We have tried to make the kits more complete and easier to build focusing on what builders seem to struggle with the most. At the factory last week we focused on one particular change to the kits. Drilling the ailerons & flaps completely so builders just insert the bolts, tighten the bolts/nuts, and all is done except covering. I discussed with Bob how we would implement this change, and think a description will be useful to everyone building their kits or scratch builders.
At the end of this post I will ask for comments from you guys on a couple things.
Bob had the workers make four plywood stands for the wing bottom and four more conforming to the wing airfoil shape on the top. See pictures - especially side view. Since we had just loaded the biggest truckload of kits ever (6 kits) in a 53 ft trailer four days before, we didn't have a fully riveted wing to work with. That's why all the clecos. We found that with these plywood boards top & bottom, it was super easy to position the ailerons and flaps vertically. First time we saw the aileron a little high, but adjusted the hinges to where the aileron fit tightly between the boards. Same with flap. Hinges were clamped in place with small C clamps.
Bob instructed us to position the ailerons horizontally by first making sure the trailing edge rib that the wingtip is attached to was totally straight/inline with the outboard main rib. Then give the aileron the 1/2" spacing called for. Then space the flap with the 1/2" between the flap and the aileron. All pretty straight forward and easy.
The only harder part was when the aileron nose rib was rubbing on the upper skin trailing edge when the aileron was moved. I was aware of this as on my new Patrol and my LSA also I had to remove some material from the upper skin trailing edge to give some clearance. Bob had us look at EVERYTHING to see why it was rubbing. That the aileron attach weldments had the proper distance from the rear spar - they did. The amount of skin extending aft of the rear spar in the pocket ribs area on the upper and lower skins. The upper was spot on. Lower was a little longer but caused no problem. The shape of the pocket ribs as made by the rib hydroform plant. They were perfect. So we couldn't really find any deviation from the plans of the parts being used to account for the interference.
Scaling off the plans - the upper skin (where the rubbing was) - extends .500 aft from the upper bend in the pocket skin. Leaving .500 for that row of rivets for the trailing edge there in the aileron pocket area. After explaining to Bob what we saw - he said no issue trimming off up to maybe 1/4" of the skin in that area. Leaving 1/4" of area for that last row of rivets grabbing the top skin and the pocket skin. The goal was 1/8" gap between the aileron leading edge and the upper rear skin. Leaving room for the fabric covering that goes on the aileron.
It turned out taking .150 gave a little more than 1/8" clearance required. Still leaving lot of spacing room for the line of rivets. We paid some attention to the vertical placement of the flap/aileron steel hinges so their attach holes had good edge margin on the .063 doublers on the aft side of the spars. The workers now understand how to do this and how the end result needs to be. I am sure the next time they do it will take a little time, but soon it will be quite fast for them to do this additional step on the kits.
Per the plans - the hinges for the flap and aileron do not allow the pushrod rod end bearings Bob recommends to just fit in between the hinges as the ball of the rod end bearing is wider than the spherical bearings used on the attach weldments, So builders have needed to put a little joggle into the upper parts of the hinges where the pushrods attach. In the picture you can see a workers first attempt at joggling the hinges. Not perfect but certainly usable. The ones delivered with kits will look better.
Now a question that I hope will give some of your thoughts on one change that Bob has considered. He has always recommend nutplates for the aft face of the aileron & flap spars so hinges can be removed. But recently he told me that he has never once needed to remove a hinge after covering. So he thought regular AN365 nuts were probably good enough. What do you guys think? Has anyone ever needed to remove aileron or flap hinges after covering? I have not. Please let me know your collective thinking on this question. While I do not have 3/16" nutplates down at the factory now - they could continue the same approach with nutplates if it is best. I can send some nutplates of that size down. Either way - the triangle and pyramid shaped reinforcing gussets will be all finish riveted. Not left to be finish riveted by the builder after installing nutplates. Please let me know what you think.
One other question concerning all the changes in the kits during the past 1.5 years. I would like some opinions on how many hours of work these changes would save a builder. Here are the changes:
1) Drilling wings to fuselage, and wing struts all drilled
2) Fuel tanks finish installed in the wings with the straps made at the factory and the upper skin opened for the tank filler neck.
3) Pouring most or all of the lead required for the elevator counter weights.
4) Now having the ailerons & flaps finish drilled so just inserting the bolts places the control surfaces in the correct place.
How many hours of work do yall think these changes saved? There have been some other improvements like the Patrol/LSA throttle set up. The new Model B ceiling that allows easier installation of skylights. Or continue to use a fabric ceiling. And the more finished way we are set up to install the fuel vales and gascolators. But these do not really save time actually building. But may save some head scratching time figuring out how to do these things. Your response on the time saved from us doing the above steps would be interesting.
