Project: BuckRV-8   -  
            Listing for Category : fuselage
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Builder Name:Buck Wyndham   -  
Project:   Vans - RV-8   -   VIEW REPORTS
Total Hours:3907.05
Start/Last Date:Jan 08, 2002 - No Finish Date
Engine:AeroSport Power IO-375-M1S
Propeller:Whirlwind 330-3B/72H-73 3-blade CS
Panel:G3X, G5, GTN650, GTR20, GTX45R, GMA245, GMC507
 
Friendly URL: https://eaabuilderslog.org?s=BuckRV-8

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Apr 01, 2024     Flap pushrod gap seals - (1.8 hours)       Category: Fuselage
Fabricated the other flap pushrod seal, including the retaining plate and the foam seal.

Both seals are now ready for final installation when the floorboards are installed.


 
Mar 24, 2024     Flap pushrod gap seals - (0.6 hour)       Category: Fuselage
Continued work on the flap rod boots:

1. Used a piece of see-through plastic to draw a template around the pushrod hole in the floorboard, then used this to cut a piece of 0.025" aluminum. This will be the retaining plate for the foam. The plate will be kept in place by one of the #8 floorboard screws and two other #6 screws/nuts.

2, Drilled the attach holes.

3. Cut out the pushrod hole and several other holes -- and I made sure it they had plenty of intentional ragged edges. (These rough edges will retain the foam under the plate.)

4. Cut the foam to shape.

5. Used a hot soldering iron to create the screw holes through the foam.


 
Mar 19, 2024     Flap rod boots; Interior nutplate prep - (2.1 hours)       Category: Fuselage
1: Since the flap actuator rods go right through a big holes in the floor, I want to prevent too much cold air from getting in. I began construction of a pair of boots for the flap rods. Each one will be made from a foam painter's brush, with a capture plate made of scrap aluminum. The rods will slide through holes in the foam.

2. To speed up the final assembly of the airplane later on, I have begun running a tap through all the painted nutplates in the floorboards, side panel pieces, and any other interior piece containing a nutplate. Today, I did all the baggage compartment pieces, along with the aft floorboards.


 
Mar 04, 2024     Exhaust ramp polishing - (1.7 hours)       Category: Fuselage
The paint scheme for the airplane is pretty well set in stone, but I've been thinking about one particular detail for a while -- how to deal with the exhaust ramp under the belly. It will be subject to a lot of heat, and I can see the potential for long-term heat-damage to any paint that's applied. So today, I decided to polish it.

I masked off the panel, then used Eagle One Nevr-Dull wadding polish to shine it up. It came out looking nice, but I wonder how quickly it will tarnish, and how much work it will be to keep it looking good. At least I didn't decide to polish the entire airplane.


 
Feb 19, 2024     Flap fairings - (1.6 hours)       Category: Fuselage
1. Sanded all of yesterday's filler in the flap fairing rivets.
2. Shot a quick coat of primer on each side to check if any more sanding needs to be done. (It does!)


 
Feb 18, 2024     Final-shaping of R flap fairing; Attach R fairing; Fill rivet heads - (2 hours)       Category: Fuselage
1. Sanded both sides of my special R flap fairing to get it as thin and unnoticeable as possible.
2. Riveted R flap fairing to fuselage.
3. Filled all pull-rivet heads.


 
Feb 17, 2024     R flap fairing prep - (0.8 hour)       Category: Fuselage
1. Carefully sanded both sides of the R flap fairing and primed it.
2. Clecoed and test-fit the fairing, and decided to sand the back side a bit more.
3, Removed the fairing, sanded the back side mostly flat, then re-primed it.


 
Feb 17, 2024     Empennage fairings -- nutplates, attach holes, and glass work - (1.1 hours)       Category: Fuselage
1. After much thought and experimentation, I figured out a way to attach four nutplates that will hold the forward end of the upper empennage fairing in place. I'd already ruled out rivnuts because they would cause the fairing to not lay flat on the fuselage skin. I've wanted to use ClickBond nutplates on the inside of the fuselage skin, but the area is almost inaccessible to human arms. Today, I realized that I could grab the rubber stem of the ClickBond plates with a 3-foot pickup tool, feed the tool through a narrow gap in the aft fuselage bulkhead, push the stem through the screw hole, and have a friend pull the adhesive side of the nutplate into position. With the help of my friend Jim, we did exactly that, and it worked great.

2. Opened up and tapped the two fuselage holes for the front end of the lower fairing.

3. Opened up and deburred all the remaining attach holes for the fairings.

4. Sanded off the various blobs of resin that managed to land on the tail and aft fuselage skins during the construction of the empennage fairings.

4. Sanded off spots of primer from the lower empennage fairings and filled some divots with filler.


 
Feb 16, 2024     Flap fairing prep and attachment - (0.95 hour)       Category: Fuselage
1. Carefully sanded the backside of my "special" R flap fairing to make it as flat as I possibly could without compromising its appearance or structural strength.
2. Clecoed the R flap fairing in place. I think it will look OK (although *I* will be able to see its flaws every time I look at it. Oh well.
3. Riveted the L flap fairing onto the fuselage. It looks perfect.


 
Feb 09, 2024     R flap fairing - sanding and priming - (1 hour)       Category: Fuselage
My R flap fairing is quite special in its construction, and today I sanded and primed it so it will be relatively unnoticeable once it's riveted in place (I hope...)


 
Nov 11, 2023     Flap fairing - (0.4 hour)       Category: Fuselage
Sanded filler on flap fairing.


 
Nov 06, 2023     Flap fairing - (0.6 hour)       Category: Fuselage
Sanded and filled the filler on the flap fairing notch.


 
Oct 10, 2023     Flap fairing modification - (1.45 hours)       Category: Fuselage
1. I was sanding yesterday's filler some more, when the filler piece popped out in my hand. I think I know exactly why it happened, so I decided to try again.
2. Sanded and prepped the fairing.
3. Mixed up some thick flox, and applied it to the notch, leaving a much wider margin for it to bond to this time.


 
Oct 07, 2023     Flap fairing modification - (0.5 hour)       Category: Fuselage
Sanded the repair to the flap fairing and shot it with a coat of primer to assess how much filler, if any, is needed.


 
Oct 06, 2023     Flap fairing modification - (0.5 hour)       Category: Fuselage
1. Removed the R wing flap fairing.
2. Sanded the previously-made modification (which involved making a slot, slightly bending the fairing, then using flox to fill the slot.)


 
Mar 27, 2023     Top skin rivet line fill (R) - (0.6 hour)       Category: Fuselage
1. Masked, sanded, cleaned, and primed the filled rivets on the right forward top skin.


 
Mar 26, 2023     Top skin rivet line fill (L) - (0.7 hour)       Category: Fuselage
1. Sanded the filler on the left-hand lines of rivets on the top skin.
2. Cleaned and primed them.


 
Mar 05, 2023     Fuselage blind rivet sanding - (1.5 hours)       Category: Fuselage
With some extra time I had this evening, I began the process of preparing some of the lines of blind rivets on the top forward fuselage for paint. A few months ago, I'd hastily slapped some filler on these rivets and quickly sanded them, knowing I'd revisit them later.

1. First, I masked off the area around the rivets with blue tape to keep the sanding localized.
2. Used a 220-grit sanding block to sand the rivets and the area around them in order to remove as much of the filler around the head of each rivet as possible.
3. Vacuumed and cleaned up the sanded area with acetone.
4. Primed the area with self-etching primer

This process seemed to work pretty well, and it appears it will work well of the remainder of the areas.


 
Jan 16, 2023     Elevator pushrod access/inspection covers - (5.1 hours)       Category: Fuselage
Began fabricating a pair of custom access covers that will cover not only the standard access door for the elevator pushrod attach point, but also extends upward to cover the area the empennage/fuselage fairing would have covered. The reason the fairing isn't going to cover this area is because I'm going to cut it off. This will make the fairing easier to remove and replace.

1. Fitted the stock access covers.
2. Cut out pieces of stiff cardboard and laid them above the covers. Marked and trimmed them to fit the space required.
3. Laid out cut lines on a sheet of 0.025" aluminum sheet.
4. Cut out, trimmed, filed and sanded the covers.
5. Drilled the four lower attach holes using the stock covers as drill guides.
6. Began marking the new covers for the next trim line that will be required, the curved openings where the elevator control linkage will pass.


 
Nov 27, 2022     Access door - (0.6 hour)       Category: Fuselage
Trimmed the fuel filter access hatch on the forward fuselage to create a consistent gap for painting.


 
Sep 13, 2022     Flap fairing - (0.3 hour)       Category: Fuselage
Began riveting on the left flap fairing, but I realized I didn't have enough of the proper rivets, nor could I drive and buck the rest of the rivets myself, so I moved onto something else.


 
Sep 08, 2022     Baggage door; Top skin rivets; R side vertical channel cap; Misc. - (4 hours)       Category: Fuselage
Did a bunch of miscellaneous projects today:

1. Prepped and painted the baggage door hinge support channel and spacer.

2. Touched up the paint on numerous areas in the baggage compartment and cockpit.

3. Organized Vans drawings and pulled spare kit parts off the hangar shelves to clean the place up a bit.

4. Filled the hollow stems of any Cherry Max rivets I could find on the airplane. [PHOTO]

5. Riveted the remaining R side vertical channel cap. The left one will be accomplished after I verify the rear seat throttle pushrod has enough clearance, and after I receive my shipment of more LPS4-3 rivets. [PHOTO]

6. Worked on getting the vertical stabilizer cap to fit better.

7. Studied the construction steps for the baggage door.


 
Sep 07, 2022     Top skin; Skybolt plates; Baggage door - (4.9 hours)       Category: Fuselage
1. Riveted on all but the lower three Skybolt fasteners on each side. These will be added later, after I trim the cowling halves.

2. Assembled and marked the forward baggage door hinge support channel, spacer, and hinge.

3. Drilled out the nutplate near the top center of the avionics door bulkhead that interferes with the baggage door hinge support. I will have to rivet the support channel to the bulkhead using new holes, carefully avoiding the old screw hole and nutplate holes.

4. Clamped the hinge support parts into position, then drilled and clecoed them, using the prepunched holes in the skin as a drill-guide. Also drilled the four rivets holes on the ends of the support channel (two through the avionics bulkhead and two through the firewall).

5. Marked the baggage door flange for trimming to allow the hinge to pass as the door opens.

6. Disassembled all the parts, then deburred them.

7. Countersunk the spacer and dimpled the top skin.

8. Sanded, cleaned, and primed the spacer and hinge support channel.


 
Sep 06, 2022     Top skin; Skybolt fasteners - (6.2 hours)       Category: Fuselage
1. Completed most of the riveting of the top skin -- everything except for the firewall flange. I unapologetically ended up using quite a lot of Cherry Max rivets... basically anyplace where I couldn't easily get access to the backside of the skin with a small bucking bar.

2. Used a rivet shaving bit to smooth out a couple of rivet stems that weren't totally flush.

3. Riveted the skin / rollbar connector rib into place.

4. Removed the Skybolt plates and countersunk the fastener rivet holes.

5. Positioned and drilled the Skybolt plates under the firewall skin flange, one at a time, using the skin holes as a drill guide. I used a 0.24" flange reveal distance for the plates, in accordance with the manufacturer's suggestion.

6. Removed all the Skybolt plates and deburred them, then re-clecoed them into position. (BTW, I left off the bottom three plates on each side, just so I can tweak their spacing slightly after I trim the top and bottom cowlings. I want to make sure the bottom Skybolt fastener on the firewall is directly in line with the horizontal row on the cowling split line.)


 
Sep 05, 2022     Top skin - (5.5 hours)       Category: Fuselage
Made some good progress on the top skin today:

1. Countersunk the top/forward skin spacer strip.

2. Finished splicing all the power and ground wires for the cockpit lighting.

3. Clecoed on the top skin (every hole).

4. Began riveting on the the skin, starting top-center of the aft bulkhead (the instrument panel), and working alternately down the sides. I used solid rivets as long as I could reasonably reach inside the EFIS hole with a small, tungsten bucking bar. As soon as something behind the panel got in my way, I switched to CR3214-4-4 Cherry Max rivets, driving them with my awesome new Milwaukee M12 cordless blind-rivet tool. (I long ago decided that the rivets' price of $0.54 each is well worth it when I'm riveting alone. The tool makes setting them a total non-event.) By the end of the evening, I was almost done with riveting the aft bulkhead.


 
Sep 04, 2022     Misc. prep for top skin attach - (4.3 hours)       Category: Fuselage
Continued finishing up the last tasks required before riveting on the top skin:

1. Tightened and torque-sealed three of the last five fuel connections on the fuel pump assembly. The last two connections will be made once the rudder pedal assembly is installed.

2. Marked the Skybolt plates, and marked their centerlines on the firewall, so I can position them again later. Removed the plates.

3. Deburred all holes on the firewall flange.

4, I began clecoing the skin on, but I discovered that when I bolted the back of the radio rack in place, I'd "locked" the instrument panel in a way that meant the top attach angle could not flex at all. This meant that the fit of the top skin became difficult because the aft row of attach holes didn't line up any more. After thinking about it for a while, I decided to un-bolt the radio rack from the Z-channel, and let it "float." My rationale is that the rack sits securely on the Z-channel, it can't move fore/aft more than about 1/16", nor can it move left-right at all. In theory, it could move up down about 1/8", but the rack is securely attached at it front end, and it's really not going to go anywhere, even under a negative 2G load. I lightly twisted some safety wire through the bolt holes and called it satisfactory.

5. Clecoed the left side of the skin onto the fuselage and checked the fit again. The panel floats perfectly. I shoved a folded-up moving blanket under the right side of the skin, giving me some room to work on the final electrical wiring connections.

6. Found that the four wires for the recently-mounted LED lights strips were slightly too thick to pass through the plastic hole grommet I'd previously installed on the panel, so I removed the grommet, drilled the hole to the next-larger grommet size, and re-installed a new grommet.

7. Labeled all the cockpit lighting wires, trimmed them, spliced a couple of them with longer leads, and prepped them for making the final connections to the lighting controller and ground leads..


 
Sep 03, 2022     Misc. prep for top skin: Avionics door, rack mount, wiring, gear towers, air vent - (7.2 hours)       Category: Fuselage
Spent the whole day preparing and installing various items before I rivet the top skin, since these tasks would all be very difficult to perform after the fact.

1. Marked and cut the notch in the avionics access door that will allow the baggage door hinge channel to be mounted. I may have to trim a little bit more from the door later, but for now, it's pretty close.

2. Drilled the two attach holes in the angles that secure the back end of the avionics rack stack to the supporting Z-crossbar. Used #8 screws and nuts to fasten the rack.

3. I probably didn't need to do this, but I spent over an hour adding lacing cord and the occasional zip tie to the wiring behind the panel, just to clean it up as much as possible.

4. Prepped the six lighting grounds and power leads that I will need to connect and tie up once the top skin is set into position. I did not install the avionics fan or the small GPS antenna to the glareshield, because I'll be able to do those tasks much later, through the large EFIS hole in the panel.

5. Installed a headset hanger on the right gear tower cover.

6. Secured and tie-wrapped numerous wires inside the gear towers. Secured the L fuel tank vent line inside the left tower.

7. Attached the left and right gear tower covers.

8. Installed (but did not tighten) two hard fuel lines (one from the fuel filter to the fuel pump, and the other from the fuel selector to the fuel pump.)

9. Installed the red and white LED lighting strips on the underside of the glareshield. In addition to the adhesive strip on each one, I added a bead of clear E6000 adhesive to keep them in place permanently. Heat-shrinked the four power wires to keep them looking tidy. They will pass though a small hole on the right side of the instrument panel (already drilled and grommeted.)

10. Measured, cut, and installed the SCAT tube from the left NACA scoop to the air vent on the instrument panel.



 
Sep 02, 2022     Top skin prep; Aft bulkhead paint - (3.5 hours)       Category: Fuselage
1. Deburred and dimpled the edges of the top skin

2. Dimpled the attach holes in the skin rib that attaches to the roll-bar.

3. Measured and prepped the LED panel light strips that will go on the underside of the glareshield.

4. Polished the top sides of the spacer strips under the top skin. (These are the front baggage compartment edge strips that support the baggage door, and they will be visible when the door is open.

5. Countersunk a few remaining skin attach holes along the firewall.

6. Sprayed a second coat of paint on the entire aft cockpit bulkhead.


 
Sep 01, 2022     Top skin rib; Touchup paint; Flap fairing - (4.2 hours)       Category: Fuselage
I'm really trying to ramp-up my work output during my vacation. Today I got a lot done!

1. Finished drilling, then primed and painted the two ribs that attach the top skin to the roll-bar. They are ready to install.

2. Removed the top skin.

3. In preparation for attaching the top skin, I inspected the forward baggage area and found some paint that had gotten chipped, especially on the aft wall of the bay. So I reacquainted myself with my old airbrush and mini compressor, then mixed up a half-ounce of Ford Tractor Gray paint, reducer, and hardener. I repaired the chipped areas, then used the rest of the paint to touch up the bulkhead behind the rear seat, an area on the top longeron next to the instrument panel, and several small areas in the cockpits. The airbrush is a perfect tool for this job, because it's accurate and delivers extremely small quantities of paint, which makes it easy to spot-treat paint chips in an unobtrusive way.

4. Cleaned and clecoed the left flap fairing into position on the fuselage, in preparation for riveting.


 
Aug 31, 2022     Canopy bar / top skin support plates - (1.1 hours)       Category: Fuselage
1. Fit , drilled, and clecoed the two attachment plates that tie the top skin to the main rollbar. They each required some massaging and tweaking to fit right. Next, they will be drilled to the rollbar, then removed and painted black.


 
Jun 18, 2022     Headset wire clamps - (0.6 hour)       Category: Fuselage
1. Added an Adel clamp under each of the right armrests to better support the RCP headseat jack cable bundles.


 
Mar 18, 2022     Top skin - (0.4 hour)       Category: Fuselage
Using a strap duplicator tool, I match-drilled the final seven holes in the left edge of the top skin. (These are the large Dash-4 holes).


 
Mar 17, 2022     Top skin - (1.0 hour)       Category: Fuselage
Drilled and clecoed the remainder of the holes in the top skin (all except for seven of them, which must be match-drilled with a strap duplicator.)


 
Mar 16, 2022     Flap actuator re-do; Top skin - (3 hours)       Category: Fuselage
1. I decided to disassemble and perfect the installation of the flap actuator arm. First, I removed the upper attach angle and removed all the hardware. Then I cut the safety wire and removed the cupped washers I'd previously installed around the rod end. I replaced these with flat washers, then reassembled everything using new hardware, lubricated the rod end, and re-safetied it in accordance with the applicable Vans Service Bulletin. Then I installed the flap actuator cover using new #6 screws with nylon washers to prevent scratching the cover.

2. Clecoed the top skin in place and clamped it tight to the fuselage using a band clamp. Began drilling and clecoing the skin edges to the fuselage.


 
Mar 15, 2022     Gear fairings; Top skin - (2.6 hours)       Category: Fuselage
Did some miscellaneous projects this evening:

1. Filed, shaped, and sanded the edges and inside surfaces of the upper gear fairings.

2. Clecoed the top skin to the fuselage to check its fit and mark a few specifics about the rivets I'll be using to fasten it on. Used my new Cleaveland Tool edge-rolling tool to pre-bend the lower edges of the skin so they will lay flat after being riveted. (I had to make several progressive passes to get the results I wanted.)

