HI Guys,
Ok, I have the rear spar assembled and permanently installed. I have all the nuts, bolts, screws, etc in the main spar, hundreds of them :-) The only thing left to do is rivet the outer ribs and the aft edge of the aft ribs to the rear spar. I went to the airport and picked up a roll around table that is about the right height to support the outer wing panel.
The main spar pins and pivot bolts are in place and fit snug.
It is difficult to get a hangar where I am. So, when I liquidated my fleet in order to get prepared for retirement, I picked up a Grega GN-1 Aircamper so they couldn't kick me out of my hangar. The plan was to fly the GN-1, build a house for retirement, build another airplane, and be back in shape in about three years. Life and responsibility got in the way. Now it's been about eleven years. The poor GN-1 has been sitting and collecting dust while keeping my hangar reserved. I feel bad that I let it go, but it did serve its purpose.
Sure felt good to be at the airport. Can't wait to be back!
Anyway, the Onex rear spar pin location is drilled to 1/4" . I will ream the outer wing panel rear spar to 1/4" and see if everything mates up.
Questions:
The Onex will eventually share a hangar. so folding wings is critical to it's mission. Are there any secrets to getting a smooth locking action? Any advice appreciated.
It appears that the final pin hole in the rear spar needs to be drilled/reamed at a slight angle to line up with the locking mechanism. Is that right? I really want a tight fit.
The holes in the rear spar for rib #3 are missing. Any idea why?
Thanks for Your Time,
Wes