before and someone with insight argued why using a pip pin on the
      starboard side was not such a good idea. It had something to do with the
      different arrangement and thus different torsional loads on the
      starboard side because the spars overlay "the other way around". The pin
      had to be longer there to allow some movement, and because it needs to
      have some play a pip pin can not be used (unless you make it longer than
      it should be but then you need an additional retaining mechanism which
      of course negates the whole idea of using a pip pin in the first place.)
      
      Although I have modified my aircraft quite a lot, this is an area where
      I am shy to deviate from the build plan, as it is one of the most
      critical structural area's. As all of the other pins are pip pins my bet
      is that there must have been a reason why to use a different arrangement
      on this specific pin. Surely it can't be because it was cheaper or so,
      or the designer was short of one pip pin and decided to wo=  --> 
      http://www.matronics.com/Navigator?Europa-List
      _ref="http://forums.matronics.com/" 
      target="_blank">http://forums.matronbsp; Thank you for your generous 
      nbsp;             -Matt Dralle, List Admin.
      
      
      http://www.matronics.com/Navigator?Europa-List
      <           - MATRONICS WEB FORUMS -
      http://forums.matronics.com
      http://www.matronics.com/contribution
      
      
Message 23
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  | 
      
      
| Subject:  | Re: Scottish trip - advice? | 
      
      
      so going the same way, shame we cant tie up.
      Looks a great scheme. Personally, though I would have thought it unlikely to get
      eight consecutive flyable days in a mountainous UK region.  My plan is to watch
      the weather and pick my day or two days and use the coast if I need to fly
      low level.
      
      --------
      Graeme Bird
      G-UMPY
      Mono 912S/Woodcomp 3000/3W
      Newby: 55 hours 1 year 
      g(at)gdbmk.co.uk
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=402238#402238
      