3. Marked the underside of the glareshield portion of the top skin for the location of the two LED strip lights.

4. I noticed that the inside color of the top skin is slightly different from the other gray in the fuselage -- despite the fact that it's supposed to be the same color. Perhaps the color specifications have changed in the 10 years between the two paint jobs, or perhaps it just faded. I'll have to decide if I want to repaint it, or just let it slide.


 
Mar 14, 2022     Fuel selector panel - (1.8 hours)       Category: Fuselage
1. Did some more filing and sanding on the fuel selector panel, then fitted it and secured it with black stainless #8 screws.

2. Fitted the fuel selector plate and handle. (I initially used socket-head cap screws for the plate, but they were too tall and they interfered with the free travel of the selector handle, so I changed them out for stainless pan-head screws that are about 1/16" shorter.

This completes the installation on the fuel selector panel, except for some minor paint touchups that will be needed later.

3. Changed out a steel clamp on one of the exhaust hangers. This will allow the cabin heat able to pass through this area better.


 
Mar 10, 2022     Fuel selector panel - (1.1 hours)       Category: Fuselage
1. Cleaned under the fuel panel. Vacuumed out all chips, dust, washers, etc, that might have been under there.

2. Performed a final inspection of the fuel lines and wires under the selector panel.

3. Attached the fuel selector mount to the fuselage structure.

4. Attached the three electrical connectors under the panel.

5. Prepped the selector cover panel. (It appears it will have to be filed a bit on the left side.)


 
Feb 23, 2022     Top skin; Aft wiring; Throttle grip; Flap switch wiring - (3.7 hours)       Category: Fuselage
Today I did a bunch of small miscellaneous projects:

1. Got the top skin back from my painter friend, Jim. He did a great job painting the inside of the skin using the same Ford Tractor Gray color I used for the rest of the inside of the fuselage.
2. Added a half-dozen zip-tie bases inside the aft fuselage, and secured the remainder of the wiring there.
3. Since the JB Weld around the smoke switch had fully set, I painted it flat black. It looks like it will match the grip really well.
4. Prepped and labeled the backside of the flap switch, in preparation for installation.
5. Trimmed and stripped the five flap switch wires and installed the ring terminals on the wires.


 
Feb 09, 2022     Placards - (2.2 hours)       Category: Fuselage
Today I worked on installing a couple of necessary placards.

1. First, I marked and drilled the holes that will mount the new N-number placard, to cover the old N-number. I really liked the way the screen-printing looked on the panel, but I like the new N-number even more... I'll install the new placard once I receive the cool low-profile socket-head cap screws I ordered from McMaster-Carr.

2. The second project was the "Passenger Warning" placard, which I mounted on the right side wall, between the seats. (The protective plastic will come off later.)


 
Feb 04, 2022     Sidewall measuring - (0.3 hour)       Category: Fuselage
Installed the flap actuator cover. I am having custom upholstery made, so I needed to measure the resulting part of the sidewall in the rear cockpit that is not taken up by the actuator cover.


 
Feb 03, 2022     Cowl prep; Aft throttle quadrant; Top skin dimpling - (2.4 hours)       Category: Fuselage
1. Began planning the cowling installation by reading the details about the process, including how I will install the Skybolt fasteners. (The Skybolt instructions are really terrible, and it makes me want to rewrite their manual for them…)

Fabricated a non-scratch marking tool so that I could mark a Sharpie line on the fuselage skin, exactly 2" aft of the firewall edge. This will help me make some measurements on the cowl to determine where to cut it off later. I made the tool from a plastic parts-drawer separator, a long AN426 rivet, and some duct tape, with a small hole drilled 2”away from the rivet where I could insert a fine-tip Sharpie marker. I marked the line all the way around the firewall.

2. Test-assembled the rear cockpit throttle quadrant. Made several hardware adjustments from the plans. (For instance, I used a nylon washer underneath the main bolt, and I used a shorter bolt than what Vans called out.) Painted the head of the main attachment bolt flat black to match all the other cockpit hardware.

3. With help from my friend Jim, I dimpled two rows of holes on the top skin -- the row along the top of the instrument panel, and the row on the avionics bulkhead forward of it. [ No photo yet.]


 
Feb 03, 2022     Top skin and bulkheads - dimple/countersink - (2.1 hours)       Category: Fuselage
Began prepping the top skin and its underlying bulkheads for riveting:

1. Dimpled all the holes in the flange at the top of the instrument panel.
2. Countersunk all the holes in the flange at the top of the "avionics bulkhead."
3. Began dimpling the corresponding holes in the top skin. (I did all the ones that laid flat on the table. I'll do the others when I have help holding the skin up a bit.)


 
Jan 25, 2022     Top skin preparation - (0.9 hour)       Category: Fuselage
1. Marked top skin for dimpling. (I'm not going to dimple the holes along the sides until I match-drill them with the underlying structure.)

2.. Since it hasn't been used in a long time, I had to do some repairs to my dimpling table, which took some abuse while it was in storage. I cut several lengths of 2x4s and screwed them to the bottom of the table to replace the ones that somehow disappeared. I also cleaned and lubricated the C-frame dimpler, then installed it into the table.


 
Jan 19, 2022     Instrument panel bracket rivets - (0.5 hour)       Category: Fuselage
Riveted the four rivets (two on each side) that hold the side instrument panel brackets to the skin.


 
Jan 18, 2022     Control cables and rear throttle - (3.2 hours)       Category: Fuselage
1. I spent a lot of time trying to figure out where to drill the final two holes through the left gear tower. These two holes will be for the Alternate Air control and the Oil Shutter control. Optimally, I'd like these two knobs to be right next to each other, with the Oil Cooler shutter knob in full view of the pilot and probably closer to his left leg than the other knob, since it will be used much more often. With that goal, plus the limitations of the knob size (each will be 1" in diameter), the items inside the gear tower (fuel vent line, brake line, and lots of wires), the location of the fuel selector, the location of the fuel filter on the front side of the gear tower, the location of the air vent SCAT tube, the location of the already-drilled firewall pass-throughs, and the fact that the McFarlane cables have a 6" non-bending section just behind the knob control, I made a template and set to work scouting locations. After over two hours of investigation and inspection, I think I've located the one location this setup might work -- outboard, below the throttle quadrant, and with the two knobs stacked vertically. It will be very close.

I have a couple of other options: a). Use a cheap Bowden cable for one or both of these items. This would allow me to bend the cable inside the gear tower and exit in a different location other than directly in line with the knob. This would be super helpful for the installation process, but I would have to make some kind of label/placard next to each knob, which is a look I was trying to avoid. (The McFarlane cables are custom engraved right on the knob, and they're really great-looking), b). I could put the knobs in grossly different locations on the gear tower -- which, again, is an incohesive look I was trying to avoid. I'm going to call McFarlane tomorrow and see if they have any solutions, or different models of cable that might bend closer to the knob.

In the meantime, I set about trying to get something -- anything -- done that would be productive.

2. Took measurements for the two remaining cables. They will be ordered as soon as I talk to McFarlane.

3. After consulting with quite a few RV owners, I decided that I do not need my prop lever to get full-range of motion all the way to the low-RPM stop on the governor. As long as it hits the high-RPM (flat pitch) stop and doesn't hit the quadrant stop first, I am OK with not making it all the way back to low-RPM (high-pitch), since there are only two times anyone ever pulls the blue knob ALL the way back: The runup on the ground, and possibly in the event of an engine failure to decrease the descent rate. Most of the time in cruise, the blue lever is within 1.5 inches of the forward stop, and that results in ~2400 RPM. I am willing to lose a bit of reduction capability, rather than having to rebuild the quadrant or somehow ream-out and shim the cable holder. Who cruises at 1900 RPM or less? With all that in mind, I marked and drilled the final hole in the prop control arm. Done.

4. Installed the white nylon throttle sliders for the rear cockpit throttle slot. Once the controls are ready to go in for good, I'll add the engraved placard that covers the rivets.


 
Jan 17, 2022     Brake system updates - (2.1 hours)       Category: Fuselage
Removed both brake master cylinders and brake fluid reservoirs, removed all AN fittings. Cleaned all remnants of old sealant because it had been on there a while and because I have learned there are better sealants than what I used the first time. Re-installed all AN fittings using Loctite 567 sealant. Clocked all fittings and the two fluid reservoirs. Replaced AN3 bolts and cotter pins as necessary. Cleaned up all hardware. Lubricated slide tube.


 
Dec 21, 2021     Top skin priming; GPS coax pass-through - (1.4 hours)       Category: Fuselage
Did a couple of miscellaneous jobs today:

1. Scuffed, cleaned and primed the underside of the top skin, in preparation for painting it next week.
2. Permanently installed the firewall passthroughs for the three GPS/XM antenna coax cables. I used gray, 1000-degree sealant in addition to the stainless steel grommet caps.
3. Measured for, and ordered, a few custom SCEET and CEET ducts for various uses, including the cabin heat and the fresh-air vent. I ordered them with their ends sealed with vulcanized rubber so they will never unravel.


 
Dec 20, 2021     Top skin; G5 GPS antenna - (1.9 hours)       Category: Fuselage
Entry 2

In preparation for riveting on the top forward skin (the boot cowl / glareshield), I:

1. Un-clecoed and removed the skin.
2. Drilled the two mounting holes and the coax wire hole for the small GPS puck antenna that will go on top of the glareshield.
3. Began prepping and cleaning the inside of the skin for priming/painting.
4. Fabricated the F-873H spacer for the baggage door attach point on the skin.
5. Spent quite a bit of time reading up on the baggage door fabrication process.


 
Dec 16, 2021     Elevator attach bolt inspection windows - (1 hour)       Category: Fuselage
I only had a short time available today, so I began making inspection windows in the two aft cover plates (under the horizontal stabilizers). This will allow me to visually inspect the elevator pushrod attach point on every preflight -- with a flashlight, instead of having to remove a bunch of screws. I will cut some plexiglas for the actual viewing windows.

I marked the two plates for 2-9/16" holes, drilled out the centers with a unibit, and used a nibbler and a file to get the first of the two holes up to full-size.


 
Nov 06, 2021     Cabin heat control - (1.2 hours)       Category: Fuselage
1. Located and drilled the mounting hole for the cabin heat knob on the aft face of the right-side forward baggage wall. Test-installed the control cable to see how it looks.
2, Located and marked the location for the Garmin GA26C GPS antenna on top of the glareshield. It will be just forward of the avionics fan.


 
Aug 25, 2021     Cabin Heat cable; canopy handle engraving; N-number plaque - (2.3 hours) Category: Fuselage
1. Researched and ordered an engraved N-number plaque for the instrument panel, now that I have acquired my new N-number.
2. Researched and ordered custom engraving on the exterior canopy handle. Packaged the handle for shipping.
3. Measured for and ordered a custom-engraved Cabin Heat cable from McFarlane.

[No photos today.]
 
Mar 28, 2021     Final coax run; Baggage door and top skin - (3.8 hours)       Category: Fuselage
1. Fabricated the final coax connector and installed the last of three coax runs from the panel up to the front side of the firewall.

2. Wire-laced several more areas behind the instrument panel, and also in the avionics hell-hole.

3. Got out all the baggage door components and laid them out with the plans so I can better understand how it will all go together. I had vague recollections of the F-473G hinge support not fitting well several years ago, and sure enough, when I clecoed it in place, there was about a 1/8" gap between the ends of it and both the firewall and bulkhead. Rather than make plans to shim it somehow, I just fabricated another part that's 1/4" longer. Easy-peasy. I also marked where the avionics access door will have to be notched to fit around the hinge support -- although I'll wait to actually notch it until the baggage door is under construction.


 
Mar 24, 2021     LED cockpit wiring; Panel gap filler; Boot cowl work - (4.1 hours)       Category: Fuselage
1. Laid out, positioned and trimmed the white and red LED strips that will be mounted under the glareshield.
2. Drilled a #8 hole in the right side of the panel for the LED light strips' power/ground leads to pass.
3. Began securing the wires for the other LED lights under the lower Z-channel.
4, Began to address the gap between the instrument panel and the side skin on the right side. I started to play with a way I might be able to hide it, although after looking at it, I'm not sure it will actually be that noticeable. And fixing it might make it worse. Anyway, I cut some heavy card stock and traced the curve of the gap onto it, then cut out the card. Using this as a template, I could attach a gray-painted strip of aluminum to the edge of the panel, with the joggled tabs being bonded to the back of the panel. I will think about this solution for a while before I do anything permanent.
5. Marked the rivet sizes on all the holes in the top skin / boot cowl.
6. The glareshield skin hits the rollover bar pretty firmly, and it would mar the bar's powder coat if I allowed it. So I decided to re-profile the curve of the skin to keep it away from the bar. I used a nibbler to start the process, then curved files and sandpaper to finish it up.
7. Performed a preliminary magnetometer interference test (which it passed), just to see if that unlocked any secret game levels. None were apparent..


 
Mar 23, 2021     Fan hole; Boot cowl skin/glareshield - (3.5 hours)       Category: Fuselage
1 Cut out the hole for the avionics fan. Filed and sanded it smooth. Drilled the four mounting holes.

2. Strain-relieved the fan wires inside the fan housing, Cut off the original connector and crimped on D-sub pins to both ends of the power leads. I will connect the fan just before the top skin is riveted in position, but first the skin has to be prepped and painted, inside and out. The section inside the windshield (on top) will be flat black. Underneath (just above the instrument panel), it will be light gray. I am going to research different fabrics and coatings for the top of the glareshield.

3. Hooked up the avionics fan and tested it. It works great.

4. Clecoed the top forward skin in place to check clearances and fit. The holes in the instrument panel attach angle had to be wrestled into alignment, but I got them to cooperate eventually. There is a rather large gap between the right side skin and the top edge of the instrument panel. I might have to install some sort of cosmetic shim there to take up the space. It also looks like the skin will need to be trimmed slightly at the rollover bars.


 
Feb 03, 2021     Holes for throttle quadrant cables - (1.9 hours)       Category: Fuselage
1. Researched, located and drilled two 1" holes for the throttle/mixture/prop control cables -- one on the forward side and one on the aft side of the gear tower.
2. Located and drilled a 3/8" hole in the aft side of the gear tower for the PTT and smoke switch wires on the throttle, plus the backup PTT button on the quadrant.
3. Began assembling the throttle quadrant.


 
Dec 29, 2020     Service Letter SL-00014 accomplishment; Avionics - (2.1 hours)       Category: Fuselage
1. Complied with Vans Service Letter SL-00014. Installed left and right tailcone stiffeners.
2. Installed backplate on GTN 650 rack.
3. Researched Garmin "best practices" for making harnesses.


 
Dec 15, 2020     Baggage tiedown rings; transponder antenna doubler; more - (3.5 hours)       Category: Fuselage
1. Installed two baggage tiedown rings on floor of aft baggage compartment. Drilled attachment holes for two more on the upper hat shelf.

2. Removed transponder antenna from belly of airplane. Trimmed Dynamat sound dampener to fit antenna backing plate. Cleaned inside and outside skin area, removing all Dynamat residue. Marked and drilled backing plate for 20 rivets. Drilled all 20 holes. Clecoed backing plate to inside of skin. Match-drilled holes through fuselage skin. Removed backing plate and countersunk all holes. (Tomorrow, I will get some help and dimple the 20 holes in the fuselage skin, and rivet the plate inside.)

3. Removed ELT buzzer to rework its wiring harness a bit.


 
Oct 22, 2020     Throttle support angle; comm antenna doublers; backup starter switch - (3.6 hours)       Category: Fuselage
1. With the help of my friend Jim, I riveted the throttle quadrant support angle to the fuselage skin.
2. Also with Jim's help, we installed the doubler plates for the two Comm antennas on the belly.
3. Installed the backup starter switch in the aft face of the left gear tower.


 
Oct 15, 2020     RCP air vent; canopy slider track well; relay location scouting - (1.6 hours)       Category: Fuselage
1. Completed the fabrication of the RCP air vent installation. Trimmed the air duct to fit better.
2. Installed the air vent and air duct.
3. Prepped and primed the cover plate and stick boot ring.
4. Prepped, masked and primed the well where the forward end of the canopy track connects.
5. Scouted locations for the Pitot Heat relay and the EBus relay.


 
Jul 24, 2020     Antenna doubler - (0.7 hour)       Category: Fuselage
Prepped and alodined my doubler for the CI-105 transponder antenna.


 
Jul 22, 2020     Aft baggage shelf - (1.5 hours)       Category: Fuselage
1. Drilled out final hoes for attaching aft baggage shelf
2. Drilled two additional attach holes for where the upper bulkhead piece attaches. There will be two additional nutplates now.


 
Jul 18, 2020     Baggage hat shelf prep - (2 hours)       Category: Fuselage
1. Cleaned off yellow primer from access hole ring.
2. Located and drilled attach holes in baggage hat shelf.
3. Shaved camloc rivets.
4. Cleaned and prepped shelf for priming.


 
Jul 07, 2020     Pitch servo & elevator bellcrank access door - (3.1 hours) Category: Fuselage
1. De-riveted previous access door mounting ring from baggage floor.
2. Marked new baggage floor for notching, to match old floor. Nibbled, notched and filed new floor.

(No photos yet)
 
Apr 29, 2020     Dynamat - (0.5 hour)       Category: Fuselage
Installed 1.5 square feet of Dynamat to the inside of the belly skin, just aft of the elevator bellcrank. (I have heard this cuts down on possible oil-canning although I wouldn't think that will be much of a problem in the narrow RV-8 fuselage.)


 
Apr 25, 2020     Baggage wall; transducer manifold; fuel lines; aileron trim - (4.1 hours)       Category: Fuselage
1. Test-fit the forward baggage wall, then removed it and did some trimming and finishing work. Analyzed how I might be able to run an oil cooler shutter control through the avionics hell-hole, and mount the knob on the back side of the wall.

2. Fabricated the stiffener that goes on the back side of the firewall, then installed the transducer manifold on the front side of the firewall. (Have I mentioned before that drilling through stainless steel is a pain?)

3. Cleaned and inspected the two fuel lines that go from the fuel pump to the fuel flow transducer, then from the transducer to the firewall fitting. Installed clear protective tubing on these lines, since they will be subject to some occasional contact due to where they are located -- just inside the pedal access hatch.

4. Began installing the aileron trim system, and planning the wiring runs for the trim servo. (No photo).


 
Apr 24, 2020     Hole removal - (3.2 hours)       Category: Fuselage
Quite a few years ago, I decided to change the location of some of the screws that attach the aft floorboards. I did this for easier servicing and maintenance. Van's floorboards already had the screw holes pre-punched, however. So today, I made about 18 old holes in the aft floorboards magically disappear. After they were gone, I sanded, cleaned, prepped and primed both floorboards.


 
Apr 08, 2020     NACA scoop bug shields - (2.1 hours)       Category: Fuselage
I hate it when bugs fly into the cockpit, especially when they come through the air vent and smack me in the face. I also don't want them making nests inside my vent line. So today began making some screens for the NACA scoops. First, I cut a couple of thin rings from 1-3/4" OD PVC pipe. I pulled out the roll of super-strong screen material I bought a while ago, and cut a couple of circles, then notched them to fit over the rings. I mixed up some 5-minute epoxy and glued the screen material to one of the rings, then while it was starting to cure I shoved it into the front cockpit NACA scoop. Tomorrow, once it all dries, I will trim off the excess screen material and JB-Weld any areas of the assembly that don't seem completely secure. The 2" SCAT tubing will fit over the whole thing with no issues.