At this time of the year, we would like to thank you all for your business, your confidence in us, and your friendship. Mark
At the end of this post I will ask for comments from you guys on a couple things.
Bob had the workers make four plywood stands for the wing bottom and four more conforming to the wing airfoil shape on the top. See pictures - especially side view. Since we had just loaded the biggest truckload of kits ever (6 kits) in a 53 ft trailer four days before, we didn't have a fully riveted wing to work with. That's why all the clecos. We found that with these plywood boards top & bottom, it was super easy to position the ailerons and flaps vertically. First time we saw the aileron a little high, but adjusted the hinges to where the aileron fit tightly between the boards. Same with flap. Hinges were clamped in place with small C clamps.
Bob instructed us to position the ailerons horizontally by first making sure the trailing edge rib that the wingtip is attached to was totally straight/inline with the outboard main rib. Then give the aileron the 1/2" spacing called for. Then space the flap with the 1/2" between the flap and the aileron. All pretty straight forward and easy.
The only harder part was when the aileron nose rib was rubbing on the upper skin trailing edge when the aileron was moved. I was aware of this as on my new Patrol and my LSA also I had to remove some material from the upper skin trailing edge to give some clearance. Bob had us look at EVERYTHING to see why it was rubbing. That the aileron attach weldments had the proper distance from the rear spar - they did. The amount of skin extending aft of the rear spar in the pocket ribs area on the upper and lower skins. The upper was spot on. Lower was a little longer but caused no problem. The shape of the pocket ribs as made by the rib hydroform plant. They were perfect. So we couldn't really find any deviation from the plans of the parts being used to account for the interference.
Scaling off the plans - the upper skin (where the rubbing was) - extends .500 aft from the upper bend in the pocket skin. Leaving .500 for that row of rivets for the trailing edge there in the aileron pocket area. After explaining to Bob what we saw - he said no issue trimming off up to maybe 1/4" of the skin in that area. Leaving 1/4" of area for that last row of rivets grabbing the top skin and the pocket skin. The goal was 1/8" gap between the aileron leading edge and the upper rear skin. Leaving room for the fabric covering that goes on the aileron.
It turned out taking .150 gave a little more than 1/8" clearance required. Still leaving lot of spacing room for the line of rivets. We paid some attention to the vertical placement of the flap/aileron steel hinges so their attach holes had good edge margin on the .063 doublers on the aft side of the spars. The workers now understand how to do this and how the end result needs to be. I am sure the next time they do it will take a little time, but soon it will be quite fast for them to do this additional step on the kits.
Per the plans - the hinges for the flap and aileron do not allow the pushrod rod end bearings Bob recommends to just fit in between the hinges as the ball of the rod end bearing is wider than the spherical bearings used on the attach weldments, So builders have needed to put a little joggle into the upper parts of the hinges where the pushrods attach. In the picture you can see a workers first attempt at joggling the hinges. Not perfect but certainly usable. The ones delivered with kits will look better.
Now a question that I hope will give some of your thoughts on one change that Bob has considered. He has always recommend nutplates for the aft face of the aileron & flap spars so hinges can be removed. But recently he told me that he has never once needed to remove a hinge after covering. So he thought regular AN365 nuts were probably good enough. What do you guys think? Has anyone ever needed to remove aileron or flap hinges after covering? I have not. Please let me know your collective thinking on this question. While I do not have 3/16" nutplates down at the factory now - they could continue the same approach with nutplates if it is best. I can send some nutplates of that size down. Either way - the triangle and pyramid shaped reinforcing gussets will be all finish riveted. Not left to be finish riveted by the builder after installing nutplates. Please let me know what you think.
One other question concerning all the changes in the kits during the past 1.5 years. I would like some opinions on how many hours of work these changes would save a builder. Here are the changes:
1) Drilling wings to fuselage, and wing struts all drilled
2) Fuel tanks finish installed in the wings with the straps made at the factory and the upper skin opened for the tank filler neck.
3) Pouring most or all of the lead required for the elevator counter weights.
4) Now having the ailerons & flaps finish drilled so just inserting the bolts places the control surfaces in the correct place.
How many hours of work do yall think these changes saved? There have been some other improvements like the Patrol/LSA throttle set up. The new Model B ceiling that allows easier installation of skylights. Or continue to use a fabric ceiling. And the more finished way we are set up to install the fuel vales and gascolators. But these do not really save time actually building. But may save some head scratching time figuring out how to do these things. Your response on the time saved from us doing the above steps would be interesting.
At this time of the year, we would like to thank you all for your business, your confidence in us, and your friendship. Mark
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