      
Message 24
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  | 
      
      
| Subject:  | Re: You'll Cry Pip Pins | 
      
      William=0Ajust a bit more ignorant than me! The wing spars stop the wings f
      olding up, (or down), the rear lift pins take the weight of the fuselage=0A
      into the wings and stop them folding forwards at high G loading, (that's no
      ne intuitive isn't it?) the front pins carry the resat of the fuse weight i
      nto the wings.=0AThe spars don't need to be tied the the fuselage.=0AGraham
      =0A=0A=0A=0A=0A________________________________=0A From: William Daniell <w
      daniell.longport@gmail.com>=0ATo: 'Pete' <peterz@zutrasoft.com>; europa-lis
      t@matronics.com =0ASent: Friday, 7 June 2013, 18:05=0ASubject: RE: Europa-L
      ist: You'll Cry Pip Pins=0A =0A=0A=0AWell I damned, I=99d never have 
      thought that.=C2- Those thick spars look like they should be supporting t
      he aircraft but the weedy looking fuze pins are actually do all the (liftin
      g) work. =C2-So the spars=99 main job is to prevent the wings foldi
      ng forward or back?=0A=C2-=0ASo the really important thing is to keep the
       spars together not tie the spars into the fuze?=0A=C2-=0AI am woefully i
      gnorant.=0A=C2-=0AWill=0A=C2-=0AFrom:Pete [mailto:peterz@zutrasoft.com]
       =0ASent: Friday, June 07, 2013 10:56=0ATo: europa-list@matronics.com=0ACc:
       wdaniell.longport@gmail.com=0ASubject: Re: Europa-List: You'll Cry Pip Pin
      s=0A=C2-=0AAll the lifting loads are taken by the lift pins on the side o
      f the fuse. The pip pins function only to tie the spars together and keep t
      he wings from folding up under G.=0A=C2-=0AThe geometry is such that when
       the main spars are flexing under load, the pip pin locations on the spars 
      move downward relative to the lift pins at the side of the fuse (as the lif
      t pins are further out along the radius of the flexing spars), so the net r
      esult is that the pip pins actually push DOWNWARDS on the seat back under h
      igh positive G's.....totally counter productive. =C2-The seat back bushes
       should be clearance vertically IMHO to avoid this situation.=0A=C2-=0ATh
      e seat back bushes may however provide some (weak?) support in keeping the 
      pip pins from twisting out of the spars under their asymmetrical=C2-twist
      ing load. =C2-Many gliders use fork-spar arrangements to avoid this.=0A
      =C2-=0ACheers,=0APete=0AA239=0A=0AOn Jun 7, 2013, at 9:45 AM, "William Da
      niell" <wdaniell.longport@gmail.com> wrote:=0AGraham=0A>=C2-=0A>I am very
       interested by this statement .so as I understand it the spars are
       the main load bearing structure in the airpcraft if the seat back
       bush does not do the this what does?=C2- How does the motorglider work?
      =0A>=C2-=0A>Will=0A>=C2-=0A>From:owner-europa-list-server@matronics.com
       [mailto:owner-europa-list-server@matronics.com] On Behalf Of GRAHAM SINGLE
      TON=0A>Sent: Friday, June 07, 2013 04:42=0A>To: europa-list@matronics.com
      =0A>Subject: Re: Europa-List: You'll Cry Pip Pins=0A>=C2-=0A>Frans=0A>The
       pip pin on the port side is there to prevent the starboard spar from twist
      ing away from the =0A>port spar under high load. The starboard side has no 
      need of retention because the overlapping =0A>spar provides that function. 
      =0A>Strictly speaking the bush in the seat back bulkhead is of no value, in
       fact it increases the load on the spars.=0A>Be better without it as per th
      e motor glider. (but DYOR)=0A>Graham=0A>=C2-=0A>=C2-=0A>=0A>___________
      _____________________=0A>=0A>From:Frans Veldman <frans@privatepilots.nl>=0A
      >To: europa-list@matronics.com =0A>Sent: Friday, 7 June 2013, 9:07=0A>Subje
      ct: Re: Europa-List: You'll Cry Pip Pins=0A>=0A>--> Europa-List message pos
      ted by: Frans Veldman <frans@privatepilots.nl>=0A>=0A>On 06/07/2013 09:40 A
      M, Tony Renshaw wrote:=0A>=0A>>=C2- Talking about pip pins, does anyone s
      ee any merit in using two of the Port pip pins, another for the Std spar to
      o?=0A>=0A>If I recall correctly, there was some technical reason why both p
      ip pins=0A>are different. I forgot the details, but this discussion has bee
      n held=0A>before and someone with insight argued why using a pip pin on the
      =0A>starboard side was not such a good idea. It had something to do with th
      e=0A>different arrangement and thus different torsional loads on the=0A>sta
      rboard side because the spars overlay "the other way around". The pin=0A>ha
      d to be longer there to allow some movement, and because it needs to=0A>hav
      e some play a pip pin can not be used (unless you make it longer than=0A>it
       should be but then you need an additional retaining mechanism which=0A>of 
      course negates the whole idea of using a pip pin in the first place.)=0A>
      =0A>Although I have modified my aircraft quite a lot, this is an area where
      =0A>I am shy to deviate from the build plan, as it is one of the most=0A>cr
      itical structural area's. As all of the other pins are pip pins my bet=0A>i
      s that there must have been a reason why to use a different arrangement=0A>
      on this specific pin. Surely it can't be because it was cheaper or so,=0A>o
      r the designer was short of one pip pin and decided to wo==C2- --> http
      ://www.matronics.com/Navigator?Europa-List=0A>_ref="http://forums.matroni
      cs.com/" target="_blank">http://forums.matronbsp; Thank you for your gene
      rous nbsp; =C2- =C2- =C2- =C2- =C2- =C2- -Matt Dralle, List Adm
      in.=0A>=0A>=0A>=0A>=0A>=0A>=0A>=C2-=0A>=C2-=0A>http://www.matronics.com
      /Navigator?Europa-List=0A><=C2-=C2-=C2-=C2-=C2-=C2-=C2-=C2-
      =C2-=C2-=C2-- MATRONICS WEB FORUMS -=0A>http://forums.matronics.com
      =0A>http://www.matronics.com/contribution=0A>=C2-=0A>=C2-=0A>=C2-=0A>
      http://www.matronics.com/Navigator?Europa-List=0A>http://forums.matronics.c
      ======= 
      