 
Mar 19, 2020     Rear seat fiberglass cap - (0.4 hour)       Category: Fuselage
Sanded final round of pinholes and primed. I think I've finally gotten this seat-back as close to perfect as I can get. Onward.


 
Mar 18, 2020     Throttle quadrant, rear seat and avionics door - (1.1 hours)       Category: Fuselage
1. Assembled flap switch and installed on angled panel at forward end of throttle quadrant. 2. Filled more pinholes on rear seat cap. 3. Painted second side of avionics door.


 
Mar 17, 2020     Avionics access door and throttle quadrant - (2 hours)       Category: Fuselage
1. Rived hinge on avionics access door. Painted first coat on door. 2. Riveted quadrant cable support to back side of throttle quadrant. Assembled part of quadrant to see how the chosen hardware looks (Black bolts, stainless screws with washers.) Painted flap switch panel.


 
Mar 14, 2020     Avionics access door - (0.3 hour) Category: Fuselage
Painted the other side of the avionics access door.
 
Mar 13, 2020     Rear seat fiberglass cap; avionics door; throttle quadrant - (0.8 hour) Category: Fuselage
1. Completed sanding the transition between the rear seat and its fiberglass cap. Primed it.
2. Re-primed and re-painted the avionics door and throttle quadrant.
 
Mar 12, 2020     Paint strip; rear sear sanding - (1.6 hours)       Category: Fuselage
1. Stripped both parts that bubbled yesterday. Sanded them both down and began re-priming them. 2. Continued sanding down the new SuperFil transition on the rear seat.


 
Mar 11, 2020     Throttle wiring; rear seat; paint puzzlement - (4.3 hours)       Category: Fuselage
1. Continued working through the process of wiring the throttle quadrant. Made the wire slot a bit wider, and added several more layers of tough, marine heat-shrink to the cable for protection. After doing some rub tests along the edge of a piece of aluminum, I think the heat-shrink layers should last for many years before having to be replaced. Secured the wire with a nylon cable clamp screwed to the quadrant frame. This will allow the wire to gently flex as the throttle is moved full forward and aft. 2. I decided to add a clear, protective coat of paint over the previously painted avionics access door and throttle quadrant top plate. The paint was definitely enamel, so I grabbed a rattle-can of Rust-Oleum clear protective enamel and shot the two parts -- with annoying consequences. The paint almost immediately began to blister and crinkle. Not sure why that happened. 3. Added a smooth transition of SuperFil filler between the rear seat back and the fiberglass cap.


 
Mar 07, 2020     Forward spar attach angle, throttle quadrant and grip, cockpit sills - (4.5 hours)       Category: Fuselage
1. Filed both forward spar attach angles a bit so they will clear the wing root fairings. 2. Mounted new throttle grip and engineered a way for the wires to run down through the quadrant. Cut a notch in both the throttle quadrant and its mounting angle. 3. Painted cockpit sills.


 
Mar 06, 2020     Rear seat, cockpit sills, forward spar angle - (3.5 hours)       Category: Fuselage
1. Applied a resin layer to the back of the upper flange on the RCP sear cap, in accordance with Van's suggestions. This will help prevent excessive wear on the paint of the bulkhead it rests on. 2. Prepped and primed the cockpit sills for painting. 3. Partially unbolted forward spar attach angle from fuselage.


 
Mar 05, 2020     Rear seat fiberglass cap and forward spar angle - (2.2 hours)       Category: Fuselage
1. Filled a few pinholes in the transition between the rear seat and its fiberglass cap. Sanded everything again. 2. Used T-Rex tape to mask off the forward spar attach angle, so I can try to trim off about 1/16" from the forward upper part of the angle that was interfering with the wing root fairing. I only had limited luck with this method, and it looks like I'll have to partially unbolt the angle, in order to file it completely.


 
Feb 11, 2020     Rear seat fiberglass cap - (0.6 hour)       Category: Fuselage
Finished rear seat work by final-sanding the cap, cleaning it, and priming it.


 
Feb 10, 2020     Rear seat fiberglass cap - (1 hour)       Category: Fuselage
Spent another hour filling and sanding the transition between the fiberglass seat cap and the rear seat. It's very close to being perfectly smooth.


 
Feb 06, 2020     Rear seat fiberglass cap - (1.2 hours)       Category: Fuselage
Now that the filler is fully dry, I continued sanding the intersection of the rear seat-back and the fiberglass cap. (Sprayed the area with quick-drying primer first, which allows you to see high spots better as you sand.) It's looking pretty good, but I think it'll need about another half-hour of sanding, and maybe some work on the sides with a very fine file--before I pronounce the seat ready for paint.


 
Feb 02, 2020     Rear seat fiberglass cap - (0.5 hour)       Category: Fuselage
Continued applying a mix of resin and microballoons to the rear seat, this time on the front side. Once it dries, I'll sand everything down to create a smooth, un-noticeable transition between the seat and the cap.


 
Feb 01, 2020     Rear seat fiberglass cap - (2 hours)       Category: Fuselage
Finished riveting fiberglass cap to rear seat back. Began filling gaps at sides of cap with resin and microballoons.


 
Jan 29, 2020     Rear seat fiberglass cap - (3 hours)       Category: Fuselage
Final-fitted the fiberglass cap on the rear seat-back: Trimmed off about 3/8" of cap in accordance with plans. Filed and Dremeled various areas to improve the fit. Marked and center-punched rivet locations on seat. Clamped fiberglass cap in position. Finished fabricating small side stiffener pieces and drilled/clecoed them in place. Match-drilled cap and seat-back to #40 size. Removed fiberglass cap. Finished fabricating top aluminum stiffener angle, clamped it to seat and match-drilled it to existing holes. Reassembled all pieces and final-drilled them all to #30.


 
Jan 28, 2020     Right cockpit switch panel mounts - (1.1 hours)       Category: Fuselage
Worked on mounting angles and nutplates for the sloped switch panel on the right side of the front cockpit. I am working to ensure that the switch panel will be easily removable, if needed someday, to replace switches. or inspect the wiring underneath. This requires installing a few more nutplates than I'd originally installed, and also modifying some of the angles.


 
Jan 25, 2020     Aft baggage floor - (1.5 hours) Category: Fuselage
Finished installing nutplates in aft baggage floor!
 
Jan 24, 2020     Aft baggage floor - (2.5 hours)       Category: Fuselage
Continued installing nutplates in aft baggage compartment floor and middle fuselage longerons.


 
Jan 23, 2020     Aft baggage floor - (2.8 hours)       Category: Fuselage
Continue installing nutplates in floors of aft baggage compartment and middle fuselage longerons. (Working in the aft baggage compartment is painful. Can't wait to get this particular job done!)


 
Jan 22, 2020     Aft baggage floor - (1.6 hours)       Category: Fuselage
Installed all #6 nutplate in flange of sidewalls of aft baggage compartment.


 
Jan 21, 2020     Flap pushrod holes; rear seat fitting; aft baggage floor - (3.3 hours)       Category: Fuselage
Installed rear floorboards in order to check clearance of flap pushrods as the flaps move up and down. Operated flaps with 9V battery and marked several areas of the floorboards to trim. Fitted rear seat back and marked upper Fiberglass piece for riveting. Removed floorboards and trimmed/filed them. Continued working on installing aft baggage floor nutplates.


 
Jan 20, 2020     Aft baggage floor - (3.1 hours)       Category: Fuselage
Match-drilled baggage floor and side panels for #6 screws, then drilled side panels for nutplates. Match-drilled 7 attach holes on top of each side panel for #8 screws in longeron. Deburred all, then sanded, cleaned, prepped and primed side panels.


 
Jan 19, 2020     Avionics access door and aft baggage mod - (3.1 hours)       Category: Fuselage
1. Continued fabricating new avionics door. Cut, filed and sanded edges to match old door. Cut, located, drilled and clecoed new door hinge.

2. Decided to install nutplates in all parts of aft baggage floors, so ALL of it can easily be removed if needed for maintenance, inspections, etc., including the floor and side panels. (Originally, these would have been blind-riveted in place.) Clecoed side panels to floor panel in preparation for drilling.


 
Jan 17, 2020     New avionics access door - (1.5 hours)       Category: Fuselage
Began fabricating new avionics access door from 0.040" stock. Traced around the old one to get a good match.


 
Jan 22, 2015     FCP NACA scoop - (.3 hour)       Category: Fuselage
After letting the filler dry on the fuselage NACA scoop, I finished sanding it, cleaned it, masked it, and shot some primer on the whole area.


 
Jan 18, 2015     FCP NACA scoop - (1.1 hours) Category: Fuselage
Applied SuperFil to the rivets around the NACA scoop that feeds the front cockpit vent.
 
Jan 13, 2015     Skin hole filler - (.1 hour)       Category: Fuselage
Shot a little primer on the now non-existent hole under the flap fairing. The holes is now gone.


 
Jan 12, 2015     Skin hole filler - (.3 hour) Category: Fuselage
Sanded the filler on the magical, disappearing hole under the L flap fairing. So now the hole is gone, never to be spoken of again.
 
Jan 02, 2015     Skin hole removal - (.5 hour)       Category: Fuselage
A couple of years ago, when I was previously working on this part of the project, I had the brilliant idea to add an Adel clamp to hold the plastic tubing that I used to protect the flap motor wiring under the armrest. I used my best guess to determine that it would be OK to drill a hole for the attachment bolt inside the well where the flap would retract. Unfortunately, my guess was off by about an inch. So today, among other projects, I fabricated a patch, and bonded it over the hole in the inside of the fuselage skin under the floorboards on the left side. Tomorrow, after the adhesive cures, I will make the "outside"of the hole disappear with SuperFil. No harm done, in this case. But dang, I hate it when I'm stupid.


 
Dec 21, 2014     Flap rods and rod holes - (4.6 hours)       Category: Fuselage
Time to start connecting the flaps. I began by removing the right flap and connecting the ball end of the flap rod to it. This was much easier said than done. The drawings are in conflict. Drawing 14B shows that there is a nutplate inside the flap that holds the rod end bearing. Drawing 26 shows that you must use a AN364 nut. My flaps have no nutplate in them, and thus began the long process of getting a nut into a nearly-impossible location. 90-degree angled needle-nose pliers were the only way to hold the nut as the bearing was turned. I had placed one washer under the bearing, but it turned out more were needed (see below), so after another lengthy session with the needle-nose pliers, I added another regular washer and a thin washer. This is all that I could add, even with a thin nut, in order to have some thread showing.

Next, I mounted the flap and began filing away the edge of the flap rod hole. After at least a dozen iterations, it became apparent that the rod end bearing on the flap is still not far enough out from the flap (inboard) to give me the required angle for the flap rod. I cannot file much more off the top end of the hole, or the hole will interfere with the flap fairing. I think I will call Van's and see if a longer 1/4" rod end is available or acceptable.


 
Dec 18, 2014     Wing tank support angles - (1.5 hours)       Category: Fuselage
After several years, I waded back into where I left off on the wing forward attach angles. I began by resuming the process of filing a bit of material off the backside of the angles so they lay flat against the fusealge sides.

I also spent a bit of time re-familiarizing myself with all the components in the wing root area, and figuring out what tasks I need to complete, and what order I should do them. I'd like to finish up the wings completely in the next month or so.


 
Nov 05, 2013     Rear baggage floor revision - (1.8 hours)       Category: Fuselage
As I mentioned, when I decided to take out the hard-wired video recorder system from the aft baggage area, this left the hat shelf and right sidewall with ugly notches where the wiring harness passed through. I initially built a cover plate to hide the notch in the hat shelf. The sidewall was easy -- I just bought another piece of sheet metal and started over. But the hat shelf began to bug me. I had already spent many painstaking hours building a cool access hatch for the autopilot servo and elevator bellcrank, and I just didn't want to ditch all that work and start over with a new hat shelf, but that lone cover plate made things look lopsided, or like it was covering up a major error of some kind. I could already hear a future question from another builder at Oshkosh (or perhaps a judge) -- "What's that little access port on the right side of the baggage compartment?" Ugh.

My solution? Add a second "cover plate" on the opposite side. In my opinion, this eases the esthetic look of the whole thing -- it makes it look like those plates are supposed to be there. Once everything is painted, people should hardly notice.

[Superseded.]


 
Nov 04, 2013     Rear baggage floor revision - (.9 hour)       Category: Fuselage
When I began building my airplane, I had grand visions for an integrated remote video camera system. I purchased a remote, two-channel DVR and a couple of "bullet cameras." (One camera was going to be built into the top of the vertical stabilizer, and the other would be on a flex-mount in the cockpit.) With the rise of GoPro cameras in the last couple of years, that plan has been totally rescinded. Unfortunately, I had already hard-wired the plane for the old system, including a mounting location on the right sidewall of the aft baggage compartment where the DVR would be mounted and notches in the wall for the wiring harness to pass through (Photo #1 below). There was no way to remove these without leaving unexplained, ugly holes in my baggage wall, so I ordered a new sidewall. (Note that any time you order replacement parts of this kind, they probably won't be pre-drilled, as in this case.)

After some careful measuring, I installed a pair of sidewall attachment nutplates and drilled the required mounting holes, and now my baggage sidewall will be pristine and perfect. And I have another part to hang on the Wall of Shame. ;-)

The next project will be similar and related -- but a bit more complex. More soon.


 
Nov 03, 2013     Rear baggage floor revision - (1.1 hours)       Category: Fuselage
After letting the SuperFil cure overnight, I sanded down the attach angles and re-primed them. My goof from two years ago is fixed. Onward.


 
Nov 02, 2013     Rear baggage floor revision - (2.1 hours)       Category: Fuselage
The last time I was regularly working on the airplane, I made a few mistakes -- and today I fixed one of them. I had mistakenly riveted the angle pieces that attach the smoke oil tank to the rear baggage floor. They are actually supposed to be detachable using four 1/4-20 wing-nut bolts. Otherwise, you'd be carrying the angles around all the time, even when the smoke oil tank is removed to maximize your baggage space. Today, I drilled the rivets out and removed the angles, re-riveted the four floating nutplates to the floorboard, them filled the extra holes in the attach angles with SuperFil. After some sanding and an eventual coat of paint, nobody will be the wiser.

I also did quite a lot of organizing and cleaning in the workshop.


 
May 09, 2011     Flight controls - (3.0 hours)       Category: Fuselage
In order to install the flaps, flap fairings, ailerons and wingtips, I had to re-install the control column, pushrods and sticks. This took quite a while and, of course, required many trips in and out of the cockpit -- a process that takes some extra effort now that the wings and flaps are on. I think I have it down to a science now.


 
Mar 19, 2011     Wing attach angles - (1.1 hours)       Category: Fuselage
Took the forward wing tank attach angles off the storage shelf and began profiling them to the sides of the fuselage. As I'd noted long ago when I made them, they contact the fuselage sides in only two locations -- about where the AN4 bolts will pass through. I'd like them to sit more flush to the skin, so I began tapering the bases a bit using a belt sander. I didn't remove too much material, but even a small amount made a big difference. They're still not completely flush, but I think they're a lot better than they were before.


 
Mar 01, 2011     Wing mounting prep; Fuel line - (7.5 hours)       Category: Fuselage
I spent a lot of time making sure everything on the wings is ready to go, because tomorrow is "Mounting Day." I drilled out the rivets that were mistakenly installed in the lower root ribs by the Singapore workers who assembled the kit. (These are the holes where the screws and nutplates will go.) I also marked a location 3" outboard of these holes for reference. After the wings are on, this will be the only way to find the holes so I can match-drill the belly skins.

I installed the right fuel line (the one from the fuel selector to the to right wing).

I prepped the shop and laid out every tool I might need. I also set up the sawhorses, workstands and padding for the cockpit.

Finally, I fabricated the wing incidence-setting tool -- a 3-foot steel ruler with a short piece of pointed aluminum clamped to it that extends downward the required 2-51/64".


 
Feb 28, 2011     Prep fuselage for wing attach - (1.0 hour)       Category: Fuselage
With the assistance of my friend Jim, I leveled the fuselage longitudinally and laterally. We added a couple of shims, and got it within 0.1 degree in both axes. Close enough for me.

Next, I removed the comm antenna baseplates from inside the belly skin so they won't get damaged when we tap the drift pins through the wing spar.

Next, I mic'ed the aft spar attach bolts and prepped some of the tools I'll need on Wednesday, which will be Wing-Hanging Day.

Finally, I pondered some solutions to a slight mistake I made last night when I was creating the flap hinge pin keepers. More later.


 
Feb 14, 2011     Autopilot servo mount; RCP map light clamps - (2.9 hours)       Category: Fuselage
Several miscellaneous little jobs today:
- Safetied remaining attach bolt on autopilot pitch servo.
- Began wiring to rear cockpit map light. Drilled attach hole for Adel clamp and installed grommet just aft of the rear seat throttle quadrant. Drilled hole in floor support for conduit.
- Ran 1/4" nylon conduit for wire.


 
Jan 28, 2011     Front seat support bar re-install - (3.9 hours)       Category: Fuselage
Today I received my newly-powder-coated front seat support, rollover bar and canopy frame from the powder coat shop. I re-installed the front seat support today, replacing the standard cad-plated AN3 bolts with black hex cap socket screws and black washers -- all in keeping with the military look I'm going for in my cockpit. (Honestly, I don't remember seeing any hex-cap socket screws in any of the military fighters I flew, but hey...)

Re-installing the support bar also now allows me to get back inside the fuselage. (I've restricted myself from climbing in without this crossbar in place, because I didn't want to risk buckling the skins.)

[UPDATE: Never use black oxide screws in your airplane. They look great at first, but after a couple of years, they begin to rust! Just a word to the wise. Instead, just paint your screw-heads black.]


 
Jan 16, 2011     Comm antenna mounts - (3.8 hours)       Category: Fuselage
I back-drilled the two antenna back-plates to the fuselage skin, using 11 additional holes on each plate for attach rivets, and four holes for the #8 screws that actually attach the antennas. I also marked, drilled and countersunk the plates for four nutplates each. Next, I masked and stripped contact patches inside the fuselage skin for to provide a good grounding surface, using a sanding disc to remove the paint. The attach holes in the skin were dimpled with a pop-rivet dimple set. The stripped patches and the backplates were alodined with a Touch-N-Prep pen, then I riveted on the nutplates.

All that remains is to rivet the plates to the skin, and the comm antennas will be ready to install when the time comes.


 
Jan 15, 2011     Comm antenna mounts - (2.0 hours)       Category: Fuselage
Today's job was to drill the screw holes for the two belly-mounted comm antennas. I had initially thought of mounting the antennas on the inboard-most wing access covers, in an effort to move them to the manufacturer's-specified distance apart. As time went on, however, I have realized that this causes a few more problems than it's worth. Many, many other RV-8 builders have mounted them in the fuselage with no issues. So today I began mounting them in the fuselage belly, as far outboard as I could get them -- basically in line with the aileron pushrod holes. I'll be using right-angle BNC connector adapters, so there will not be any conflict with the pushrods.

Because I don't want the antenna's connectors goobered up by the nearby hammering that will occur as I tap in the temporary spar pins, the antennas will not actually be mounted until after I attach (and remove) the wings. I'll attach the backplates to the belly skin tomorrow.


