Fitting the longerons to the aft fuselage - 9 hours

As usual. It's been a very busy week leaving not a whole lot of time to work on the RV. I am teaching ground school one day a week but frankly its lots of work to write power point presentations. Did I mention its not easy to teach...You really want to know a subject, try teaching it.

I rechecked the fit of the longerons just to make sure I was happy with everything. I need to make very small adjustments for the vertical stabilizer bars. (Longeron openings are a tad snug). I also double checked the ends of the angles for trimming.


Now that I'm happy with the fit of the F-710B angle I riveted it to the bulkhead.

Next step I cleaned up the longerons. I filed the openings for the horizontal stabilizer bars so they weren't so tight. I filed down some thickness on the flange that was trimmed back on the aft end, and I also timed the aft length so that it sat flush with the tab on the aft bulkhead.


All ready to install on the fuse and then to flip the fuse over.


Next I was then ready to join the aft and center sections. Slow and easy wins the race.

It occurred to me after some time that the F-704 Bulkhead does not sit "in" the angle. I used some spacers to lift up the F-704 bulkhead as it sits on "top" of the angle.Then the side skins and everything else started to fit quite nicely.

Worked on the F-710B angle - 3 hours.

The Van’s Facebook group basically came back with the opinion that given the chance. Make a new angle. Fortunately I have a length of spare angle already so making a new one is fairly easy. Getting the angle cut to a correct length was relatively easy since I have the old piece as a guide. I could easily fine tune the length as I could cleco the angle in and measure the 0.125" off the side skins.

The trickier item is I made a relief for the tab to fit in the angle which would allow. This took quite a bit of work with the files but here is what it looks like.

The result is that this allows the top side of the angle flange to overhang the tab and allows for a very snug fit with the longeron.



At the end of the day, there was a lot of fussing with this area to get the angles to fit snug. I highly recommend that anyone trying this pre-order some spare angle and prepare yourself to fuss with this area. Seems many planes out there have fitment issues with this area and edge distance can become an issue if you are not careful. As a side note, Steven Lynn on the Vans Group suggested a gusset/shim in that area (Normally the plans call for just a shim) but I sure like the idea of this gusset.

Working on finishing up the center section - 7 hours

While I’m waiting on the paint to dry on the new platform I built in the garage. I went to work on the center section to clean up a few outstanding items. One of the items I haven’t addressed is countersunk the F-705 bulkhead for the nutplates (for the removable baggage floors).

I countersunk for nutplates and then I masked off the assembly and spot primed the area. 

Since I had the primer out, I touched up the skin under the forward F-704 bulkhead/spar. 

Next step I need to make sure the aft fuselage is prep’d for the longerons. Reading other build logs. I see that the relief hole for the longerons in the bulkheads need to be enlarged slightly. I have some scrap 3/4x3/4x125 angle so it made adjusting those holes pretty easy. 

I fitted the longerons to the aft fuselage to check fit. 

Like Mike Bullock’s build page. I too had a slight bit too much of Bulkhead F-711 that kept the longerons from sitting flush with the side skin. I will need to trim those down.

I checked the fit at the back and marked the longeron that I purposely left long to be cut right where the rear tab ends. No edge distance issues here! 

Using the method Mike Bullock used. I isolated the F-711 bulkhead from the horizontal stabilizer mount with a plastic scrapper and used a small flat file to remove about 1/32” of material. Worked very well.

 

Next step I wanted to take a good look at the F-710B angle. I haven’t riveted it yet to the bulkhead as I wanted to take a good look at how all this was going to mesh with everything. I cut and shaped the F-710B angle exactly to the dimensions on the plans and then fitted it to the F-710 bulkhead. Looking at other build logs, I see that there can be quite the issue with getting proper edge distance with the AN3 bolt used to mount the horizontal stabilizer. There’s just not much material to work with there. I can get things more snug. I built the F-710B angle to fit between the tabs of the bulkhead but I could have made it longer. I’m about 1/32” to 1/16” short on both sides if I want it tight to the longerons.

I sat and looked at it for a while. Looked at other builds. Scratched my head. I think I’ll post this dilemma to the Van’s Facebook group and see what more experienced eyes say. 

Finished the platform - 2 hours

I finished up the platform and painted the base so this will be the home for the fuselage for quite a while.  As I waited for the paint to dry, I spent a good part of the day working on the center section getting a bunch of small things done.

Building a platform for the Fuselage - 3 hours

I need to get things ready to join the aft fuselage and the center section. One of the battles that I have is that my garage floor I’ve very uneven and sloped. So placing sawhorses directly on the concrete is not a great way to try to work on the fuselage if I want it straight. I've finally settled on building a semi-permanent platform (that’s level) to place the saw horses on.

Much of the time was spent on cleaning up the garage and getting area ready. I picked up twelve 8’ 2x4’s and went to work. I have the frame built and then levelled the assembly with the laser. All good to go. Just need to put some 3/4” ply down and paint it.

Finished riveting the aft fuselage - 3 hours

My buddy Mike was able to spare some time tonight. We riveted about 8 rivets in 3 hours. That tells you just about how much fun this area is. The curved skin is really tough to rivet and the space for the bucking bar just makes it super tricky.

Getting ready to fit the longerons - 5 hours

Bit of a long day today working with little progress. Some tedious tasks that I need to take care before I can fit the longerons. Firstly I need to set a handful of rivets still in the aft fuselage. These are not that easy to set due to the curvature of the skin. I managed the very rearward set of rivets but for 8 others I need to call my buddy mike for help.

Mike texted me back will come by in a few days so in the mean time I will have to put the fuselage on pause and move onto the longerons. I brought them down from storage and cleco'd them together. One of the tasks that I held off on was to cut the groove into them. I wanted to wait till now to do that rather than do it prior to bending them.

Now that they are celco'd together, I could verify that they are nearly symmetrical. (well one was out about just a tad ~ 1/32 or 1/16"). So I set it all up, and remeasured and sorted the correct length. Now that they are perfect. I marked out the areas I need to cut.


Rough cuts made on the bandsaw, but then all the rest of it was finalized with lots of careful filing.


I left the aft end of the longeron long on purpose. I will mark them for proper edge distance and cut later. I also left them purposely thicker than 0.125". I'll take the thickness down later.