Message 25
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  | 
      
      
| Subject:  | You'll Cry Pip Pins | 
      
      Well i damned again and you=99re right it=99s not in the 
      least intuitive. It=99s fascinating!
      
      
      Did I understand that tie bar between the rear lift pins in the XS is 
      not present in the classic?  If so the these folding forward forces are 
      merely supported by the fuselage sides.
      
      
      Thanks
      
      
      Will
      
      
      From: owner-europa-list-server@matronics.com 
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of GRAHAM 
      SINGLETON
      Sent: Friday, June 07, 2013 15:15
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      William
      just a bit more ignorant than me! The wing spars stop the wings folding 
      up, (or down), the rear lift pins take the weight of the fuselage
      into the wings and stop them folding forwards at high G loading, (that's 
      none intuitive isn't it?) the front pins carry the resat of the fuse 
      weight into the wings.
      The spars don't need to be tied the the fuselage.
      Graham
      
      
        _____  
      
      From: William Daniell <wdaniell.longport@gmail.com>
      Sent: Friday, 7 June 2013, 18:05
      Subject: RE: Europa-List: You'll Cry Pip Pins
      
      
      Well I damned, I=99d never have thought that.  Those thick spars 
      look like they should be supporting the aircraft but the weedy looking 
      fuze pins are actually do all the (lifting) work.  So the spars=99 
      main job is to prevent the wings folding forward or back?
      
      
      So the really important thing is to keep the spars together not tie the 
      spars into the fuze?
      
      
      I am woefully ignorant.
      
      
      Will
      
      
      From: Pete [mailto:peterz@zutrasoft.com] 
      Sent: Friday, June 07, 2013 10:56
      Cc: wdaniell.longport@gmail.com
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      All the lifting loads are taken by the lift pins on the side of the 
      fuse. The pip pins function only to tie the spars together and keep the 
      wings from folding up under G.
      
      
      The geometry is such that when the main spars are flexing under load, 
      the pip pin locations on the spars move downward relative to the lift 
      pins at the side of the fuse (as the lift pins are further out along the 
      radius of the flexing spars), so the net result is that the pip pins 
      actually push DOWNWARDS on the seat back under high positive 
      G's.....totally counter productive.  The seat back bushes should be 
      clearance vertically IMHO to avoid this situation.
      
      
      The seat back bushes may however provide some (weak?) support in keeping 
      the pip pins from twisting out of the spars under their asymmetrical 
      twisting load.  Many gliders use fork-spar arrangements to avoid this.
      
      
      Cheers,
      
      Pete
      
      A239
      
      
      On Jun 7, 2013, at 9:45 AM, "William Daniell" 
      <wdaniell.longport@gmail.com> wrote:
      
      Graham
      
      
      I am very interested by this statement .so as I understand it 
      the spars are the main load bearing structure in the airpcraft 
      if the seat back bush does not do the this what does?  How does the 
      motorglider work?
      
      
      Will
      
      
      From: owner-europa-list-server@matronics.com 
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of GRAHAM 
      SINGLETON
      Sent: Friday, June 07, 2013 04:42
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      Frans
      The pip pin on the port side is there to prevent the starboard spar from 
      twisting away from the 
      port spar under high load. The starboard side has no need of retention 
      because the overlapping 
      spar provides that function. 
      Strictly speaking the bush in the seat back bulkhead is of no value, in 
      fact it increases the load on the spars.
      Be better without it as per the motor glider. (but DYOR)
      Graham
      
      
        _____  
      
      
      From: Frans Veldman <frans@privatepilots.nl>
      Sent: Friday, 7 June 2013, 9:07
      Subject: Re: Europa-List: You'll Cry Pip Pins
      
      
      <frans@privatepilots.nl>
      
      On 06/07/2013 09:40 AM, Tony Renshaw wrote:
      
      >  Talking about pip pins, does anyone see any merit in using two of the 
      Port pip pins, another for the Std spar too?
      