 
Jan 10, 2011     Front seat support bar removal; Temporary spar pins - (2.8 hours)       Category: Fuselage
I removed the front seat support bar (the aft cross-bar). This, along with the main rollover bar and the canopy frame, will be going to the powder-coater tomorrow to be blasted and powder-coated black.

I also made the wing drift pins, in preparation for mounting the wings. I bought eight 7/16" x 5-1/2" bolts, cut off the threads, and spun them on the grinding wheel and Scotchbrite wheel until they looked nice. At least I demonstrated one small bit of construction skill today... ;-)


 
Dec 01, 2010     Canopy center rail - (.5 hour)       Category: Fuselage
I got several parts back from the anodizer today -- one of which was the center (fuselage) canopy rail. I reattached it and I think it looks really nice. Now it matches the side rails, which were black-anodized earlier this year.


 
Nov 12, 2010     Map pockets - (.9 hour)       Category: Fuselage
Installed all nine nutplates for the upper right map pocket (seven in the fuselage structure seen below, and two in the vertical channel cap).


 
Nov 05, 2010     Canopy rail removal - (.4 hour) Category: Fuselage
With the help of my friend Eric, I removed the rear canopy rail from the fuselage in preparation for having it anodized.
 
Nov 04, 2010     Brake lines; Wiring clamps; Wiring - (2.5 hours)       Category: Fuselage
I decided to permanently install the right brake line today. (I'd already fabricated most of it long ago -- today, I cut the lower end to length, installed the fitting, and flared it.) I can't install the left brake line yet, because I still have to make and install two fuel lines through the bottom of the left gear tower first.

Next, I installed four or five Adel clamps along the cross-cockpit brace in preparation for running lots of wires later. Because of some possible interference with the harnesses that will come off the avionics hub mounted below, there's a possibility that I'll have to invert three or more of the clamps.

I also began twisting some 18AWG wire pairs for use in the fuselage.


 
Nov 03, 2010     RV-8 conversion bolts - (3.6 hours)       Category: Fuselage
Today, I decided to tackle a dreaded project -- installing the 12 bolts in the forward spar webbing that Van's refers to as the "RV-8 Conversion Bolts" and builders often call the "Bag 999" bolts. Since the RV-8 and RV-8/A utilize the same spar, the taildragger version of the airplane has 12 extra holes that, in the nosedragger, would be where the main gear structure would be attached. If you build the proper, tail-sitting version, you have to fill those holes with bolts. Because of the lack of access to the backside, it's a pretty tough job.

The first thing I had to do was to remove the entire control column, because I needed access to the center opening in the spar.

After tapping the bolts in, I used my special "washer tool' from Avery Tools to get the washers on, then taped each nut onto a long screwdriver blade. This allowed me to reach in and hold the nuts in position while I turned the heads of the bolts to get the nuts started. I then torqued each nut to 50-70 in/lb in accordance with Van's instructions.

Sounds simple and straightforward, but it took me over 3 hours to do it. (But it's another tedious job I'll never have to do again!)

Photo 1: The front side of the spar, with 8 of the 12 bolts visible.
Photo 2: The only way I could get the nuts threaded was to tape them to a 12" screwdriver. Worked great!


 
Jun 14, 2010     Main switch panel improvement - (1.5 hours) Category: Fuselage
Today I began installing nutplates along the inboard lower edge of the main switch panel. This will allow me better maintenance access to the switches later if I ever need it, as well as making wiring the panel a lot easier. The left side plate of the panel will now be removable, so instead of having the remove the entire panel to change a switch or re-wire something, I'll just remove 8 screws and be able to do it.
 
Jun 06, 2010     DVR Mount - (1.5 hours)       Category: Fuselage
Attached the four nutplates that will attach the Digital Video Recorder to the sidewall of the right aft baggage compartment. I also riveted on the two nutplates that will attach the cable pass-through plate in the aft baggage wall.


 
Jun 05, 2010     Elevator bellcrank access hatch (v.1) - (8.1 hours)       Category: Fuselage
I guess this hatch should technically should be called an ELT/Strobe/Autopilot Servo/Elevator Bellcrank access hatch, because it will allow some visual access to all of those items. Today, I finished the project. I completed the shaping and filing of the cutout, cut all the hinges, stiffener angles and spacer pieces to size, and cut the door down to its finished size. Next, I taped all the components firmly in position and inserted the hinge pins while I back-drilled the hinges. I bent the forward edge of the hatch slightly to get it it seat flush with the baggage floor. Then everything got sanded, cleaned, prepped, primed, dimpled, and riveted. Finally, I bent the hinge pins into the necessary shapes and drilled the "keeper" holes for them in the wall below them.

This project was a nice one to get me going on the project again. I think it will be a very useful modification. Thanks to the guy on VAF from whom I stole the idea! ;-)

[Hatch design superseded.]

Photo 1: Hatch, assembled. It's held in place with two removable hinge pins.
Photo 2: The lower end of the pins go into the two small keeper holes in the baggage wall.
Photo 3: View showing the construction of the hatch and the shape of the pins.


 
Oct 03, 2009     Elevator bellcrank access hatch (v.1) - (1.0 hour) Category: Fuselage
I started laying out an access door in the floor of the "hat shelf" section of the aft baggage compartment. This will allow me to inspect access the elevator bellcrank, the autopilot pitch servo, the ELT, the strobe pack, and the fuselage area behind the aft baggage compartment -- all without removing the baggage floor.
 
Sep 22, 2009     DVR mount - (1.2 hours)       Category: Fuselage
Match-drilled screw holes for wire cover plate, then drilled holes in baggage wall for nutplates. Trimmed a notch in the plate for the DVR wires, then test-fitted various rubber grommets until I found one that would work. Sanded and filed all edges, then pre-bent the side edges of the cover plate. Cut a small notch in the flange of the baggage wall to allow the rubber grommet to sit flush. [Superseded.]

Photo 1: The connector and harness will hardly be noticable behind the DVR unit.
Photo 2: This is the view of the harness as it exits the back of the baggage compartment wall.


 
Sep 11, 2009     DVR mounting platenuts; circuit breaker plate - (2.1 hours) Category: Fuselage
Installed floating nutplates in baggage compartment wall where the DVR will mount. [Superseded.]

Marked and drilled the 12 holes for the circuit breakers in the right mid-cabin cover, and also drilled the 11/16" hole for the front cockpit Powerlet socket. [Superseded.]
 
Sep 07, 2009     DVR mount and wiring cover plate - (.9 hour) Category: Fuselage
I managed to find only enough time to drill the mounting holes for the Digital Video Recorder in the sidewall of the baggage compartment, and also cut out a 2x3" plate of 0.032" that will eventually be screwed to the sidewall and cover most of the large wiring cutout. (See yesterday's entry).
 
Sep 06, 2009     Remove false spars; RCP stick well cover; DVR mount - (3.1 hours)       Category: Fuselage
Removed the false wooden spars that have been bolted to the fuselage for three years.

Marked the outline of the aft stick-well cover plate onto the floorboards, then removed the cover and all floorboards. Re-assembled the plate and floorboards on the workbench, then trimmed about an inch off the aft edge of the cover plate to allow future access to the floor screws. Back-drilled two holes from floorboards into the cover plate, then drilled them out to #8 and dimpled them. (The two screws that go here will be the only two that go though both the floor and the new cover plate.) The cover plate will also be attached with the screws that attach the vent. I marked the possible future location of the holes that will attach the stick boot to the ring, although I won't drill these until I receive the stick boots.

Finally, I cut notches in the aft baggage wall that will allow the wire plug and harness of the Digital Video Recorder to pass through. This large notch will be covered with a 2"x3" cover plate with a smaller notch and anti-chafe protection. I'll fabricate this plate later. [Superseded.]


 
Aug 29, 2009     Rear cockpit stick well cover - (1.1 hours)       Category: Fuselage
Trimmed the edge of the stick-boot cover ring to match vent hole. Taped the vent assembly to the cover and marked it for 4 mounting holes. Drilled the holes to #40 size. Inserted the cover into the rear cockpit and drilled two pilot mounting holes in fuselage structure.


 
Aug 24, 2009     Main switch panel work - (3.5 hours)       Category: Fuselage
When I built the angled, main switch panel last year, I ended up filing a bit too much off the aft, inboard corner of the removable, aft piece of the panel. Basically, I rounded it a bit, and I shouldn't have. The result was that I needed to fix it to make it look right. I took care of that today. Can you say "JB Weld"? The stuff's great for minor cosmetic filling work like this. After it dried, I filed and sanded it to match the adjoining parts, and you can't tell anything was done to it.


 
Aug 22, 2009     Magnetometer shelf modification (v.2); RCP throttle lever - (1.5 hours)       Category: Fuselage
Since Grand Rapids Technologies added a second AHRS as a standard option on their dual-screen EFIS system, I found out that I'll be getting a second magnetometer as well. This necessitated a slight mod to the shelf in the aft fuselage where the units go. I removed the two centerline-mounted nutplates and installed four new ones. The units will be spread apart about six inches. I also used non-ferrous, aluminum nutplates this time, since I've learned that even a tiny steel nutplate can have a slight impact on the accuracy of the magnetometers.

I found out the fate of my missing throttle lever. It apparently fell off its hook while it was being anodized, and ended up down at the bottom of the anodizing vat. The people doing the work didn't realize what had happened -- and when they did, the part had been almost completely dissolved. So I'll have to make or buy another lever.


 
Aug 19, 2009     Anodized canopy rails - (.2 hour)       Category: Fuselage
Today, I got the canopy rails back from the anodizer. They look pretty good anodized black. In my opinion, though, they might have been a little "under-dyed." The black color is not as dark as I'd hoped. I think it will work out OK.

I also expected to receive my black-anodized rear-seat throttle lever, but all they sent me was the knob. I hope they didn't lose the lever. (The shop was already closed when I opened the package, so I'll have to contact them tomorrow.)


 
Jul 20, 2009     Aft bulkhead; HS spacer painting - (1.0 hour)       Category: Fuselage
After handling, thinking about, modifying, and finally scrapping and fabricating a new copy of the aft upper fuselage bulkhead (F-810A), it finally got installed and riveted in place today. Hallelujah. Onward and upward.

I painted the two spacers that go under the forward spar of the horizontal stabilizer, and also touched up the aft deck.


 
Jul 19, 2009     Aft bulkhead - (1.6 hours)       Category: Fuselage
Next, I clecoed the F-810A aft bulkhead in place and attached the ELT antenna cable to the bulkhead fitting. Since my homemade F-810A has a smaller lightening hole than the stock bulkhead, I'll probably have to use blind rivets in some areas, and I can already tell that tightening the horizontal stab bolts is going to be a challenge, since I can't reach my hand through the hole.

I also primed the two spacers that will reside under the front spar of the horizontal stabilizer.


 
Jul 17, 2009     Upper-right map pocket - (1.1 hours)       Category: Fuselage
Did some final trimming and fitting of the upper-right map-pocket, then drilled and clecoed it to the fuselage structure I had to make a slight joggle at the forward edge of the pocket so it matched up with the vertical channel cap, and also bent the bottom edge so it matched the angle of the armrest.


 
Jul 16, 2009     Main switch console; map pocket - (3.0 hours)       Category: Fuselage
Today, I riveted several of the stiffener angles to the right switch console, and clecoed the assembly in place to the right instrument subpanel and right vertical channel cover. As I suspected, the console is nice and sturdy; however, the lower edge of it moved laterally about 1/8" with about five pounds of hand pressure. Since I want this console to be very sturdy, I fabricated a cross brace between the lower inside stiffener and the sidewall of the cockpit. (Actually, I used the existing, "extra" stiffener that was designed for the stock switch panel.) The cross-brace is merely a 4" piece of 1/4" aluminum tube, flattened on both ends and drilled for attach screws/bolts. The console is now rock-solid. Sweet!

I also riveted the stiffener on the lower-right map pocket, and it's now ready to paint and install.


 
Jul 15, 2009     Tail conduit mount - (1.6 hours)       Category: Fuselage
The next project was to improve the way the tail electrical conduit was mounted to the aft bulkhead. Previously, I'd attached it with a couple of zip-ties around a bulkhead fitting, but this particular support needs to be absolutely, positively secure, and for a good long time. Once the empennage is mounted permanently, this area will be hard to get to, and the conduit is above the right rudder cable. I fabricated an angle bracket and, with the help of my friend Bill, attached it to a nearby bulkhead and bolted a good old Adel clamp to it. That conduit isn't going anywhere. My mind is now completely at ease about that installation.


 
Jul 15, 2009     Map pocket - (1.5 hours)       Category: Fuselage
I finished fabricating the lower-right map pocket. First, I countersunk the 0.040 sheet to accept the rivets that will attach the stiffener, then prepped and primed both parts. I'll rivet them together tomorrow. I also installed the three nutplates in the fuselage. The lower aft one was a MS21051-L08K one-leg type. (The upper-aft screw will use an existing nutplate that also attaches the flap actuator cover.)


 
Jul 14, 2009     Alternator controllers; Map pockets - (1.2 hours)       Category: Fuselage
After having determined a good mounting location for the avionics hub yesterday, I figured out where to mount the two alternator controller boxes -- on the same bulkhead as the hub. Once again, this required the temporary installation of a brake line. I'll use 1/4" pan-head screws to mount the controllers, with the head on the front side, inside the baggage compartment.

I also worked on the lower-right map pocket and the bottom-edge stiffener I designed that will be riveted to the inside of it. (The stiffener will be on the bottom inside of the pocket and will prevent the passenger's foot from bending it.)

Finally, I match-drilled the pocket mounting holes in the fuselage and deburred them.


 
Jul 08, 2009     Map pocket - (1.5 hours)       Category: Fuselage
Continued fabricating the upper-right map pocket. This pocket will fit two Flight Guides, plus contain a map light socket. Trimmed the panel around the corner where it will meet the switch panel.

I also further refined the mounting location for the flexible map light and smaller LED cockpit lights.


 
Jul 06, 2009     Map light mount; Map pockets; Misc. - (2.4 hours) Category: Fuselage
I spent quite a while organizing all the various small projects that need to be done before I mount the tail, and categorizing them further into projects that would be best to accomplish before I mount the landing gear.

I also continued fabricating and began installing the two right map pockets, and tried to figure out a location for plug/mount for the flexible, LED map light. I temporarily installed the front seat to get an idea of geometry and ergonomics issues.

My friend Jim came by and suggested I actually mount it inside the upper-right map pocket (on what is the right armrest). It looks like this might actually keep it out of the way when not in use. I have to examine whether the wires would protrude too much from under the armrest, and interfere with the passenger's right foot. [Superseded.]

I also adjusted the tail wires to their final lengths, and took care of a few more wiring details in the baggage compartment.
 
Jul 02, 2009     Mid-cabin cover (v.3); ELT antenna mount - (2.2 hours)       Category: Fuselage
Since the mid-cabin cover on the right side of the cockpit will probably be used to mount a power outlet that will be used to charge the EFIS battery, I felt that the stock 0.025" cover was not going to adequately stand up to years of use and wear. It just seemed too flimsy, and it flexed too much when I plugged in and removed a power plug. Today, I fabricated a replacement mid-cabin cover out of 0.040" sheet. It seems plenty strong now. I might even use the bottom side of it to mount the SafetyTrim module or something... [Superseded.]

I also drilled a 1/2" hole in the F-810A and installed a BNC bulkhead connector. This will be where I mount the ELT antenna (underneath the empennage fairing.)


 
Jun 29, 2009     Wiring / plumbing grommets - (1.0 hour)       Category: Fuselage
I measured and laid out another wire for the aft fuselage -- this time the four-conductor tail strobe wire. I also drilled the hole in the aft bulkhead where this wire will pass through, and installed a grommet.

In the left gear tower, I installed an edge grommet in one of the remaining 1" holes where the fuel lines will pass through.


 
Jun 18, 2009     Conduit standoffs - (1.0 hour)       Category: Fuselage
Fabricated a couple more wiring standoffs for the aft fuselage, including two that will hold the VOR antenna coax, camera cable, and trim wire away from the elevator pushrod in the aft fuselage.

[Camera wire later deleted.]


 
Jun 15, 2009     Rear fuselage access covers       Category: Fuselage
Installed the nutplates for the aft fuselage access covers (the ones under the horizontal stabilizer on each side). I think these covers are the only external items on the whole airplane that use non-countersunk hardware. It would have been possible to make them flush, but frankly, I just wanted to get the job done. At last, a project I accomplished that was totally stock!

[Superseded in 2023 into non-stock covers!]


 
Jun 14, 2009     Wiring conduit; Elevator stop; Misc. - (4.4 hours)       Category: Fuselage
Today was supposed to be the big day when I mounted the tail, but I found some more things to take care of first -- lots of miscellaneous projects:

1. RTVed the ends of the wiring conduit in the aft fuselage, much like I did in the wings.

2. Attached the elevator stop to the aft fuselage deck. Torqued nuts to final value.

3. Torqued tailwheel attach nut to final value.

4. Fabricated a spacer plate for my new rear cockpit power outlet. (I recently discovered Powerlet sockets, which are much higher quality that a standard "cigarette lighter" outlet. They are a smaller diameter unit, however, so I had to create a plate to cover the slightly oversize hole in the bulkhead where it'll be mounted.) Photos tomorrow. [Superseded.]

5. Engineered an attachment method for the static line as it passes the strobe power pack.


 
Jun 13, 2009     Rear fuselage conduit - (3.1 hours)       Category: Fuselage
In preparation for attaching the tail section to the fuselage, I installed a wiring conduit from the tail up to the aft baggage area. In order to minimize the proximity of current-carrying wires to the GRT magnetometer at the top of the aft fuselage, I elected to keep the conduit run relatively low, rather than use the existing bulkhead pass-thru holes near the top longerons. This required creating a couple of standoffs for the conduit. The aft one is merely two tiewraps clinched around each other. Going forward, the next attachment point is made of two 1/2" angles riveted together, with a teflon tiewrap anchor screwed to one of them. Next, the conduit passes through a 3/4" hole in a bulkhead flange. The conduit ends here. Forward of this, wires will turn downward and pass through an Adel clamp bolted to a piece of angle riveted to the longeron.

Squeezing into the aft fuselage is really a chore for me, and I'm very glad this particular job is over!


 
Jun 12, 2009     Prime and paint aft deck - (1.3 hours)       Category: Fuselage
Prepped and primed the aft deck and the aft bulkhead. Painted the aft deck using the same "Ford Gray" color I used on the interior. The aft bulkhead will be painted much later, with the rest of the exterior of the plane.

I also painted the elevator stop and the F-810A upper aft bulkhead, and cleaned and prepped the two spacers that will go under the leading edge of the horizontal stabilizer spar.


 
May 29, 2009     Tail wiring mounts - (.5 hour) Category: Fuselage
Began cutting angle aluminum pieces that will be used to mount some Adel clamps to the edges of the lightening holes in two of the aft fuselage bulkheads.
 
May 14, 2009     Front seat support bar - (.4 hour) Category: Fuselage
Riveted the left half of the front seat attach bar to the fuselage.
 
May 10, 2009     Front seat support bar - (.7 hour) Category: Fuselage
Since the side rails for the canopy are complete, I decided to permanently attach the WD-808 bar between the front and rear seats. On the QB fuselage, it comes attached only with four AN-3 bolts. Today I installed half of the other 20 rivets that complete it (the ones on the right side).
 
