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#11
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On Apr 20, 7:44 am, wrote:
I saw a reference to a repair team in one of Bob Kuykendall's posts, a team that did the 103's, but I suppose those were Grob guys Bob? Gosh, it's been like a dozen years, I don't remember that much about it. But as I recall it, it _was_ a team sent around by Grob, they'd lined up several aircraft each at several shops around the country and did a grand tour. I saw them briefly, I think at Steve Brown's Bay Area Composite Repair. As I recall the repair involved cutting through the spar stub shear web to liberate the chunks of plywood to which the spigot was bolted or riveted, leaving an ugly rectangular notch at the end of the stub but not removing material from the spar caps. The beefier replacement spigot and its support (probably plywood, but perhaps prefabbed fiberglass plate, I don't recall) was placed into this notch, aligned with a fixture that the team had brought with them, and floxed into position. After the flox cured, the spigot and its support was secured with several shear wraps of cloth. I don't recall if they ground away the original shear wraps; they might have done so to keep the spar stub within its original envelope. As an aside, this series of repairs is one of the events where I first started to comprehend that there's no particular magic to composite aircraft structure. I remember spending quite a while looking at one of the cut-open aircraft under repair after the guys had knocked off for the day. I don't remember much of what I saw, but I do remember thinking "What, is this all there is?" Of course, there's a lot of careful engineering to it, engineering that I'm not qualified to practice or for some of it to even understand. But I think that a lot of it is just a mix of common sense plus stuff that people tried and tested and found to work sufficiently, and the engineering came later to figure out _why_ it worked. Thanks, Bob K. |
#12
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Hello Stephen,
FYI - An AD for this issue was put out in Canada many years ago (February 1991)! looking at grob.aerospace.de I found this document: http://www.grob-aerospace.net/filead...SB_Summary.pdf And searching this document I found: 11.10.90 Überprüfung und Austausch der Holmstummelbolzen Inspection and replacement of spar spigot assemblies ASTIR CS, ASTIR CS 77, ASTIR JEANS, STANDARD II, CLUB II, CLUB III, STANDARD III, CLUB IIIb alle Werk-Nr. / all S/N regards Werner |
#13
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Todd,
The work must be done in a FAA certifid glider repair station, like John Murry's or Gehrlein in your neck of the woods. it involves about 20 hours of work + the cost of the kit from Grob. It involves assembling the ship with wax donuts on the old spigots to determine the excess lateral slop that must be removed when the new spigots are installed, then grind and remove the old, then fit the new with factory jig, scarf spar but and lay up 8 layers of 92125 for the replacement spar wrap. I would estimat $1800 to $2400 bucks. JJ |
#14
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JJ,
Would Rutan style 7725 be a similar cloth to the 92125 European cloth? Thanks, Brad On Apr 20, 5:20 pm, JJ Sinclair wrote: Todd, The work must be done in a FAA certifid glider repair station, like John Murry's or Gehrlein in your neck of the woods. it involves about 20 hours of work + the cost of the kit from Grob. It involves assembling the ship with wax donuts on the old spigots to determine the excess lateral slop that must be removed when the new spigots are installed, then grind and remove the old, then fit the new with factory jig, scarf spar but and lay up 8 layers of 92125 for the replacement spar wrap. I would estimat $1800 to $2400 bucks. JJ |
#15
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On Apr 22, 10:25 am, Brad wrote:
JJ, Would Rutan style 7725 be a similar cloth to the 92125 European cloth? Thanks, Brad Yep, but when working with certified aircraft like the 102, one must use the specified stuff. The kit I got from Grob had per-cut 92125 sections, everything but resin...............BTW, Williams Soaring (Rex) just got 50 gallons of L285 epoxy at half the price that Spruce & Seciality is getting. JJ |
#16
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JJ,
Thanks a lot for this information. It was a factory supplied jig that was used for the replacement ? Todd On Apr 20, 8:20 pm, JJ Sinclair wrote: Todd, The work must be done in a FAA certifid glider repair station, like John Murry's or Gehrlein in your neck of the woods. it involves about 20 hours of work + the cost of the kit from Grob. It involves assembling the ship with wax donuts on the old spigots to determine the excess lateral slop that must be removed when the new spigots are installed, then grind and remove the old, then fit the new with factory jig, scarf spar but and lay up 8 layers of 92125 for the replacement spar wrap. I would estimat $1800 to $2400 bucks. JJ |
#17
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On Apr 23, 8:46 am, toad wrote:
JJ, Thanks a lot for this information. It was a factory supplied jig that was used for the replacement ? Todd On Apr 20, 8:20 pm, JJ Sinclair wrote: Todd, The work must be done in a FAA certifid glider repair station, like John Murry's or Gehrlein in your neck of the woods. it involves about 20 hours of work + the cost of the kit from Grob. It involves assembling the ship with wax donuts on the old spigots to determine the excess lateral slop that must be removed when the new spigots are installed, then grind and remove the old, then fit the new with factory jig, scarf spar but and lay up 8 layers of 92125 for the replacement spar wrap. I would estimat $1800 to $2400 bucks. JJ Todd, Did you happen to notice the 3/21/05 response date on the Airworthiness Concern Statement? |
#18
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![]() Todd, Did you happen to notice the 3/21/05 response date on the Airworthiness Concern Statement? Yes, at least after it was pointed out :-) I think that there might be a typo. The real deadline for comments in May 11th, I think. Todd |
#19
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On Apr 23, 10:11 am, toad wrote:
Todd, Did you happen to notice the 3/21/05 response date on the Airworthiness Concern Statement? Yes, at least after it was pointed out :-) I think that there might be a typo. The real deadline for comments in May 11th, I think. Todd Correct, 5/11/2007 is the deadline for comments into the AOPA. Jim |
#20
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What the heck is a spar spigot?
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