      If I recall correctly, there was some technical reason why both pip pins
      are different. I forgot the details, but this discussion has been held
      before and someone with insight argued why using a pip pin on the
      starboard side was not such a good idea. It had something to do with the
      different arrangement and thus different torsional loads on the
      starboard side because the spars overlay "the other way around". The pin
      had to be longer there to allow some movement, and because it needs to
      have some play a pip pin can not be used (unless you make it longer than
      it should be but then you need an additional retaining mechanism which
      of course negates the whole idea of using a pip pin in the first place.)
      
      Although I have modified my aircraft quite a lot, this is an area where
      I am shy to deviate from the build plan, as it is one of the most
      critical structural area's. As all of the other pins are pip pins my bet
      is that there must have been a reason why to use a different arrangement
      on this specific pin. Surely it can't be because it was cheaper or so,
      or the designer was short of one pip pin and decided to wo=  --> 
      http://www.matronics.com/Navigator?Europa-List
      _ref="http://forums.matronics.com/" 
      target="_blank">http://forums.matronbsp <http://forums.matronbsp/> ; 
      Thank you for your generous nbsp;             -Matt Dralle, List Admin.
      
      
      http://www.matronics.com/Navigator?Europa-List
      <           - MATRONICS WEB FORUMS -
      http://forums.matronics.com <http://forums.matronics.com/> 
      http://www.matronics.com/contribution
      
      
      http://www.matronics.com/Navigator?Europa-List
      http://forums.matronics.com
      http://www.matronics.com/contribution
      
      
      http://www.ma <http://www.ma%22nofollow> "nofollow" target="_blank" 
      href="http://forums.matronics.com/">http://f=========
      