May 05, 2009     Canopy rails - (3.5 hours)       Category: Fuselage
Today, I attached the canopy side rails. I started by removing the rails and making the forward notches in them just a bit taller, so they completely cleared the base of the rollover bar. I then placed the rails in position and carefully measured their distance apart to make sure they were parallel and the correct distance apart. It turned out that the canopy frame rollers moved much more easily with the rails about 1/16" closer than the plans called for.

With the canopy rails positioned and duct-taped down, I drilled the 12 attach holes and enlarged them to #19 for the screws. Thanks to my friend Jim for the assistance with the fitting and drilling process.

Finally, I trimmed the aft outboard parts of the rails, where they hung over the edge of the fuselage. I also filed the notches for the screw heads at the aft end of the rails.


 
May 04, 2009     Forward skin - (1.4 hours)       Category: Fuselage
Removed the forward skin and trimmed the aft end, near the rollover bar, to allow the canopy frame to close. Re-clecoed the skin in place to prepare for drilling the two small stamped pieces that will attach it to the rollover bar.


 
May 03, 2009     Forward fuselage skin - (3.5 hours)       Category: Fuselage
Today, because I finally received my replacement 120-degree countersink bit, I decided to attach the aft baggage door strip, and then drill and cleco the forward skin on. The new strip was match-drilled to the old one, deburred, and attached with LP4-4 blind keeper rivets (hence the need for the 120-degree countersink bit.)

Next, the skin was laid on the bulkheads. This time, I VERY carefully pushed the skin into the proper position and tightly duct taped it to the fuselage sides. The duct tape made a big difference. I got the sides of the skin even on both sides and, with a bit of persuasion, sighted the longeron centerline marks through the pre-punched holes on both sides. (Last time, the skin was uneven by about 1/16" between sides, not enough to be a structural or even a noticeable cosmetic issue, but enough that it would have driven me nuts forever.)

I clecoed the skin to the firewall using the existing holes, then drilled and clecoed the skin on as before, middle bulkhead first, and from the center down each side. It went very smoothly. The resulting slightly figure-8 holes in the flange will be addressed with oversized rivets.


 
May 02, 2009     Aft bulkhead stiffener ring - (.3 hour)       Category: Fuselage
I finally received the tool I needed to create the stiffener ring around the lightening hole in my custom-made F-810A aft fuselage bulkhead. (It's a Hole Flanging Tool, sold by Avery.)

In no time, I'd created the stiffener ring in the bulkhead, which removed all the oil-canning I'd experienced before. I'm going to call this particular project complete -- and a complete success!


 
May 01, 2009     Aft canopy slide rail; Side rails - (2.1 hours)       Category: Fuselage
Today I backdrilled the last slide rail support mounting hole, up through the fuselage and through the aft canopy slide rail support. Next, I assembled the slide rail and the support piece by setting all the double-flush rivets. (I discovered that, although Vans calls for AN426AD3-6s here, 3-6s are too short. 3-7s work much better.) With the exception of countersinking the screw holes and chrome-plating, the aft slide rail is complete.

Next, I cut the canopy side rails to length per the plans. With help from my friend Jim, I positioned the rails on the fuselage and taped them in place to check the fit of the canopy frame. I assembled the canopy rollers and temporarily installed them in the frame. Then we put the canopy frame on the rails and slid it back and forth to check its operation. After tweaking the rail position, the canopy was still a little sticky near the middle of its travel, but I think this will get better with time and proper lubrication. I'll play with it a bit more next time.


 
Apr 28, 2009     Aft canopy slide rail - (2.3 hours)       Category: Fuselage
Today's first project was to double-countersink the aft canopy slide rail support to accept the rivets that will attach it to the rail itself.

I also enlarged the attach holes in both parts to accept the #6 mounting screws. These will be contersunk later.

Next, I fitted the rail support to the fuselage and checked out how it laid in the forward recess. It looked good, so I taped the rail support onto the centerline of the fuselage, and drilled the attach holes into the fuselage skin.

I'll have to crawl into the fuselage next, so I can drill the final, forward mounting hole. There's not enough room to do it from the top.

My plan is to rivet the two rail components together, then have them either chromed or anodized -- along with the side rails and attach screws.


 
Apr 27, 2009     Aft canopy slide rail - (1.8 hours)       Category: Fuselage
Trimmed the aft canopy rail support to length. Trimmed and bent the rail itself to match the support bar. Drew centerline on the rail and marked it for the location of rivets and screws. Clamped both parts together and drilled all holes to #40 size.


 
Apr 16, 2009     Forward skin - (1.9 hours) Category: Fuselage
As I mentioned the other day, I was not happy with the way the symmetry of the forward fuselage skin was shaping up -- not because it would be seen from the outside, but because of the edge distance for the attach rivets in the upper longerons. It would just be too close for comfort.

I reordered and received a new flange strip for the instrument panel, and I've also ordered a new baggage door support strip. Today, I installed the new instrument panel flange, and marked the centerline of the flange in preparation for re-drilling it. Next time, the skin will be pulled down and duct-taped to the fuselage sides to ensure it doesn't shift one iota.
 
Apr 15, 2009     Smoke oil line - (1.2 hours)       Category: Fuselage
Because of the numerous fuel lines that must run through the left gear tower, I repositioned the smoke oil line from the left side of the fuselage to the right. I drilled four new bulkhead holes and installed snap bushings, then ran the line. It will have to be secured, of course, and I won't run it forward of the spar until after the wings have been attached.


 
Apr 10, 2009     Cabin heat valve; Instrument panel mount - (2.9 hours)       Category: Fuselage
With the assistance of my friend Jim, I cut a 2" hole in the firewall for the cabin heat box. (We removed the engine mount to get better access.) I used a fly-cutter to cut the hole, which worked fine, but was very slow. I had to remove and sharpen the cutter at least 10 times -- the stainless steel really dulled it quickly. Jim held a 2x4 on the back side while I drilled. I dressed the edge of the hole with a stone wheel in a Dremel tool.

I have a stainless steel cabin heat valve from EPM.AV Corp (not stock, of course) which is great, except it requires some changes to the stock installation. In my case, the firewall-forward part of the valve will be mounted in accordance with Drawing OP-34, but the aft portion will be turned 90 degrees so it misses the nearby firewall angle, and leaves room for the control cables to pass through the firewall. This new attachment method means there will be four bolts to attach the box instead of two. No biggie.

I had time for one additional task: I drilled the bolt holes that attach the instrument sub-panels to the side longerons, one on each side.


 
Apr 08, 2009     Forward fuselage skin - (2.2 hours)       Category: Fuselage
Today I got the forward skin drilled and clecoed to the instrument panel flange. In order to prevent the skin from being slightly buckled down near the bottom edge where the instrument panel flange has a gap, I began by removing a half-dozen of the clecoes on the outboard bottom edges of the instrument sub-panel, and then pushed the flange up to meet the skin. I marked the new position of the flange and removed the skin and panels. Then I re-drilled the flange to its new position along the sub-panel. (Since I enlarged the holes to #30 to do this, I'll use "Oops" rivets to fill the larger holes.)

Then I reinstalled everything and drilled the skin on. The process worked pretty well. There was only a small gap remaining. My friend Jim helped with drilling and clecoing. I plan to cover the gap on the inside of the cockpit (along the outer edges of the sub-panel, where the backside of the flange now shows a bit) with engraved panel plates that will contain the switch markings.

My only bummer of the day came when I saw that somehow, I've developed a small mismatch in the overhang of the skin on the fuselage. The left edge is higher by about 3/32". I hope this doesn't cause any issues when drilling the skin through the longerons. It certainly won't be noticeable unless someone actually measures it. I'll think about this issue over the next few days.

Finally, I installed the avionics access door and clamped the baggage compartment hinge channel in place, then marked where I will have to notch the avionics access door for it to clear. Also, I noted that the hinge channel, which I built to plans a while ago, is about 1/8" to 3/16" too short, so it will either require a shim or I'll have to build a new one.

Photo 1: As expected, the baggage door hinge channel (top) will require me to put a notch in the avionics access door.
Photo 2: I had to do a little trimming of the skin along the edges so they didn't rub on the rollover bar.
Photo 3: Skin drilled and clecoed to the instrument panel.


 
Apr 07, 2009     Forward fuselage skin - (3.8 hours)       Category: Fuselage
Today I removed the forward skin and began prepping it. I cut out the cockpit recess, using snips to get within about quarter inch of the line, then a notching tool to get within 1/32", then a pneumatic rotary disk and sandpaper to get it perfect. I also removed strips of the blue plastic along the rivet lines.

Next, I removed the extra skin piece where the baggage door will go, then filed down the tabs along the edges and polished the skin edges.

I clecoed the skin back on the fuselage and began installing the instrument panel and sub-panels. I noticed right away that there's a gap between the sub-panels and the side skins (Photo 3). Just about every other RV-8 builder I've ever talked to has reported this same issue. I might be able to remedy it by building a pair of curved filler tabs, and riveting them to the side panels.


 
Apr 06, 2009     Forward fuselage skin - (3.4 hours)       Category: Fuselage
Today was very productive! With the help of my buddy Jim, I got the forward fuselage skin drilled and clecoed to the fuselage. I didn't have the wherewithal to take many photos of the process, but here's what I did:

I started out by completing the installation of the two baggage compartment support strips that go between the skin and the two bulkheads (one of which is the firewall). I attached these with flush keeper rivets located in between the existing pre-punched skin holes. Next, I marked the flange centerlines on both bulkheads.

I then set the skin in place and measured everything to make sure it was centered. I coerced the firewall into its proper 8-degree-bent position, and clamped it securely in place. I tweaked the bulkhead position until it was reasonably close to its final position, then clamped the skin down with a band clamp. Then I began drilling and clecoing the skin to the firewall, starting in the middle and working outward.

One the firewall was clecoed, we moved aft to the bulkhead. Jim reached through the cockpit with a padded wooden rod and pushed or pulled the bulkhead until I could see the centerline mark on the flange through the skin holes. Then I drilled and clecoed -- again, working from the center outward. It all worked out very nicely -- the skin is smooth and wave-free. Gotta love CNC technology.

My final task was to drill and prep the instrument sub-panels for nutplates. These will be attached tomorrow. Then the subpanel attach angles will be drilled and clecoed to the skin as well.


 
Apr 05, 2009     Forward skin - (1.6 hours)       Category: Fuselage
I began installing the support strips that will attach to the flanges at the tops of the firewall and F-866BPP fuselage bulkhead. More of this tomorrow. I'll be very interested to see how the top skin fits, since the firewall arrived already pre-bent at about 20 degrees, vs. the 8 degrees the plans call for. Fitting the skin could be a bit of an adventure.


 
Mar 18, 2009     Aft bulkhead fabrication - (2.9 hours)       Category: Fuselage
My previous attempt at fabricating a new aft upper bulkhead (F-810A) was mostly successful, except that the finished product was slightly too wide due to a measuring error on my part. Today, I modified the form block to the correct dimensions, located a scrap of 0.032 aluminum, and fabricated the bulkhead all over again.

This one came out really, really nice. After fluting the tabs, it fit like a glove! Sweet.

All that's left to do is create the stiffener ring around the lightening hole, then drill/cleco the new part in place.


 
Mar 14, 2009     Aft bulkhead fabrication - (2.4 hours)       Category: Fuselage
Today I cut the lightening holes in my new F-810 A bulkhead, made the former blocks used to hammer the bulkhead flanges, and hammered the flanges.


 
Mar 09, 2009     E-bus diode wiring - (.6 hour)       Category: Fuselage
Tonight I did the first wiring in the forward fuselage -- the two 10 AWG connector wires between the main bus, Schottky diode, and Essential Bus. I used a RhinoPro 3000 label maker and yellow heat-shrink labels. The connectors are PIDG ring terminals with double-wall heat-shrink. I used K-nuts on the connections.


 
Mar 05, 2009     Mid-cabin cover - (.9 hour)       Category: Fuselage
After revising my electrical system details over the winter, I decided to re-make the right side cabin cover. This will accommodate a different style of power outlet and a different map light. I happened to have some extra 0.025 sheet, so I replicated the existing cover.

[Superseded.]


 
Feb 10, 2009     Aft bulkhead fabrication - (2.2 hours) Category: Fuselage
I decided to tackle the mis-fitting F-810A bulkhead today. I came to the conclusion that instead of trying to modify the existing factory-stamped bulkhead to fit by trimming off the ears, moving them, and riveting them back on, I would simply start with a clean sheet and make the thing from scratch myself. I traced the existing fuselage opening onto cardboard, marked it up, and used it as a template to cut the part from a sheet of spare 0.032". I trimmed it, cut out the notches, and prepared it for being hammered over a wooden mold (which I'll create next).
 
Nov 06, 2008     Strobe pack; static line; switch panel angle - (2.0 hours) Category: Fuselage
I completed the installation of the strobe unit mount underneath the aft baggage compartment. Once the wiring and other installations in the aft fuselage are complete, the strobe pack will just screw right on.

Next, I ran the static line from the T-connector in the aft fuselage up to the vicinity of the instrument panel. I had originally thought I would route it along the bottom of the upper longeron, but I found a way to do it under the floor that will be less obtrusive and will not require going through or around the instrument panel sides. The line will be secured along its length with a combination of Adel clamps and zip ties.

Finally, I clecoed an attach angle to the fuselage that was once destined to support the right-hand switch panel. For me, since it will be covered by a custom angled switch panel, it will support a couple of Adel clamps and a large wire bundle.
 
Nov 05, 2008     Strobe pack and ELT mounts - (1.2 hours)       Category: Fuselage
Today I mostly finished the installation of the mounting plates for the strobe pack and the ELT.

I installed the nutplates on the three strobe mount angles, then blind-riveted them to the longerons in the aft fuselage.

I also screwed the ELT mounting plate to its mounting angles using Torx-bit #8 screws and Loctite.

[Superseded.]


 
Nov 04, 2008     Strobe pack mount - (1.2 hours) Category: Fuselage
Finished drilling the new strobe pack mount to the fuselage, then prepped the attach-angles for nutplates. Deburred, cleaned, primed and painted all three pieces. Countersunk holes in the upper longeron so the CS-4 rivets won't interfere with the baggage compartment floor.
 
Nov 03, 2008     Strobe pack mount - (1.5 hours) Category: Fuselage
Today I finished fabricating the three angle pieces that will mount the strobe power pack to the left side of the fuselage in its new location. I clamped and drilled them to the longerons just behind the aft baggage compartment on the left side. Next, I'll prime/paint them and mount the nutplates.

Since both the ELT and the strobe pack will now be on the left side of the fuselage, I'll have to run the "noisy" strobe power wires over to the right side to keep them away from the lower-power and antenna leads that generally run up the left side.
 
Oct 23, 2008     Strobe pack mount - (1.0 hour) Category: Fuselage
I cut a second access hole in the wooden work floor that fits into the aft fuselage. This will allow me to install the strobe package in its new location, one bay forward of where it was originally going to be located. (This move was required by the magnetometer's requirement for 18" of space between it and any ferrous material or power supply.)

I measured between the longerons and cut up some scrap 1" angle. I'll rivet an angle on each longeron, and the existing mounting plate will be re-used.

[Superseded.]
 
Sep 24, 2008     Strobe pack mount - (.5 hour) Category: Fuselage
I spent some time installing the rear floorboards and inserting the wooden work floor in the back of the fuselage, in preparation for installing the strobe power pack in a new location about 2 feet forward of where I initially wanted to install it.

[Superseded.]
 
Sep 03, 2008     Systems re-installation Category: Fuselage
Since all the interior paint is dry, I re-installed the smoke oil line and rudder cables through their bushings in the floor supports and spar.
 
Aug 19, 2008     Wiring bushings and routing planning - (1.5 hours)       Category: Fuselage
Yesterday, I took a dozen or so pictures of the inside of the fuselage, and today, I mounted the 8.5" x 11" photos on a foam core board. I began drawing some of the various wires and key components that will live under the floor, planning where the wires will go based on their function and how "noisy" or "noise-sensitive" they are.

I also drilled another four or five holes, and installed snap bushings in several bulkheads.


 
Aug 19, 2008     Static line; Smoke oil line - (2.4 hours)       Category: Fuselage
Today I began by installing the static line from the aft fuselage up to the instrument panel area, just to check which bulkheads will need holes, and where. Running it up under the left longeron seems to be the best routing. I had to trim a small notch out of the flap actuator cover, but other than that, the installation appears like it will be straightforward. I won't actually install the static line, the hole grommets, or the Adel clamps until after the canopy rails are fitted.

Next, I ran the smoke oil line from the aft baggage compartment up to the firewall, drilling several 5/8" holes through the bulkheads and installing snap bushings. I'll secure it along its length with Adel clamps later.

[All routings superseded.]


 
Aug 18, 2008     Wiring bushings - (.9 hour)       Category: Fuselage
This evening I drilled a bunch of 5/8" holes and installed about a half-dozen plastic snap-in bushings in various places in the fuselage -- through the spar web and through several bulkheads and support ribs. These will be used mostly for for electrical wires, but also for things like the static line, smoke-oil line, etc.

"Noisy" or high-current wiring will go along the left side of the fuselage. Low-current, critical or shielded wiring will go along the right side. The smoke oil line will go up the middle, more or less.


 
Jul 15, 2008     Electrical busses - (.5 hour)       Category: Fuselage
Laid out the Main and Essential fuseblocks/busses and the Schottky diode & heatsink on the back side of the avionics access door. I played with various configurations that would allow everything to fit, while still leaving room for the deep avionics on the left side of my instrument panel. I made an effort to ensure that the wires from the Essential buss will clear the top edge of the door opening once they're attached to the tabs.


 
Jul 15, 2008     Forward baggage floor modification - (.5 hour)       Category: Fuselage
I completed work on the forward baggage floor modification by dimpling the three holes in the overlapping edges of both of the floor pieces, installing the three countersunk nutplates, and setting the final three rivets on the new floor stiffeners -- the ones I couldn't reach with the hand squeezer.


 
Jul 12, 2008     Forward baggage compartment modification - (1.5 hours)       Category: Fuselage
Installed three nutplates in the existing baggage compartment floor, where the new floor piece overlaps.

Fabricated two stiffeners for the bottom of the new baggage floor piece. Dimpled and primed the stiffeners, then riveted them to the floor.


 
Jul 11, 2008     Forward baggage compartment modification - (2.4 hours)       Category: Fuselage
Installed nutplates in fuselage support angles that will attach the forward baggage floor extension.


 
Jul 08, 2008     Forward baggage compartment modification - (2.3 hours)       Category: Fuselage
Today I decided to cover over the lower portion of the forward baggage compartment and turn this area into an electrical "hell-hole." This is a popular option for some RV-8 builders, and it's one I've been considering for a while. With all the extra wiring and electrical components I'll be installing, the extra couple of cubic feet will be very welcome. I'll probably use it to mount the grounding buses, the Approach Pro-Hub avionics hub, some relays, a backup EFIS battery, or other items. It might also allow me to mount a heating vent on the rear (cockpit) side of the vertical wall outboard of the pilot's right leg, and will be a great place to run wires fore and aft from the engine compartment and panel area.

I temporarily installed the forward baggage compartment floor, measured the area I wanted to cover, and cut out a cover plate from a sheet of 0.032. I notched it to fit in the right front corner, match-drilled it using one hole in the existing floor, and drilled #8 holes in about a dozen other places along the edge for screws and nutplates. The right-aft edge will be supported by a stiffener only, and there will be another stiffener under the center of the new floor piece, similar to the ones on the existing floorboard.


