Friday, November 29, 2013

December 1st, 2013 forward fuselage, panel, static port and lines, misc

Finally starting to get a head of steam again, although I realized yesterday when  I was reading over the instructions that I am literally on the last paragraph of the fuselage section and have not yet ordered the finish kit.  I knew I was close but didn't think I was that close.

After letting the paint cure for 3 or 4 days I reassembled it loosely to make sure I hadn't missed anything major.  There are still a couple of things I need to paint (seat backs and braces and the forward brake/fuel line covers) but that will have to wait until we get some warmer weather.

Once I got the panels back in place I did mock up the forward fuse quickly just to sit in it and make airplane noises.


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I got some seat height measurements when I was watching a webinar DJ Lauritzen did on seating (she makes really nice RV seats, Vans demonstrators among them).  She and her husband run Cleaveland Tools.

 Based on her guidance the height will be fine and the rudder pedal location I chose will work as well.

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Once I was done with that I started on the forward fuselage.  Forgot to take any pics of the angles that support the panel.  Pretty straightforward, they just need to be fluted to match the upper curvature on the outboard edges.

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The F7109 plate reinforces the center rib.  There is a roll bar support that bolts between this rib and the forward roll bar for the sliding canopy.

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Reinforcing plate cut to shape but not drilled yet.  This gets match drilled using the center rib as a drilling template.

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Decided to take a break from the forward section to work on the rudder cable exits at the rear.

The adel clamps were a bear to get started.  Finally ended up using a pair of needle nose (note to self - use the forceps next time) and that did the trick.  Hopefully I won't have to mess with these again.

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 I thought about ordering some of the fairings to cover/dress up the exit holes, but ASC wants $16, and there is nothing to them.  I was googling around and found some Sam Buchanan did and shamelessly copied his idea.

This is a lousy picture, but all I have at the moment.  I'll try to get a better one and fix it.

Basically you take some light (I used .020) sheet about 4" long and 2 1/2 to 3" wide, cut it to an arrow shape,  then bent it in the middle.


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Sunday, November 17, 2013

November 17th, 2013 - finish up the empennage, mount avionics tray, paint the interior

Way behind on the updates, and I haven't been able to work on the project much.  Also had a bunch of stuff to do around the house.

I was at a conference in Bethesda a few weeks ago.  It ended up around noon, which gave me a chance to run out to Winchester.  There is an engine shop I'd heard good things about that I wanted to visit.  Got a chance to meet Tom Schweitz at Aero Engines (who seems like a great guy), and he gave me some options re: engines.  I've basically got my pick - he carries both ECI and Superior, and can either build one for me per my specs or I can come up and build it with one of his guys.  Also mid-time are not a problem.  He'd just received a shipment of 19 O-320s from an outfit that was upgrading their Super Cubs to O-360s.  They obviously do a ton of engine work, and seem completely able to do the job, as well as having a good reputation among both the certified and experimental community.

Basically in the last few weeks I've finished up as much as I can on the empennage, mounted the Van's avionics tray in the fuse and painted the interior.

Last thing to do on the empennage was to mount the aft tie down.  It's riveted to the forward side of the aftmost bulkhead.  I made up a drilling guide/jig from some scrap aluminum so I could get everything lined up.  There is no way (that I have anyway) to drill from the tie down bar into the bulkhead.  It's too tight.  There is also no good way to clamp the tie down bar in that position.

Basically what I did was lay out the tie down bar, drilled it on the drill press, then match drilled the drilling jig, the laid that out on the aft bulkhead, then drilled the bulkhead.  Once I had both drilled, I clecoed the tie down bar in place and cleaned the holes up.  I drilled everything undersize (#40) so the alignment would be no problem.

Here's the drilling jig getting aligned with the bulkhead.

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I match drilled the bulkhead using the jig, then clecoed the tie down bar (which was already drilled) into place.

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Inside view of the tie down bar clecoed in place.  Tight fit.


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Once I was done with that, I had to match drill the lower vertical stab spar to the aft bulkhead.  This will be bolted in place later.  These holes go through the bulkhead and the tie down bar as well.

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Starting to work on the avionics tray.  Van's sells a AHARS (or ADAHARS) tray that fits right behind the aft baggage wall.  This gets it clear of magnetic interference as much as possible.  I'm using manual trim, so the trim cable is a bit in the way - I'm going to install a nutplate in the elevator horn rib and clamp the trim cable with an adel clamp.

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Since there is no way to dimple, I used my tight fit dimple kit I got from Cleaveland.  It works pretty well if you pull it a couple of times.  They give you copper finishing nails, but I found that some stainless vinyl trim nails work much better.  I can do 2 holes before they are stretched too much and break.