      
Message 26
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  | 
      
      
| Subject:  | Re: You'll Cry Pip Pins | 
      
      Yes,=0AGraham=0Ano comment!=0A=0A=0A=0A=0A________________________________
      =0A From: William Daniell <wdaniell.longport@gmail.com>=0ATo: europa-list@m
      atronics.com =0ASent: Friday, 7 June 2013, 21:48=0ASubject: RE: Europa-List
      : You'll Cry Pip Pins=0A =0A=0A=0AWell i damned again and you=99re ri
      ght it=99s not in the least intuitive. It=99s fascinating!=0A
      =C2-=0ADid I understand that tie bar between the rear lift pins in the XS
       is not present in the classic?=C2- If so the these folding forward force
      s are merely supported by the fuselage sides.=0A=C2-=0AThanks=0A=C2-=0A
      Will=0A=C2-=0AFrom:owner-europa-list-server@matronics.com [mailto:owner-e
      uropa-list-server@matronics.com] On Behalf Of GRAHAM SINGLETON=0ASent: Frid
      ay, June 07, 2013 15:15=0ATo: europa-list@matronics.com=0ASubject: Re: Euro
      pa-List: You'll Cry Pip Pins=0A=C2-=0AWilliam=0Ajust a bit more ignorant 
      than me! The wing spars stop the wings folding up, (or down), the rear lift
       pins take the weight of the fuselage=0Ainto the wings and stop them foldin
      g forwards at high G loading, (that's none intuitive isn't it?) the front p
      ins carry the resat of the fuse weight into the wings.=0AThe spars don't ne
      ed to be tied the the fuselage.=0AGraham=0A=C2-=0A=C2-=0A=0A___________
      _____________________=0A=0AFrom:William Daniell <wdaniell.longport@gmail.co
      m>=0ATo: 'Pete' <peterz@zutrasoft.com>; europa-list@matronics.com =0ASent: 
      Friday, 7 June 2013, 18:05=0ASubject: RE: Europa-List: You'll Cry Pip Pins
      =0A=C2-=0AWell I damned, I=99d never have thought that.=C2- Those
       thick spars look like they should be supporting the aircraft but the weedy
       looking fuze pins are actually do all the (lifting) work. =C2-So the spa
      rs=99 main job is to prevent the wings folding forward or back?=0A=C2
      -=0ASo the really important thing is to keep the spars together not tie t
      he spars into the fuze?=0A=C2-=0AI am woefully ignorant.=0A=C2-=0AWill
      =0A=C2-=0AFrom:Pete [mailto:peterz@zutrasoft.com] =0ASent: Friday, June 0
      7, 2013 10:56=0ATo: europa-list@matronics.com=0ACc: wdaniell.longport@gmail
      .com=0ASubject: Re: Europa-List: You'll Cry Pip Pins=0A=C2-=0AAll the lif
      ting loads are taken by the lift pins on the side of the fuse. The pip pins
       function only to tie the spars together and keep the wings from folding up
       under G.=0A=C2-=0AThe geometry is such that when the main spars are flex
      ing under load, the pip pin locations on the spars move downward relative t
      o the lift pins at the side of the fuse (as the lift pins are further out a
      long the radius of the flexing spars), so the net result is that the pip pi
      ns actually push DOWNWARDS on the seat back under high positive G's.....tot
      ally counter productive. =C2-The seat back bushes should be clearance ver
      tically IMHO to avoid this situation.=0A=C2-=0AThe seat back bushes may h
      owever provide some (weak?) support in keeping the pip pins from twisting o
      ut of the spars under their asymmetrical=C2-twisting load. =C2-Many gli
      ders use fork-spar arrangements to avoid this.=0A=C2-=0ACheers,=0APete=0A
      A239=0A=0AOn Jun 7, 2013, at 9:45 AM, "William Daniell" <wdaniell.longport@
      gmail.com> wrote:=0AGraham=0A>=C2-=0A>I am very interested by this statem
      ent .so as I understand it the spars are the main load bearing str
      ucture in the airpcraft if the seat back bush does not do the this
       what does?=C2- How does the motorglider work?=0A>=C2-=0A>Will=0A>=C2
      -=0A>From:owner-europa-list-server@matronics.com [mailto:owner-europa-lis
      t-server@matronics.com] On Behalf Of GRAHAM SINGLETON=0A>Sent: Friday, June
       07, 2013 04:42=0A>To: europa-list@matronics.com=0A>Subject: Re: Europa-Lis
      t: You'll Cry Pip Pins=0A>=C2-=0A>Frans=0A>The pip pin on the port side i
      s there to prevent the starboard spar from twisting away from the =0A>port 
      spar under high load. The starboard side has no need of retention because t
      he overlapping =0A>spar provides that function. =0A>Strictly speaking the b
      ush in the seat back bulkhead is of no value, in fact it increases the load
       on the spars.=0A>Be better without it as per the motor glider. (but DYOR)
      =0A>Graham=0A>=C2-=0A>=C2-=0A>=0A>________________________________=0A>
      =0A>From:Frans Veldman <frans@privatepilots.nl>=0A>To: europa-list@matronic
      s.com =0A>Sent: Friday, 7 June 2013, 9:07=0A>Subject: Re: Europa-List: You'
      ans@privatepilots.nl>=0A>=0A>On 06/07/2013 09:40 AM, Tony Renshaw wrote:=0A
      >=0A>>=C2- Talking about pip pins, does anyone see any merit in using two
       of the Port pip pins, another for the Std spar too?=0A>=0A>If I recall cor
      rectly, there was some technical reason why both pip pins=0A>are different.
       I forgot the details, but this discussion has been held=0A>before and some
      one with insight argued why using a pip pin on the=0A>starboard side was no
      t such a good idea. It had something to do with the=0A>different arrangemen
      t and thus different torsional loads on the=0A>starboard side because the s
      pars overlay "the other way around". The pin=0A>had to be longer there to a
      llow some movement, and because it needs to=0A>have some play a pip pin can
       not be used (unless you make it longer than=0A>it should be but then you n
      eed an additional retaining mechanism which=0A>of course negates the whole 
      idea of using a pip pin in the first place.)=0A>=0A>Although I have modifie
      d my aircraft quite a lot, this is an area where=0A>I am shy to deviate fro
      m the build plan, as it is one of the most=0A>critical structural area's. A
      s all of the other pins are pip pins my bet=0A>is that there must have been
       a reason why to use a different arrangement=0A>on this specific pin. Surel
      y it can't be because it was cheaper or so,=0A>or the designer was short of
       one pip pin and decided to wo==C2- --> http://www.matronics.com/Naviga
      tor?Europa-List=0A>_ref="http://forums.matronics.com/" target="_blank">
      http://forums.matronbsp; Thank you for your generous nbsp; =C2- =C2- 
      =C2- =C2- =C2- =C2- -Matt Dralle, List Admin.=0A>=0A>=0A>=0A>=0A>
      =0A>=C2-=0A>=C2-=0A>http://www.matronics.com/Navigator?Europa-List=0A><
      =C2-=C2-=C2-=C2-=C2-=C2-=C2-=C2-=C2-=C2-=C2-- MATRONI
      CS WEB FORUMS -=0A>http://forums.matronics.com=0A>http://www.matronics.com/
      contribution=0A>=C2-=0A>=C2-=0A>=C2-=0A>=C2-=0A>http://www.matronic
      s.com/Navigator?Europa-List=0A>http://forums.matronics.com=0A>http://www.ma
      tronics.com/contribution=0A>=C2-=0Ahttp://www.ma"nofollow" target="_bla
      nk" href="http://forums.matronics.com/">http://f========
      ===0A=C2-=0A=C2-=0A=C2-=0A=C2-=0Ahttp://www.matronics.com/Navig
      ator?Europa-List=0Ahttp://forums.matronics.com=0Ahttp://www.matronics.com/c
      ==================== 
      
