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Wing Construction of my Rans S6S Page 1 |
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Final assembly & engine install
If you don't have it this is an invaluable book for aircraft mechanics and homebuilders. Aircraft Inspection Repair and Alterations AC 43.13-1B AC 43.13-2A
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3-28-06 |
Assembled left front and rear wing spar |
1.5 hrs |
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3-29-06 |
Assembled left wing internal structure |
2.5 hrs |
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3-31-06 |
Assembled rib jig and ribs for left wing |
2.5 hrs |
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4-2-06 |
Assembled ribs on left wing structure |
2.0 hrs |
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4-3-06 |
Assembled root rib, riveted top root skin, assembled and installed tip rib on left wing |
2.5 hrs |
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4-4-06 |
Installed lower root skin, epoxied top and bottom root skins to spars |
1.25 hrs |
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4-5-06 |
riveted leading edge skin to ribs and epoxied to to spar |
1.5 hrs |
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4-6-06 |
installed fuel scupper, cut filler neck to length, installed the two rivets on top and bottom root skins in rear spar, installed static port and drilled for pitot tube, installed tip wrap |
2.5. hrs |
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4-9-06 |
Began getting parts together for right wing. Rearranged shop to allow room for both wings. Relocated fuselage to the basement. |
1.0 hrs |
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4-10-06 |
Began assembly of right wing structure. |
1.0 hrs |
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PIC 1....It's hard to tell, but if you draw a pencil line on the rear spar down the center line of the predrilled holes extended to the end and draw a center line on the spar extension down the center line of the predrilled hinge holes to the inboard edge when you slide the tow together all you have to do is rotate the tube until the holes are lined up, drill and rivet. PIC 2....Drill the lift strut attach holes 3/8" with a sharp bit and the compression tube are too tight. I ran the deburr tool one turn at a time around the holes until I had a snug press fit.
PIC 2....I couldn't figure out what the second hole in the flap compression tube was for. I was talking to Mike Gordon today and he told me there was a jury strut modification mid 2003. It seems the was a possibility of vibration of the aft lift strut with the triangular jury strut setup. This is ironic as I was having a dicussion with a friend of mine a couple of weeks ago about that very possibility. Thanks Mike! If I understand the new setup the jury struts come from the from spar attach point, down to the front strut, across to the rear strut, up to the attach point at the mysterious second hole in the flap compression tube. If this is correct without any diagonal bracing thus sets the possibility of fore and aft resonance in the lift struts from the irregular propwash creating premature wear of the lift strut attach points and possible failure of same. I'm going to make my first call to Ed at Rans to get more info. Note: This is my builder log and website take my ramblings with a grain of salt just notes to myself and I may not have understand the entire setup! Entry 4-25-06: After several discussions on this subject it has become my conclusion the force vectors do no equate to the theory proposed above. I have still not talked to Rans, just several friends. Simply put I think I was wrong! |
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4-12-06 |
Built ribs for right wing |
2.5 hrs |
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4-16-06 |
worked on right wing assemble and tank installation |
6.0 hrs |
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4-25-06 |
installed tank fittings and tank in right wing |
2.5 hrs |
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| 5-10-06 | installed top and bottom root skins and wing tip bow | 1.5 hrs | |
| 5-11-06 | riveted ribs to spars began install of tip rib | 2.0 hrs | |
| 5-15-06 | finished tip rib, installed top and bottom wing root skins, laid out top leading edge skin | 2.0 hrs | |
| 5-16-06 | filled leading edge to skin transition with epoxy micro balloon mixture, installed fuel scupper and cut filler neck to proper length | 2.0 hrs | |
| 5-17-06 | built wing rotisserie stands | 2.5 hrs | |
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