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Holes in aft bottom skin all dimpled.


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Everything riveted together as mush a possible and test fit.  The tray is leveled so that the AHARS has a good attitude reference.

I won't permanently rivet it til I get the actual unit.  This one is drilled for both Garmin and one other manufacturer.  I'm planning on using Dynon, so I'll install the nut plates when I have the actual AHARS and can accurately lay it out.

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Time to paint the interior since it's wide open, and this is the easiest time.  I haven't decided if I will fabric the interior or not.  I tried several paints, shopped around, looked at a lot of ideas (textured, Zolatone, Stewart systems, etc.)   I finally settled on some Rustoleum I found.  It's pretty durable, and the color is a nice contrast with the Van's powder coat (it's Becca approved!).

I played with it and was able to get a slightly textured finish (which is what I was looking for - didn't want it to have too much glare).

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I spent days sanding, hitting it with scotch brite pads, , cleaning and masking.

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More masking.  I will only paint forward up to just above the upper stiffener.  The panel will cover everything else, and I don't want to add more weight than I need.

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Aft cockpit all masked.

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In the middle of painting.

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More or less finished with the panels lightly screwed into place.  Pretty happy with how it came out.

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Aft side.  It won't win a Lindy, but it will be more than adequate for me.  Just hope it holds up well.  If not, a fabric kit from Flightline or  DJ @ Cleavelend is always an option.

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Sunday, October 6, 2013

October 6th, 2013 - horizontal stab, trim system

I haven't had time to do any updates lately, although I have been getting some work done on the plane.

I just realized I hit the one year anniversary of working on the fuse.  I'd hoped it would go more quickly, but there have been too many side things crop up.  Sometimes life gets in the way - you just keep plugging along as you get time.

In the last few weeks I've installed the manual trim cable (which is a vernier unit similar to a mixture control, but the rapid movement part is disabled), mounted the horizontal stab and match drilled it to the fuse, drilled the elevator horns, fabbed and mounted the elevator counterweights on some other miscellaneous stuff related to the empennage.

First thing to do was install the elevator bellcrank.  It's mounted between a vertical brace and a floor rib right behind the baggage wall.

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The bellcrank has a bearing in the center and one arm is longer than the other.  Long arm hooks to the elevator pushrod, the short end connects to the pushrod that goes forward to the control yoke.  Rod end bearings are attached at the end of each arm to make everything very smooth.

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The long (and fat) elevator pushrod is attached to the rod end bearing and continues aft through a hole in the aft bulkhead where it will attach to the elevator horns.


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Also decided to run the rudder cables since this seemed like a good time.  I'd heard of folks having problems with these, but they were easily inserted by hand if I popped out the nylon bushings.  There were a few tight (or closed) spots where I couldn't pop out the bushings, and even then it wasn't terribly hard to work the end of the cable through the bushing.

I used a long grabber tool to pull the cable through the already attached baggage compartment wall.  I pulled a small rope through, attached the rope to the cable, then used it to pull the cable through.


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Aft end of the rudder cable.  It will be clamped to the aft fuse skin using an Adel clamp where the dimpled hole in the skin is.

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This is another shot of how I pulled the cable through the sealed baggage wall.

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Next I installed the trim cable.  I had it pulled all the way aft before I realized I'd forgotten to thread it through the attach plate.  Kicked myself a second, then realized it had to come apart somehow.

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Thankfully it does.  If you open up the vernier end, this is what is inside.  Similar to a brake/clutch cable on a motorcycle.  Slide the ball out of the socket and it comes right apart.  Whew!


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The aft end of the trim cable is a bear to get through the horizontal stab structure - some very tight corners and bends, and the cable is pretty stiff.

I ended up using my tubing bender spring trick to thread it through all the holes.  Worked very well.


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I'd forgotten (or decided to skip) the installation of the elevator up stop.  I needed it, so I fabbed it up and drilled/riveted/bolted it in.  It gets primed and riveted, just forgot to take a picture at that point.

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The trim cable attaches to a nut welded on to a small square of sheet steel.  That gets riveted to the trim access cover on the bottom of the left elevator.  I'm laying it out for drilling here.

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Once it's drilled, you screw the nut on to the trim cable, cleco that to the trim access cover, then work all that into place and screw it down.

I forgot to take a shot of it, but there is a clevis that threads on to the end of the trim cable that attaches to the actuator tab on the bottom of the trim tab.

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Here's everything in place.  Discovered something very handy when I was working out all the dimensions and where to set everything to get it centered.

The vernier cable (mine at least) is exactly 10 turns stop to stop.  So by going 5 full turns from either stop, I know the cable is dead centered.  I should be able to use that to establish some number of turns from center to set takeoff trim.