 
Jul 07, 2008     Systems installation (flaps, servos); Svc bulletin - (4.5 hours)       Category: Fuselage
Continued installation of various components:

-- Riveted in the slide tube guide for the aileron trim servo.
-- Riveted in the attach bracket for the autopilot roll servo.
-- Measured for the fuel lines, fuel vent lines, and brake lines.
-- Planned for the wiring routes through the bulkheads and wing spar.
-- Re-installed the flap motor and actuator arm/blocks. Complied with Van's Service Bulletin (drilled and safety-wired the flap motor shaft.) [Superseded]


 
Jul 05, 2008     Systems installation - (4.0 hours)       Category: Fuselage
Continued re-installing various systems and components:
-- Clamped the plastic anti-chafe covers into position where the cables exit the fuselage at the tail.
-- Riveted the aileron trim servo tray into the fuselage.
-- Installed the rudder cable forward attach clevises to the firewall.
-- Continued planning the routing of wiring harnesses forward and aft through the bulkheads.
-- Prepped lower longerons for installation of the flap actuator arm and attach blocks.
-- Attached fuel selector to its attach plate.
-- Shot a second coat of paint on various small components.
-- Finally, I pulled out and organized all the various bags of hardware that will be needed as the interior goes back together (Photo 3).


 
Jul 02, 2008     Systems installation - (1.9 hours)       Category: Fuselage
Today I began re-installing all the various subsystems I'd removed in order to paint the interior. I installed the power outlet in the rear cockpit, the fuel vent fittings inside the gear pockets, the fuel filter, and the overboard pressure-relief port for the smoke system.

Photo 1: There will be a 3/4" hole on the left for the brake lines.
Photo 2: The fuel filter. I attached it with AN-3 bolts. There are nutplates inside the gear tower.
Photo 3: Smoke system belly port, fastened with rivets and sealed with Proseal.


 
Jul 01, 2008     Wing attach fittings - (2.7 hours)       Category: Fuselage
For a change of pace, I fabricated the F-863 L/R forward wing attach fittings. Why not? They had to be made, and today just seemed like a good day to make them. Since they'll probably have to be slightly contoured to the fuselage skin later (and of course they'll have to be drilled, too), I left them un-primed and un-painted for now.


 
Jun 17, 2008     NACA scoop - (.5 hour) Category: Fuselage
I prosealed and riveted the NACA scoop to the fuselage.
 
Jun 16, 2008     NACA scoop (forward) - (2.9 hours)       Category: Fuselage
I positioned the NACA scoop on the left side of the fuselage, and drilled and clecoed it to the skin. Then I deburred and dimpled the skin, and countersunk the plastic scoop. Since I'll be installing the scoop with rivets, I needed a backing plate for the flange of the scoop, so I fabricated one out of scrap 0.20 aluminum. I match-drilled the ring and primed and painted it.


 
Jun 15, 2008     Avionics access door - (2.0 hours)       Category: Fuselage
Today I completed the avionics access door. First I prepped and primed all the components, then riveted the hinge and shim strip along the bottom the opening. Then I installed the doubler ring and nutplates around the edge of the opening. Finally, I riveted the upper half of the hinge to the door itself, installed the door, and fastened it shut with eight Torx-bit screws.

I think it looks pretty nice!

There will be a bit of notching required at the top of the door where the baggage door hinge support goes, but that will be much later.


 
Jun 02, 2008     Avionics access door - (1.6 hours)       Category: Fuselage
Continued fitting and drilling the nutplate attach holes and screw holes in the bulkhead avionics access door and the stiffener along its edge. There are several tricky areas where flush rivets will have to be installed, and their shop heads and manufactured heads will have to be oriented in a very particular way. I marked these locations so I won't forget, since it'll be a few days before I can get back in the shop.

In the photo below, you can see where the door will be held closed with eight #8 screws (black clecoes).


 
May 27, 2008     Rudder cable fairings - (.7 hour)       Category: Fuselage
I trimmed the Avery rudder cable fairings and fitted them to the fuselage to see what might the best way will be to mount them. The QB fuselage doesn't give you many options because the slot for the cable is already cut. If I'd done it myself, I would have move the slot up a bit so I could easily make the fairing removable.


 
Apr 19, 2008     Electric fuel pump; Air vent scat tubing - (2.8 hours)       Category: Fuselage
I began installing the Airflow Performance electric fuel pump today. First, I fabricated the saddle angles and ES Airflow bracket, then I located, drilled and clecoed the angles to the floor.

Next, I bagan planning the location of the fuel filter. It will be mounted to the front side of the left gear tower, but the exact location is still to be determined. The installation is a bit more complicated than it looks, because there are several potential conflicts nearby -- most notably the front cockpit air vent scat tube and the throttle quadrant cables. I'll try to work out these conflicts tomorrow.

In the meantime, I laid out the air vent line and tried to get an idea of various routing possibilities. I'd like to keep it relatively unobtrusive from the pilot's seat, but it appears to be impossible to make it completely invisible without cutting a 3" hole near the top of the gear tower, something I don't want to do.


 
Apr 17, 2008     FINISH KIT DELIVERY; Battery charger jack - (1.1 hours)       Category: Fuselage
My Finishing Kit was delivered today! Unfortunately, the process did not go flawlessly. The delivery was made by BAX Global, who told me this morning that they'd call me before the driver headed my way. Instead, they dropped off the crate at lunch time, unannounced, at the FBO, and never notified me. An hour later, as I drove past the maintenance hangar, I noticed it sitting out on the ramp by itself, unattended. I also noticed two large forklift holes punched into one end of the crate. I called Van's and asked them if I should even open the crate, or whether I should just send it back and file a claim. They instructed me to examine the contents and report back. To make a long story short, I opened the crate and found a dime-sized partial puncture of my lower cowl. The hole is only in the surface layer -- it did not go all the way through the cowl -- so I feel confident that I'll be able to fix the damage later. It'll be much easier to do this than to deal with a month's delay and stacks of paperwork to get a small settlement and not have the airplane parts I need. Needless to say, I won't be taking any of my business to BAX Global in the future.

Later in the day, after unpacking and taking inventory of everything, I managed to get a little work done: I test-mounted an XLR jack in the right-side mid cabin cover. This will provide an easy way to charge my auxiliary EFIS battery with an external charger. I like XLR plugs for applications like this because they're "keyed" and you can't goof up the plug polarity. [Superseded several times!]

I also removed the gear tower access covers, and prepped and primed them.


 
Apr 16, 2008     Floorboards; Interior painting prep - (1.3 hours) Category: Fuselage
Tonight I installed the 14 additional floor nutplates in the floor sub-structure.

Next, I began preparation for painting the interior of the airplane by removing the remaining floorboards, the flap motor, and other miscellaneous items.

I also began figuring out the placement of some miscellaneous cockpit items such as the Carbon Monoxide detector and the ELT remote indicator. I originally thought I might mount them on the right mid-cabin cover, but that area looks like it will be handy to stash maps, charts, and such. The left cabin cover is a possibility, but it's pretty cluttered right now. I'll have to wait and see once I get my GRT EIS-400 unit and fuel valve installed. I might also place them on the instrument panel.
 
Apr 15, 2008     Floorboard nutplates; Miscellaneous stuff - (1.7 hours)       Category: Fuselage
When I installed the removable floorboards a year or so ago, I had decided to skip the installation of a few of the floor nutplates in the sub-structure. I did this for weight considerations and simplicity, but I've "re-thunk" this philosophy. The empty holes looked funny to me, so I began installing 14 more nutplates today, thus filling all the holes in the floorboards and giving the floors a better, finished look. I drilled, countersunk and primed all the locations, so they're ready for the installation of the nutplates.

I also painted a few various brackets -- the ones for the flap limit switch, aileron trim servo, and autopilot roll servo.

Finally, I spent some time studying the installation and components of the Airflow Performance fuel pump and filter, and studied where I might install the Safety Trim controller unit.


 
Apr 14, 2008     Aileron trim; Autopilot servo; Gear leg prep - (3.2 hours)       Category: Fuselage
I noticed an error in Van's kit. The aileron trim servo kit comes with a jig you're supposed to use to locate and drill the mounting holes for the servo and the tube guide. This jig, as it turns out, is about 1/4" off from my pre-existing QB fuselage holes, so it appears that this is one of those times that I'll have to press ahead and work with what I actually have, rather than what the plans say I'm supposed to do.

I located and drilled the mounting holes for the trim servo tray and the tube guide, using the servo as a guide for the exact fore/aft placement of the mounting tray. I had to trim just a tiny bit from one side of the top of the mounting tray so it would clear a bulkhead intersection.

Next, I located and drilled the mounting holes for the autopilot roll servo. I elected to drill out two of the QB rivets and re-use these holes for the top two rivets on the bracket. I also discovered that the installation of the roll servo causes a conflict with a floorboard stiffener, so I trimmed off about 1/8" of the stiffener (See photo #3 below). I may have to trim some more later, during the installation of the servo actuator arm. [Superseded later by Garmin servos.]

Next, I deburred and re-primed all components, and painted the flap microswitch mount and striker plate.

The last thing I did today was remove the pre-installed gear leg covers, in preparation for installing the gear. Two of the #6 screws were so tight I had to use a "screw-out" bit and some PB penetrating oil on them. Take THAT, screws!


 
Apr 10, 2008     Rudder pedals; aileron trim - (2.2 hours)       Category: Fuselage
Tonight I began work by fabricating and installing the fairlead insert in the WD-816 rudder slide.

Next, I removed the wooden work-floors from the aft fuselage and the forward floorboards, and vacuumed out the fuselage. With a friend's help, I raised the fuselage, mounted it on the rotisserie, and rotated it to the '90-degree right' position.

I began the installation of the aileron trim system and autopilot roll servo by laying out and identifying the various components and their relationships. The autopilot servo mount will be very close to the trim servo mount, so I want to make sure I have everything right before I pick up a drill.

To make room for the installation, I removed the WD-807 Control Column. The final thing I did today was to install the two trim springs on the column. I found it easy to open the spring loops with lineman's pliers.


 
Apr 09, 2008     Rudder pedals; Aileron trim - (3.0 hours)       Category: Fuselage
I began by re-riveting the rudder pedal slider-latch mechanism. Now it's straight as an arrow.

Next, I began fabricating the components of the aileron trim assembly, starting with the servo pushrod. I used a bandsaw to make the first cut of the slot, then used a series of files to open the slot up to 1/8". I used the drill press to make the three required #30 holes in the tube.

The builder's manual says not to use a drill bit to open up the hole in the plastic bushing where the aileron trim push tube will go. It recommends using a Dremel tool instead. I started doing this, but decided to sacrifice a bushing as an experiment. Wouldn't you know, a series of larger and larger drill bits running very slowly in an electric drill worked beautifully. I held the bushing with a pair of padded pliers.

Finally, I prepped and primed the servo mount, the pushrod support bracket, and the pushrod (except for the bottom 2" of the rod you can't see in the photo...)


 
Apr 08, 2008     Flap microswitches - (2.4 hours)       Category: Fuselage
I started fitting the two flap microswitches to the fuselage, and attached the striker plate to the flap arm. After testing various locations for the components, I decided to flip the switch attach-angle upside down so the switches are closer to the fuselage skin. I did this so the fast-on tabs on the switches are UP (away from the seat belt attach point and the flap tube). This position also gives the striker plate a more elegant approach as it presses the switch arms.

I replaced a non-standard Adel clamp (the one that had been temporarily holding the wire tube to the flap shaft) with a new one.

I drilled and bolted the switch attach angle to the bulkhead with two AN3 bolts, washers and nuts, the removed the angles and the striker plate. I trimmed off about 1/4" of the width of the striker plate that won't be needed, then I deburred and primed both parts.


 
Apr 06, 2008     Rudder pedals; flap limit switches - (2.5 hours)       Category: Fuselage
I installed the rudder pedal assembly to the floor, and drilled the holes for the rudder pedal cable clevis bolts through the firewall. I also screwed the A-600 brake reservoirs to the master cylinders to check their clearance from the firewall with the pedals forward. As other builders have noted, I will have to avoid using the most forward hole in the slider bar when I position the pedals.

Next, I began installing the flap limit microswitches to the fuselage bulkhead, and the switch actuator tab to the flap arm. For now, I attached everything in place with tape, just to get an idea of the proper placement of all the components. I had to trim off about 1/2" of the angle that the microswitches are attached to. This will give it more clearance from the sidewall piece that covers the flap actuator.

Finally, I de-riveted the rudder pedal slider-latch assembly that I built last week. I didn't like the way the part "leaned" a bit, so I'll re-prime all the parts and and re-rivet them. I think the part leaned because a). I used a Dash-12 rivet instead of a Dash-11, and b). I didn't clamp all the parts together tight enough. Lesson learned.


 
Mar 29, 2008     Baggage door; Fuselage nutplates; Pedal assy. - (2.0 hours)       Category: Fuselage
This evening, I fabricated the F-873G forward baggage door hinge support. [Re-built later]

I also decided to tackle a bunch of too-tight nutplates in the forward part of the fuselage, including the 13 nutplates that attach the walls of the lower section of the forward baggage compartment. As I was running a tap through one of them, the tap broke off. (That's what I get for buying cheap Chinese taps from Harbor Freight.) Rather than trying to drill out the piece of the tap, I ended up removing the nutplate and replacing it. Glad this happened with one of the nutplates that I have good access to!

Finally, I put the final coat of paint on the components of the pedal adjustment mechanism.

Gradually, spring is coming. I've really missed working on this plane!


 
Mar 23, 2008     Avionics access door; rudder pedals - (2.1 hours)       Category: Fuselage
Today I fabricated the 0.032 doubler strip that will go around the door opening in the bulkhead. The platenuts that will secure the door closed will be mounted on this strip. I clecoed the strip in place to check its fit.

I also painted the various components of the rudder pedal release mechanism.


 
Mar 22, 2008     Avionics access door; Rudder pedals - (.8 hour)       Category: Fuselage
The AN-3 bolts that mount the aft end of the rudder slider bar to the floor are screwed into two nutplates in the floor. In the QB fuselage, these nutplates are already installed. One of the two accepted the bolt with no problems, but the other had to be tapped with a 10-32 tap in order to accept a bolt. I took care of that today.

I also began laying out the 0.032" doubler that will surround the avionics access-door. I traced the piece of bulkhead that I previously cut out, then I added 3/4" to the top and side dimensions.

Finally, I primed the components of the pedal adjustment latch. I'll paint them when the weather warms up, then rivet them together.


 
Mar 16, 2008     Rudder pedals and brakes - (2.4 hours)       Category: Fuselage
I attached the stock brake master cylinders to the pedal assembly, after deciding that modifying everything to fit the Matco MC-5 integral reservoirs was going to be too much of a pain.

I also fabricated and test-assembled all the parts for the flight-adjustable rudder pedal latch assembly. Van designed a really slick setup to adjust the pedals! Very impressive.


 
Mar 10, 2008     Rudder pedals - (.3 hour)       Category: Fuselage
I spent a little time trying to figure out how I might be able to mount the Matco MC-5 brake master cylinders to the pedal assembly. The cylinders are much wider than the stock ones, and they hit the pedal weldments. More research is needed.


 
Mar 05, 2008     Rudder pedals - (1.7 hours)       Category: Fuselage
I managed to sneak into the workshop and actually get some work done!

I attached the rudder pedal slider bar (WD-818 and WD-817) to the floor and firewall. This was greatly complicated by the fact that the pre-installed nutplates seemed to have a mind of their own and did not accept the AN-3 bolts with anything resembling enthusiasm. I finally got it done with some Boelube and the help of a buddy. I think these nutplates will have to get a tap run through them before final assembly. I then drilled the attach bolt holes through the shaft of the slider bar and the weldment.

Next, I began test-fitting my Matco MC-5 brake master cylinders to the pedal assembly. The design of the integrated brake reservoir might mean that if I use them, I'll have to modify the attach-tabs on the WD-816 weldment. Either that, or I'll make a spacer and use a longer bolt. Not sure yet.


 
Feb 16, 2008     Avionics access door, rear cockpit map light - (1.5 hours)       Category: Fuselage
I managed to get a little time in the workshop, despite the persistent, bitter cold.

I finished trimming, filing, and sanding the edge of the opening in the bulkhead for the avionics access door. Next, I'll install the platenuts. Note: I discovered that there's a brace that goes between the top of the bulkhead and the firewall. I'll have to install this somehow. It might require that I install a doubler plate along the top edge of the door opening, so I will NOT put a platenut at the top center of the door.

I also finished opening up the hole for the map-light switch in the rear cockpit. (Rectangular switch-holes -- whose brilliant idea was it to put a rectangular switch in there, anyway?) ;-) Well, it'll look nice. That's all that matters. No one will ever need to know how much time it took me.


 
Jan 28, 2008     Avionics access door; Rear cockpit map light - (5.5 hours)       Category: Fuselage
I spent a very satisfying four hours cutting a big hole in my airplane. In this case, it was the large access door that will allow access to the back of the instrument panel from the forward baggage compartment. I drilled the mounting hinge and spacer strip to the bulkhead, and also to the door, then removed them and began cutting the bulkhead with a Dremel tool. Once that was done, I filed the edges of the resulting hole to within about 1/8" of the cut-line. I clecoed / clamped the door in position, and cut the hinge pin and formed a bent handle on one end of it. The door will be secured with #8 pan-heads screws and platenuts. I thought about installing camlocs, but for the number of times I'll have to open this door, there's no sense going to all that trouble.

Next, I measured, marked, and cut out a rectangular hole next to the rear seat map-light hole for the on/off rocker switch. I'll have to enlarge the hole slightly for the best fit of the switch.


 
Jan 16, 2008     Front seat; Side console; Rear seat map light - (3.1 hours)       Category: Fuselage
I installed the final 12 nutplates that will attach the front seat assembly to the airplane. Four were under the forward cabin covers, two were in the spar cap, and six were in the under-floor structure (shown in photo #1 below). The seats are ready to paint and install.

Next, I scuffed, cleaned, dimpled, and primed the attach angle that will reside under my custom right-side console in the front cockpit. (This is the angle that would have supported the stock switch console -- which I'm not using. I'll rivet the angle to the skin in order to fill the pre-drilled skin holes, and perhaps I'll be able to attach a couple of Adel clamps to it when I wire my console.)

Next, I installed the rear seat map-light, which is an "eyeball"-type light from David Hoffman Products. The rocker switch for this light will be directly adjacent to the light fixture. (By the way, I see a lot of RV-8s with map lights mounted dead-center in this space. After sitting in the rear seat, I think moving the light a few inches aft makes it a bit more user-friendly for the rear seat occupant.)

Finally, I unpacked and played with my new empennage fairing from Fairings, Etc. (Of course, I'll have to mount the tail before the "fairing fun" really begins... a minor detail.)


 
Jan 15, 2008     Seat attach nutplates; Flap microswitches - (3.2 hours)       Category: Fuselage
The first thing I did this evening was finish installing the nutplates on the forward floorboard and the front seat pan. There are still some more nutplates to be installed in the floor structure itself.

Next, I designed and fabricated an attach angle and a striker plate for the two flap microswiches. The angle will be bolted to the bulkhead just aft of the flap motor, and the striker plate will be attached to the flap arm. When the flaps are up, one of the switches will cut off power to the "up" part of the flap circuit so the flap motor shuts off, and the other switch will signal the trim system to go to "cruise" mode (which will lower the sensitivity of the trim at higher airspeeds).