Message 27
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  | 
      
      
| Subject:  | Re: Contact of Europa now at Wombleton .... | 
      
      Better than a number lads, Karen at Europa says I, (we) can fly in now to pi
      ck up our spares and have a look round with a cup of tea thrown in gratis!! 
      
      
      Regards
      
      
      Trev G-LINN
      
      Sent from my iPad
      
      On 7 Jun 2013, at 16:46, "Bob Harrison" <ptag.dev@talktalk.net> wrote:
      
      > Hi! All you clever administrators ....
      > Having been out of circulation in the Arctic recently  I noticed a message
       come through about Europa Spares moving out to Wombleton .  Does anyone who
       files such useful info have a new contact number I can get through to them p
      lease?
      > Regards
      > Bob H
      > 
      > 
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      ==========================
      =========
      > 
      
Message 28
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  | 
      
      
| Subject:  | Contact of Europa now at Wombleton .... | 
      
      Many thanks to all who provided the "heads up " on this issue.
      
      Regards
      
      Bob Harrison
      
      
      From: owner-europa-list-server@matronics.com
      [mailto:owner-europa-list-server@matronics.com] On Behalf Of Bob Harrison
      Sent: 07 June 2013 16:47
      Subject: Europa-List: Contact of Europa now at Wombleton ....
      
      
      Hi! All you clever administrators ....
      
      Having been out of circulation in the Arctic recently  I noticed a message
      come through about Europa Spares moving out to Wombleton .  Does anyone who
      files such useful info have a new contact number I can get through to them
      please?
      
      Regards
      
      Bob H 
      
      
 
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