I'd wondered how it was done - this seems like it will be very easy to do.

Next thing to check was the trim limits.  This is full up (I know the tab is down, but that's how you get up elevator).

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Full down trim.  Both up and down worked out to almost exactly 35 degrees.  This is more than Van's specifies.  I may either have to limit it physically or just not use it all.  

In practice, you only use what you actually need anyway, so I can't imagine too much would be a problem.  

The autopilot I will use is not trim based, so that's not an issue either.


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Next thing to work on was the vertical stab.  I spent more than 2 hours measuring, clamping, re-measuring, plumbing with a plumb bob, measuring some more..... I did not want to have either this or the horizontal stab wrong.  Makes for a hard to trim plane, which I do not want.

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After measuring what must have been 50 times at least, I finally drilled the holes through the F912D elevator stop that establish the vertical stab height as well as setting vertical.

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Next is to match drill the forward vertical stab spar to the offset attach plate.  It's offset to account for P-factor I suspect.  I drew center marks on the spar and plate to make sure I got it square.  It's pretty disconcerting to see how far it's offset, although truthfully it's not that much, but you can definitely see it when you look at it looking aft.

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At this point I haven't finished final mounting the vertical stab - I just worked on aligning the rear spar of the vertical stab dead straight, then worked with the rod end bearings (there are 3) in the rudder to line them all up with the hinges as well as make sure the gap at the counterweight arm was even.  Time to call it a night.

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Tuesday, September 17, 2013

Sept 15th, 2013 - control yoke, elevator pushrod, mount the stab


Kind of on again/off again the last couple of weeks.  We people coming by to do some work on the house that required crawl space access, so I'd get something started, then have to take everything down because it was in the way, then put it back.

A lot like building a plane in fact - put it together, take it apart...

Anyway, got the control yoke done, put together the forward elevator pushrod, and today got the horizontal stab drilled to the aft deck.  After that I went flying since it was such a nice afternoon.  Lovely day to fly - the haze is more or less gone so you can actually see again instead of our usual summer MVFR we get on a "clear" day.

There is no way to mount the yoke assembly into the fuse without taking it apart.  When the center section is done, Vans has you cut a section out of the two center seat ribs and fabricate some doublers with nutplates so they are removable.  This helps to facilitate installing the yoke later.  It has to be taken apart, threaded through the forward lightening holes in the seat ribs, then the bracket on each side is bolted to the angle support which is in turn bolted to the spar carrythrough.

Tight fit.


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This is where the bracket bolts to the attach angles.  The angles have bearing inserts so the movement is very smooth.  Washers are used to remove the slack so there is no side play.

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After googling around and thinking about it, it seemed much better to me to attach all the rod end bearings to the various parts ahead of time so I don't have to try to do that in this very tight spot - trying to hold the rod end bearing and a couple of washers and then trying to thread a bolt through all that, all while having it inside this tight space.

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Each stick has a bushing that goes inside the weldment, then the whole thing is a snug fit (they come a bit over size and you grind them to fit) into the bracket.  Then an AN3 bolt with washer and lock nut to secure it.  This is the left stick.  You can see the hex rod that connects the two sticks together below.  The aileron pushrods attach to the outboard side of each stick.

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After several hours of contortions, double checking, torquing and torque sealing the nuts, this is the final result.  The right stick is a press fit and is removable.  The left is not.  I'm hoping I don't have to take them out again.  We'll see.

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Next step is to start working on the horizontal stab and elevators.  The fuse is levelled, then the stab is laid across the aft deck.

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Measurements are taken from a common point on the firewall to a common rivet (I used the center indentation on the aftmost outboard rivet on each side).  Even though everything is clamped down and as square as possible, there is just enough play to work until everything is identical.

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I must have remeasured, reclamped and measured again 10 or 15 times at least.

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Funny, after doing all that, I decided to drill the elevator horns first, so I took it all off and worked on that for a while.  There is a bolt through a caged bearing at the top of the horns that creates a common bearing for the left and right elevators.

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Here's a closeup of the two horns.  You can't quite make out the center bearing.

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Once that was done it was back to the horizontal stab and measuring a zillion times again.  Once I had it as good as I could get it (each side is shimmed 1/8" since there will be shims underneath to set the angle of incidence), I drilled the attach angles to the longerons and support angles (there is about 1/4" of aluminum bar and angle under the aft deck that spans the fuselage side to side.

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Van has you use an 11/32" drill bit to shim the aft stabilizer spar up to the correct height to set the correct angle of incidence (0 degrees in this case).

The two vertical bars will be drilled shortly for the aft attach bolts.

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