At about this time, I ran out of fuel for my shop heater. It got cold pretty quickly in there.


 
Jan 10, 2008     Front seat; Smoke system - (1.5 hours)       Category: Fuselage
This evening I finished riveting most of the nutplates on the front seat support ribs. I also finished prepping and priming the other components of the front seat. All that remains is to rivet on the nutplates that attach the forward part of the seat pan to the aft part and a few more in the floor structure. The front seat will then be ready for painting and final installation, when the time comes.

While the primer was drying, I located and drilled the five holes in the belly skin where the smoke-oil reservoir vent port will go. The port itself will be riveted on much later.


 
Jan 08, 2008     Front seat - (2.0 hours)       Category: Fuselage
Spent a couple of hours installing the various nutplates that will attach the front seat to the floorboard and the aircraft structure.


 
Jan 07, 2008     Gear tower bolts; Mid-cabin covers - (3.4 hours)       Category: Fuselage
It was over 60 degrees outside today, and the workshop was balmy! Weird!

I began by drilling the 7/16" gear bolt holes in the floorboards, using the gear tower weldment holes as a template.

The rest of the evening, I installed the nutplates under the left and right mid-cabin covers. (I miss having the fuselage on the rotisserie -- bending over to install the platenuts is back-breaking after a while.)


 
Nov 30, 2007     Fuel selector; power outlet; headphone jacks - (1.8 hours)       Category: Fuselage
I finished drilling the holes for the nutplates that will mount the left mid-cabin covers, then installed the two #8 nutplates in the aft fuel selector attach angle.

Next, I drilled a 7/8" hole in the bulkhead just behind the rear passenger's right elbow, and test-installed a 12V power outlet. The rear-seater will be able to use this for a GPS, a gooseneck map light, an iPod, or whatever. [Later superseded.]

While I was back there, I drilled two 3/8" holes on the bulkhead just forward of this for the rear seater's headset jacks.

Finally, I scouted for the ideal location for the overboard drain hole for the smoke system. The most likely location will be on the belly, under the forward edge of the rear baggage compartment floor.


 
Nov 29, 2007     Rear seat throttle; fuel selector - (2.3 hours)       Category: Fuselage
A few days ago, when I installed the rear seat throttle mounting plate, one of the platenuts seemed to be defective or stripped. Today I removed the plate and found that when I installed the nutplates, a #10 nutplate had apparently been mixed in with my drawer of #8s. Yep, that'll do it. Needless to say, I removed it and replaced it with a #8. I also finished trimming the pushrod holes in the bulkheads and the F-804 vertical channel cap. I prepped and primed the throttle arm, the pushrod, the throttle mounting plate, and the shims for the mounting plate. While they were drying, I un-clecoed and removed the UHMW anti-wear plates and widened the inboard side of the throttle-arm slot by 1/32", and also lengthened the front end of the slot by 1/8". This will make sure the rear-seat throttle does not rub, and does not limit the throw of the front-seat throttle.

Next, I worked on the Andair fuel selector mount some more. I drilled the aft support angle for two #8 nutplates, countersunk all the holes in the longerons that will eventually take rivets, then prepped and primed both support angles and the valve mounting plate. The valve mount is pretty much ready to install now, followed by the fitting of the fuel lines.


 
Nov 28, 2007     Fuel selector - (5.5 hours)       Category: Fuselage
Tonight, I began the installation of the Andair fuel selector. Since the plans do not cover the installation of an aftermarket Andair valve, this is one of those times when you just have to make everything work. Complicating the issue somewhat is the fact that I'm installing a Grand Rapids EIS unit just aft of the selector valve. (I don't want it on the main instrument panel -- I think it's sort of hideous-looking, and it's not required to be very accessible). After laying out the EIS mounting location, I proceeded to lay out the valve location.

I used a 4" x 5-1/2" sheet of 0.063" aluminum, supported by a length of 3/4" x 3/4" angle and the stock support angle, to actually mount the valve (See photos). Getting everything to fit just right, and also avoid conflicts with the pre-drilled holes in the mid-cabin cover, is a bit of a head-scratcher at times. It all came together, and the valve, support angles, and spacer plate are mostly ready to rivet and screw together when the time comes.


 
Nov 27, 2007     Rear seat throttle - (3.3 hours)       Category: Fuselage
Today I made good progress on the rear seat throttle installation. I began by continuing to enlarge the holes in the bulkheads where the throttle pushrod passes through. This is a repetitive process -- you have to file the holes a bit, test-fit the front-seat throttle, remove everything, file a bit more, etc.

When it looked like I was getting pretty close to the right dimensions for all the holes, I fitted the rear seat throttle assembly, the pushrod, and finally the front-seat throttle quadrant. After hooking them up, I played with my new moving parts for a bit, noting where a few more slight adjustments need to be made. One of these is the rear throttle arm slot -- it needs to be slightly lengthened at the forward end, because it hits the forward stop at the same time as the front throttle. I want to make sure the front throttle hits its stops first. I also want to widen the aft throttle arm slot slightly, so more of the inboard UHMW strip is exposed. As the strip wears, I don't want the throttle arm to begin scraping on the edge of the slot.

I finished up by fitting the left vertical channel cap, marking it, and notching it for the pushrod.


 
Nov 26, 2007     Rear seat throttle - (1.0 hour)       Category: Fuselage
Resumed work on the rear cockpit throttle installation. I began by cutting out the templates for the side bulkheads where the throttle pushrod will go through them. I marked and centerpunched these three locations, then drilled holes, gradualy increasing them to 1/4".

I assembled the front seat throttle and attached it to the front cockpit sidewall, then ran a string though the holes in the bulkheads, attaching it to the throttle arm on each quadrant. Using the string as a guide, I marked where I would need to trim the bulkhead holes, and began enlarging them.


 
Nov 15, 2007     Rear seat throttle - (3.1 hours)       Category: Fuselage
I began this evening's work by drilling the throttle cover plate for the nutplates, then I scuffed, cleaned, and primed the plate. Once it was dry, I installed the nutplates.

Next, I cut off 1" of the top of the throttle arm, re-drilled a new 3/16" hole for the knob about 5/16" down from the top, and bent the arm. (I bent it to about 60 degrees instead of the angle specified -- I think it looks better, and will prevent the rear seat occupant from getting his/her hand pinched.) I fitted the arm to the plate with the required hardware, and decided to file another 1/16" from the inside edge of the slot in the armrest.

After drilling the attach holes in the UHMW strips, I clamped the strips to the armrest and drilled through them into the armrest. Then I removed the strips, countersunk the holes in them, and deburred and dimpled the holes in the armrest. I had to use a pop-rivet dimpler tool for this task.

When the plate was screwed in place, I noticed there was a gap between the throttle plate and the vertical bulkheads. The gap was only on the fore and aft side of the plate (not the top), and was a result of the way the QB fuselage was put together at the factory. I decided to fabricate a couple of shim strips from 0.063 aluminum stock. This did the trick. Everything fits well now.


 
Nov 09, 2007     Rear seat throttle - (3.3 hours)       Category: Fuselage
I'm still waiting for an order of 0.063" aluminum for my fuel selector project, so tonight I started tackling the aft throttle installation. The plans for this item are very complete and detailed -- much like the empennage manual was. They are a refreshing change from the somewhat generic manual for the airframe kit that I've been following for the past year or so.

I began by drilling the required 3/16" holes in the front and rear throttle arms. Then I measured and cut the slot in the rear armrest, using a Dremel tool and widening it to its final size with various small files.

Next, I removed the top platenut on the F-806 bulkhead where the throttle cover plate will go, fabricated the pushrod, and cut the UHMW anti-chafe strip into two 5" pieces.

I finished up the evening's work by marking, clamping and drilling the throttle mounting plate into the fuselage.


 
Nov 08, 2007     Front seat; Rollover bar; Mid-cabin covers; Pedals - (6.2 hours)       Category: Fuselage
I completed the front seat-back by squeezing the remaining rivets with a friend's longeron yoke.

Next, I fitted and drilled the WD-814 rollover bar, then removed it de-burred all the holes. I also touched up the paint on one area of the bar where it had rubbed through and was showing bare steel. I also trimmed and deburred the F-8104 support rib for the rollover bar.

Next, I bent the F-881 mid-cabin covers and drilled and clecoed them in place. This allowed me to fit, drill and cleco all the front seat pan parts (F-879, F-880A and F-880Bs) in place. While I was dealing with the seat pan, I drilled out the inserts in the crotch strap on my Hooker harness. I'll replace these (somehow) with thinner inserts later.

I got my rudder pedal extensions back from the machine shop, where they'd been bent to about 15 degrees. (One was actually overbent a bit, so we bent it back slightly with a giant 50,000 lb. hydraulic press. Gotta love BIG power tools. Arrr. arrr.) I cleaned up the extensions and polished them, then filed and polished the rudder pedals. then I prepped and primed the contact surfaces of the two parts, and riveted everything together. I think they look really nice! It'll be a shame to powder coat them.

Finally, I began planning the installation of my Andair fuel selector.


 
Nov 07, 2007     Front seat; Rear seat - (4.5 hours)       Category: Fuselage
I pulled all the front seat parts out of the paint booth and riveted them all together. Presto -- a seat! (I still have to set a couple of rivets along the sides. I'll be borrowing a longeron yoke for my squeezer from a friend tomorrow.)

Next, I fabricated both rear-seat attach pins (each is 6-1/2" long, plus 3/4" for a "handle"), and installed the rear seat so I could begin fitting the fiberglass top.

As with many of the fiberglass parts in an RV kit, it did not fit well at all. I marked and trimmed the bottom and side edges until it would fit the seat back (somewhat), then marked and trimmed off the top edge so it would clear the seatbelt slots in the bulkhead. After that, it was just a matter of fitting, trimming, and filing -- again and again until it fit. My Dremel tool, portable belt-sander, and hand files got a good workout today. The critical parts of the rear seat are done -- now it'll be a matter of fine-tuning everything, attaching the support-angle and doublers, and building up some parts of the back of the seat with resin and flox to prevent excessive rubbing on the aluminum bulkhead structure.

The fitting process is pretty straightforward. It just takes time. Don't forget to wear a dust mask. My hangar and clothes were covered with fine dust when I was done. And I smelled like resin.


 
Nov 06, 2007     Front seat; Rear seat - (4.0 hours)       Category: Fuselage
Today I completed the front seat assembly. First I fabricated a hinge pin (10-3/4" long total, bent 3/4" from one end to provide an easy-to-use "handle"), then I installed the front floorboard in the fuselage. Next, I mounted the seat to the floor and clamped the seat's top angle in place with the required 1/8" clearance from the WD-808 roll bar. Then I removed the seat and drilled the angle to the seat.

After this, I un-clecoed everything, deburred all 6 parts (seat back, two side angles, top and bottom angles, and the hinge), and Scotch-brited/cleaned/primed them all.

Finally, I riveted the seat rails to the rear seat back, primed the attach hinges, and clecoed the hinges to the seat. I'll rivet the hinges next time, and also begin fitting the fiberglass part.


 
Nov 05, 2007     Front seat - (4.5 hours)       Category: Fuselage
This evening I began by doing a slight modification to my front seat -- I beveled the corners of the corrugations on the seat-back. This will eliminate any sharp edges from the seat skin that might rub on the back seat occupant's legs.

Next, I fabricated the F-832B and F-832D top and bottom seat angles, and the F-832E attach hinge.

I clamped, drilled, and clecoed the seat skin to the side rails, then drilled and clecoed on the bottom angle and attach hinge. (I had to re-make the hinge because, once again, Van's drawings depict the hinge eyes in the wrong place, just like they do on the bottom of the rear seat.)

Finally, I put the front floorboards in the fuselage and fitted the front seat in place. It all fits very well! It's almost time to climb in and make airplane noises...


 
Oct 30, 2007     Roll bar; Rear seat; Rudder pedal extensions - (5.7 hours)       Category: Fuselage
I began the process of spreading the rollover bar today. (It must be spread 1/4" to fit the fuselage.) I stood it on the floor and attached a pair of ratcheting tiedown straps to each side, then attached these to some steel columns in my hangar. I was able to spread the bar 1", but after releasing the pressure, the bar sprang back most of the way. I plan to leave the bar spread like this for the next two days while I'm away, then see how the spring-back goes. If I can't get good results this way, I'll have to locate some heavier-duty straps and ratchets. I've heard that I'll need about 3" of spread to get a 1/4" final result.

Next, I fabricated the F-833E seat-back angle and F-833F doubler for the rear seat, then drilled the F-833B L/R rails to the F-433A seat back. I clamped the two hinge segments to the bottom of the seat-back, and test-fit them into the fuselage. I'll attach the hinges next time.

Finally, I continued working on my custom pedal extensions. I trimmed the components, clamped and drilled them together, deburred them, and marked them for lightening holes. I also marked them for a 20 degree bend and attempted to do the bends. That's where my small bending brake demonstrated its limitations. Despite its best efforts, it was unable to put even the slightest bend in the 1/8" aluminum sheet. I'll have to borrow a friend's large, industrial brake next time.


 
Oct 29, 2007     Flap shaft cover; Rudder pedal extensions - (2.9 hours)       Category: Fuselage
Today I completed the custom cover over the flap actuator shaft by trimming it to its final shape, drilling it to the fuselage structure, and installing #6 nutplates in three locations (two on the aft side of the bulkhead, and one under the armrest. I attached the cover with three pan-head screws. It's amazingly strong.

Next, I began construction of a set of pedal extensions -- yet another customization I ripped off from other people. (Isn't the internet great?) First, I measured my rudder pedals and took measurements from a photo, then transferred the measurements to a heavy sheet of 0.125" aluminum. The extensions themselves will be 3" high x 4-1/2" wide, and each one will have a front lip riveted to it that will be 1" high x 4-1/2" wide. I cut out the four pieces with a hacksaw, then polished the edges.


 
Oct 28, 2007     Flap shaft cover; Elevator pushrod; Bellcrank mount - (5.1 hours)       Category: Fuselage
I began the afternoon by attaching a new M3414M rod end to the forward elevator pushrod. (The original rad end appeared to be slightly bent, so I ordered a replacement, which arrived yesterday.) I adjusted the pushrod to the required length of 30-1/8". All the pushrods are now complete.

Next, I finished riveting the elevator bellcrank mounts to the fuselage structure, using four LP4-4 blind rivets in the four locations I could not reach earlier with either a squeezer or a bucking bar.

The final project today was the main event: I designed and built a custom, removable cover for the flap motor shaft, where it protrudes through the left armrest in the back seat. I think this will prevent any issues with a backseater getting their sleeve caught in the actuator, or somehow FOD-ing the actuator inadvertently.

I started by fitting, folding, and cutting a piece of graph paper into the approximate shape I would need, then I transferred the design to a piece of thick posterboard for final tweaking. I had to make two posterboard prototypes before I got the bends and attaching tabs right. Then I transferred the design to 0.032" aluminum, cut it out, filed and sanded the edges, then bent it into the final shape. In order to make some of the bends, I created a homemade bending brake out of a steel back-riveting plate, a steel ruler, some heavy-duty clamps, and lots of manual labor. It worked great.

The final product will be attached with 3 or 4 screws.


 
Oct 25, 2007     Pedal access hatch - (2.4 hours)       Category: Fuselage
I finished the pedal access door today. First, I riveted the rest of the platenuts to the attachment ring, then re-primed the "outside" surface of the ring. Next, I dimpled the fuselage skin holes, then riveted the ring to the skin. Finally, I screwed the cover plate on.

I see one small place where I'll have to file the edge of the cover plate a tiny bit to maintain a perfect seam width, but other than that, the cover fits very well.

I know this was a relatively simple modification among all the others I've done (and will do), but I'm especially pleased with the way this one came out.


 
Oct 24, 2007     Pedal access hatch - (4.8 hours)       Category: Fuselage
Today, I finished drilling the screw holes in the cover plate and attachment ring to #19 size, then drilled the ring for the nutplates. Next, I countersunk all the #30 holes in the attachment ring.

Then, it was time to make the big cut -- the hole in the fuselage. I simply laid on the floor next to the fuselage with a Dremel tool and trimmed close to the lines. As always, it feels odd to hack a big hole in a nice, perfect skin. Once I'd cut a rough hole, I used a notching tool, a 2" drum-sander, and various files and sandpaper to finish off the edges of the hole.

I dimpled the cover plate and attachment ring, and as I expected, they both curled quite significantly in the process. I spent about 30 minutes flattening them by hand. (I've found this to be the best way to do this. There is no tool or process I know of that allows the required level of finesse). I clecoed the attachment ring to the fuselage skin and fine-tuned the fit of the cover plate. It looks really good!

Finally, I primed the attachment ring, the inside of the fuselage skin along the line of rivet holes, and the inside of the cover plate.


 
Oct 23, 2007     Pedal access hatch - (5.2 hours)       Category: Fuselage
Today, I did a lot of work on the pedal access hatch. First, I marked the access cover for 20 holes, then clamped the plate and attachment ring together. Then I drilled, clecoed and deburred all 20 holes. These will eventually be drilled-out and dimpled for #8 flush screws.

Next, I decided to check the clearance of the plate and its attachment ring, since it will be very near the NACA air scoop and various fuselage longerons. I taped the NACA scoop in place, then taped on the access plate and ring. I found that I had to trim the edge of the ring in two places. I filed a shallow notch around the bottom of the air scoop, and trimmed a bit off the forward bottom edge of the ring.

Next, I marked and center-punched the attachment ring for the 46 rivets that will attach it to the fuselage skin, then cut out the interior hole of the ring, and filed and sanded the edges. I taped the ring into the fuselage and drilled/clecoed the #40 holes through the ring and fuselage skin. Next, I deburred the ring and skin, then taped the ring onto the outside of the skin and marked the location of the future screw holes onto the skin. Then I removed the ring and taped the cover plate on the skin, using the small hole marks as a guide. Finally, I traced the edge of the cover plate onto the skin. I'll cut the large hole in the skin next time.


 
Oct 23, 2007     Flap rods - (.4 hour)       Category: Fuselage
A few weeks ago, I received a set of aftermarket flap rods from Avery Tools, and today, I temporarily attached the rod ends and attach hardware. I will eventually prime and paint the rods, but I wanted to test-fit the hardware. I will have to replace the stop nuts in the photo with the proper thin-profile type called out in the plans. These appear to be missing from my hardware bins.


 
Oct 20, 2007     Pedal access hatch - (.5 hour)       Category: Fuselage
This evening, I had time to measure and cut out the attach ring for the custom rudder pedal access hatch. Next time, I'll cut out the interior portion of the ring and start drilling the attach holes.


 
Oct 18, 2007     Fuselage access port; Elevator pushrod - (.7 hour)       Category: Fuselage
After a lot of thought, I've decided to do another custom installation: A 5" x 8" removable access plate on the left side of the fuselage (just below the NACA duct) that will give me access to the rudder pedal and fuel pump area. This will be helpful when it's time to service the fuel filter and the brake reservoirs on the pedals. The hole in the fuselage will be about 3.5" x 6.5", with a reinforcement ring and nutplates around it. The reinforcement ring will be riveted to the fuselage skin with flush rivets. I laid out some nutplates on the cut-out cover plate to see how many I'd need. Via some eyeball engineering, it looks like 20 will do.

I began by cutting out a cover plate from 0.032 sheet. This matches the thickness of the fuselage skin. The plate will be fastened to the fuselage with 20 #8 flush screws.

I also began laying out the reinforcement ring on a sheet of spare 0.040.

Finally, I ran a tap through the end of the pre-made F-839 elevator pushrod -- the one that had bad threads on one end. It works fine now.


 
Oct 15, 2007     Smoke reservoir mount / baggage floorboard - (1.0 hour)       Category: Fuselage
This evening, I riveted the smoke-oil reservoir doubler plate and nutplates to the aft baggage floor, and attached the attach angles with 1/4" bolts. Then I countersunk the holes under the reservoir that will take flush blind rivets, attaching the floor to the longerons. With the exception of painting, the floor is basically ready to install.


 
Oct 15, 2007     Flap brace and flap hinge - (2.1 hours)       Category: Fuselage
I riveted the flap brace to the wing, using MSP-42 blind rivets everywhere except the inboard three rivets, which were heavy-duty flush Monel Cherry rivets. (This is a Quickbuild procedure. Standard builders use different rivets here.)

Next, I riveted the flap hinge, brace, and wing skin together using MS1097AD4-4 rivets (1/8" Oops rivets). See the 9 October 07 entry for an explanation. The hinge looks great, and you can't tell I made a drilling mistake. Sweet!

I made a test attachment of the flap to the wing. It went on just like the left one. I did fight a bit with the curved top skin of the flap, however, so I curled it by hand, taped it in that position, and left it overnight to see if I can persuade it into the right shape.


 
Oct 10, 2007     Smoke system - (1.1 hours)       Category: Fuselage
I prepped the aft baggage floor, the doubler plate, and the reservoir attach-angles for assembly, and prepped and primed the attach angles. Because the reservoir will sit flush on the floor, the blind rivets that attach the floor to the airplane might rub on the reservoir. I decided to try putting some washers under the angle pieces to lift them up far enough to clear the rivet-heads. (I ground them down enough to clear the nutplate holes.) In theory, this would work, but after thinking about it for a while, I realized this might put undue stress on the four small contact patches under the washers. Therefore, I'll simply countersink the floorboard and install flush blind rivets to attach it to the airplane. Problem solved.


 
Oct 09, 2007     Smoke system - (1.0 hour) Category: Fuselage
Prepped, cleaned and primed the lower aft baggage floor in preparation for riveting on the doubler plate and reservoir tank attach-angles.
 
Oct 08, 2007     Smoke system - (1.0 hour) Category: Fuselage
Cut out a 3/4" hole in the floor of the aft baggage compartment for the smoke oil line and power-supply wire(s) to pass through. Rounded the edges of the doubler plate, then prepped and primed the plate in preparation for painting. (Nice alliteration, eh?)
 
Oct 04, 2007     Smoke system - (.5 hour) Category: Fuselage
Not much time today, but I think it's important to do something -- no matter how small -- if you can.

I had time to drill and deburr the holes for the rivets that will go along the edge of the reservoir doubler plate. I also planned where the oil line will pass through the baggage floorboard, and began to investigate where I might be able to route the oil line all the way to the engine compartment. The spar will be interesting to get around.
 
Oct 03, 2007     Elevator bellcrank - (.8 hour)       Category: Fuselage
I decided to see how many rivets I could set on the new elevator bellcrank. The answer is six, before I ran out of room to get the squeezer or a bucking bar in there. The nice folks at Van's said that either Cherry Max rivets or AN3 bolts with stop-washers would be fine for those last four holes.


 
Oct 03, 2007     Smoke system - (2.0 hours)       Category: Fuselage
After looking at the fuselage structure under the baggage compartment, and thinking about all the various ways I could install the smoke oil reservoir, I've decided to mount it dead-center in the baggage compartment. The support is best there, and the implications are least. There will still be plenty of room on either side of the reservoir (and on the back shelf) for tool bags, soft-sided luggage, lawn chairs, and whatnot.

I fabricated a doubler plate from 0.040 and drilled it to match the hole pattern already in the floorboard, then drilled it for four 1/4-20 nutplates -- the four points where the reservoir angles will attach to the floor. I also marked the doubler for the locations of the rivets that will attach it to the floor. (The doubler will be a permanent part of the floorboard, but the angles will be removable.) For reference, the size of the doubler is 11-1/8" x 15-1/8".


 
Oct 02, 2007     Avionics access door; Smoke system - (2.1 hours)       Category: Fuselage
I trimmed the avionics access-door to its final size and prepped it for drilling to the bulkhead. (Before I drill it and cut out the access hole, though, I want to make sure I'm not getting ahead of myself. That bulkhead will be very floppy after I cut it, so I want to make sure this won't affect the fitting of anything else, like the top skin.)

I did cut the 1/2" wide strip of 0.040 that will go under the lower half of the door hinge.

Next, I began planning the installation of the smoke system. (Mine is a model SA-100 from SmokingAirplanes.com). I might copy what one of my buddies did, and mount the reservoir along the left side of the rear baggage compartment, with the pickup tube at the back end. The oil line will go underneath the floorboards somehow.

I'll also think about mounting it on the centerline of the airplane. Not sure yet.

[Note: I ended up mounting it on the aircraft centerline.]


 
Oct 01, 2007     Avionics access door - (3.3 hours)       Category: Fuselage
While the paint dries on some other parts, I decided to begin fabricating an avionics access door that will go in the bulkhead between the instrument panel and the firewall. I began by taking a bunch of careful measurements of the bulkhead, then I spent some time planning the operation of the door and the details of its construction. (It will hinge at the bottom, and the door will open forward, into the baggage compartment. I think I'll fasten it with #8 screws and nutplates, but I'll look at quarter-turn fasteners, too.)

I measured and drew the design onto the bulkhead so I can cut out the opening, and also copied the door dimensions onto a sheet of white posterboard. After checking the clearances and verifying that my concept will work, I then used this "posterboard door" as a template to cut out the actual door from a sheet of 0.040 aluminum.

I also cut the -P3 hinge that will mount the door. By the way, for reference, my door will be 23.5" across, 6.5" high in the middle, and 4" high at the outside edges. The actual opening in the bulkhead is 3/4" less than this on the top and sides. That's where the nutplates and reinforcing ring will go.

You might notice that the opening will not quite reach the tops of the indentations in the bulkhead. That's OK, because the door will cover this area, and the nutplates will be located between the indentations.


 
Sep 30, 2007     Static ports and lines - (.6 hour)       Category: Fuselage
My friend Jim came over and drove the eight rivets that attach the static ports to the skin. I bucked from inside. It was pretty uneventful. We caught the edge of the left port with the rivet set while driving one rivet, but it barely shows. (In the Navy, is the left port the "port port"?)

Next, I attached the 90-degree static line fittings to the port, and hooked up the connecting line.


 
Sep 30, 2007     Elevator bellcrank attach angles - (3.7 hours)       Category: Fuselage
Yesterday, when I clamped the old and new elevator bellcrank attach-angles together, and drilled them, I made an assumption I shouldn't have made. I wrongly assumed the pre-existing angles were made correctly and perfectly. It's easy to get in this mindset with the Quickbuild kit.

I discovered that when the Filipinos built the attach angles, they must have drilled them into the fuselage, THEN drilled the 1/4" elevator bellcrank holes. This is certainly an efficient method for factory production, but it's something I never would have done myself. Couple this with a somewhat poorly-made set of TruTrak attach angles, and I found that some of the holes in my angles didn't line up very well, even after they were carefully match-drilled to the old angles (see Photo 1). After clecoing the new angles into the fuselage, I discovered that all three holes on the upper part of the angle were off by exactly 3/32".

I decided to fabricate another right-side angle and move the three offending holes forward 3/32". My idea worked perfectly (Photo 2), although I must say that it was interesting and educational trying to get all the holes located exactly where they needed to be, simply by measuring -- not by back-drilling through the already-drilled structures they'll be attached to.

I took care of another attach-angle related oddity: The new, longer elevator bellcrank angles would not lay flush on the longerons because the edge of the nearby bulkhead interfered. A couple of passes with a Dremel tool and some files took care of that.

Finally, I primed all the stuff I did today. A good day.

Photo 1: The bellcrank bolt barely went through the supplied attach angles....
Photo 2: ..so I made the one on the left from scratch to fix the problem. Now the bolt slides right though.
Photo 3: I had to cut off the bent edge of the bulkhead so the attach angles would clear.


 
Sep 29, 2007     Autopilot pitch servo mount (v.1); Elevator bellcrank - (1.9 hours)       Category: Fuselage
Today I began installing the TruTrak autopilot pitch servo and the elevator bellcrank. I began by drilling the old, stock bellcrank attach angles out of the airframe. (It always seems strange to un-do work that was so carefully done in the Philippines for my benefit, and for which I paid good money.)

Next I mated the old angle mounts with the new ones provided by TruTrak. I clamped them together and drilled the mounting holes in the new angle, then deburred them.

Next, I test-assembled the bellcrank and the autopilot servo components. I wanted to make sure I understood exactly where everything goes. It's tough to do this by looking at TruTrak's drawings. All they show are the major components. Astonishingly, they provide absolutely no guidance as to how the included hardware is to be attached to the servo arm. I figured out where each of the bolts goes (they're all different and they only fit in one particular place, so it's pretty intuitive. There are a couple of large fender washers, though, which could go one of several places. I'll have to research this.


 
Sep 24, 2007     ELT mount; Strobe mount; Static ports/lines - (3.1 hours)       Category: Fuselage
When I installed the ELT mount on the left side of the aft fuselage, I made a decision that was to have a big impact on this otherwise simple job. I installed 5 nutplates directly adjacent to the five holes for the blind rivets that would attach the angle to the longeron. Unfortunately, that left me very little room to actually get the rivets in there. Yesterday, I tried every method and every tool I had, to no avail. Today, I bought a smaller pop-rivet tool and ground down the sides of the nosepiece so it would fit in the small gap between the nutplates and the fuselage skin. It worked. I did, however, bleed on my work today. Long story, which I won't tell here...

After finishing the ELT attach angles, I finished riveting the strobe mounting plate together. It's done and ready to mount at a future time.

Next, I cleaned, dimpled and primed the four skin holes for each static port, and countersunk the ports themselves. (Dimpling the skin by myself was fun. It involved eight trips in and out of the aft fuselage to insert and remove the pop-rivet dimpler tool.)

Finally, I cut and connected the static lines that arc over the top of the bulkhead.


 
Sep 23, 2007     Strobe and ELT mounts; static ports - (4.5 hours)       Category: Fuselage
After about two hours of drilling, cussing and sweating profusely, I'm now just about done with the ELT and strobe pack mounts.

I completely assembled the ELT mounting plate and bracket. It's ready to go. On the ELT, the only thing left to do is blind-rivet the lower attach angle for the ELT to the airplane's longeron. This is going to be tough, because there's not enough room along the side of the fuselage for a pop rivet tool, or a squeezer, or a bucking bar. Tomorrow, I'll see if anyone around here has a smaller pop-rivet tool than mine. If not, I might have to drill four new holes in-between the nutsplate. Not a big deal.

I drilled, clecoed, cleaned, primed and riveted the strobe pack attach angles to the longeron. Tomorrow, I'll rivet the nutplates and stiffeners to the strobe mounting plate (after the paint on the plate dries), and then it'll be ready to blind-rivet into the airplane when it's needed. This will be a bit later (after I paint the interior.)

Next, I drilled the 1/4" holes on the fuselage sides for the static ports. (I'm using aftermarket CreativeAir static ports, not the stock Vans port.) Then, I drilled four attach holes for the new ports, backdrilling through the ports into the skin. Tomorrow, I'll dimple the skin and countersink the port flanges. Heck, I might even rivet the ports on tomorrow.

I squirmed my way deep into the fuselage, cut off about 30" of static tube, and routed it over the top of the bulkhead adjacent to the static ports. This will connect the ports and also connect to a T-fitting. From there, a static line will eventually go forward along the left upper longeron to the instrument panel area. I'm a pretty big guy, and getting my shoulders past that third bulkhead is tight. Glad I'm not overly claustrophobic.


 
Sep 22, 2007     ELT and strobe-pack mount - (4.0 hours)       Category: Fuselage
I finished fabricating the ELT mount, including installing all the nutplates, installing the stiffener on the back of the plate, and drilling the attach-angles to the aircraft longerons. (Side note: I've noticed that people don't stop to chat when all they can see of you is your feet sticking out of the tail cone!) I also painted the mounting plate a nice industrial shade of gray.

Next, I began constructing the mounting plate for the strobe power pack, which will be installed on the right side of the fuselage, directly opposite the ELT. [Note: the strobe pack was later moved one bay forward, then removed entirely with the advent of LED strobes.]

I cut and fabricated the mounting plate out of 0.040, and made a center, vertical stiffener, just like I did for the ELT. The top and bottom angles are the same, too, except I won't install platenuts on them. Instead, the power pack itself will be removable. I drilled and installed four 1/4" nutplates for the AN4-4A bolts that go through the mounting tabs on the unit. Because the strobe unit is pretty heavy, I drilled the nutplate holes through another pair of stiffeners. I don't foresee any stress cracks on this thing, ever...

Once everything was drilled and clecoed together, I clamped the angles and mounting plate into the fuselage and began drilling them to the longerons. I'll finish this drilling tomorrow, then I'll prime and blind-rivet all the attach angles (ELT, too) into the fuselage with MSP-42 rivets.


 
Sep 21, 2007     Work floorboards; ELT mount - (4.5 hours)       Category: Fuselage
I bought a nice 2'x4' piece of birch and cut it to fit the aft fuselage, way back where the static ports, ELT, strobe power unit, and the Grand Rapids magnetometer will be.

After fitting the floor, I laid in the fuselage for a while and figured out the final location for the ELT and strobe unit. I originally wanted to mount them directly behind the lower aft wall of the baggage compartment, but there were complications with pre-existing nutplates on the longerons. Now, I'm going to mount them one fuselage "bay" aft of the baggage compartment. This being an RV-8, adding some weight aft is OK. [Note: The strobe power pack was eventually moved one bay forward.]

I measured vertically between the longerons at two locations, 6" apart, and got to work. I made the mounting plate out of 0.040 sheet, and fabricated the angles that will attach it to the longeons at the top and bottom of the plate. I'll use platenuts to fasten the whole thing, just so I can remove it for modifications later (like when the new 406 MHz ELTs come out, inevitably in a different form-factor than this one.)

The ELT bracket will be riveted to the plate. On the back of the plate, I'll rivet on a vertical stiffener, just for fun. Also, I made a spacer shim out of 0.063 stock. This spacer will go under the bracket (see photo) to give the bracket more stability. (I've never liked how these ELT mounts are designed to sort of "balance" on the metal strap that goes underneath the bracket. The spacer will fix that.) I drilled, clecoed, deburred and primed all the parts except the two attach angles. Those still have to be drilled to the longeons.


 
Sep 21, 2007     Cockpit side console - (.3 hour)       Category: Fuselage
I clecoed all the parts of the side console together. They'll get painted later, at the same time I paint the interior of the airplane. First, though, I'll have to drill the holes for the switches and have the label overlay made.


 
Sep 20, 2007     Fuselage stand; work floors, ELT mount, A/P mount - (2.1 hours)       Category: Fuselage
With the help of my buddy Joe, I got the fuselage detached from the rotisserie and lowered onto my floor-level work stand. It works like a charm -- it's very stable, and easy to get in and out of. The only thing I still need to do is to attach the tailwheel spring. Right now, the aft fuselage is resting on a heavily-padded sawhorse. I think this would actually be OK, but I'll feel better when there's no weight on the fuselage skin.

I climbed into the fuselage for the first time, and took measurements of the "bay" behind the baggage compartment. Tomorrow, I'll buy and cut a piece of 3/4" oak or birch for a work-floorboard.

I also began laying out the raw materials I'll use to build the ELT mount and the strobe power supply.

Finally, I spent some time cleaning up the edges of the autopilot pitch servo mount.


 
Sep 20, 2007     Cockpit side console - (1.1 hours)       Category: Fuselage
I finally received some more aluminum angle today, so I completed the last mounting angle for the cockpit side console. I also finished priming all the components and riveted the six platenuts to the attach-angles.


 
Sep 19, 2007     Floor stands and work floorboards - (4.5 hours)       Category: Fuselage
Today, I designed and built a couple of stands that will support the fuselage at floor level, which will allow me to crawl inside to do the remainder of the work in the rear fuselage.

The forward stand is nothing more than a couple of 2x4s, some 10"-long sections of 4x4s, and some 6" scraps of 2x4. The 6" scraps were screwed on to make narrow channels for the false, wooden spar to sit in.

The tail support will be a customized, 17-3/4" tall sawhorse. I'll rest the tailwheel spring tube in a padded notch in the sawhorse. (Tomorrow, I'll try to mount the tailwheel tube to the airplane.)

I also built a wooden floor for the inside of the fuselage out of 3/4" oak. I'll need to make another one for the fuselage bay aft of this one, but because I haven't been able to crawl in there and measure it, I don't know the dimensions of it yet.

After all the woodwork was done for the day, I installed the aft floorboards in the airplane. This will allow me get in and out without damaging anything.


 
Sep 18, 2007     Cockpit side console - (1.9 hours)       Category: Fuselage
Today, I countersunk and dimpled all the side-console components that needed it, then scuffed, cleaned and primed them. I haven't yet fabricated the final stiffener angle on the lower left side; once I receive my latest parts order from Vans in a day or two, I get to it.

Since the side console was out of the airplane, I removed both vertical channel caps from the fuselage and deburred them.

I spent some time finalizing the mount design and location for the ELT. It will go between two side longerons, in the bay directly behind the aft baggage wall. I thought about mounting it in the bay behind this (for CG reasons, mostly), but it seems like it would be a lot of effort to squirm that far back into the fuselage when I need to replace the batteries each year.


 
Sep 17, 2007     Cockpit side console; Panel planning; ELT and A/P - (3.6 hours)       Category: Fuselage
I added two stiffeners to the right side of the cockpit side console, and now the console is rock solid, even with considerable pressure applied to it -- the way a person aggressively throwing switches or climbing in and out of the cockpit might behave. I also removed one of the stiffeners that runs along the left lower edge of the console and will replace it with a beefier one. This is the edge of the console that my right leg will probably rest against in cruise flight, and I don't want it to flex at all. This thing will probably be WAY overbuilt, but I think that's OK.

I began countersinking and dimpling the various components of the console where needed, and I scuffed and primed several attach angles.

Then I spent a rewarding hour laying out switches and panel components to get an idea of how much room I actually have on the side console and the side instruments panels. I drew some layouts and rearranged switches based on how I think I'll use them. It's interesting how my perception of good a layout has changed now that I can actually see the components and the space they'll occupy.

Finally, I spent some time laying out the autopilot pitch servo and ELT, and planning how I'll mount them in the aft fuselage.


 
Sep 14, 2007     Cockpit side console; Cockpit paint tests - (3.4 hours)       Category: Fuselage
Since I'm still waiting for a couple of parts for my wings, I moved over to the fuselage today, and began the process of mounting of my custom right-side console to the fuselage.

The panel will be attached in the following locations:
1). Four screws through the lower lip of the right side panel, and 2). At least four screws through two aluminum angles on the vertical channel caps.

All of the mounting screws will be held with nutplates, and I'm engineering everything so the console can be removed easily if I ever need to replace a switch someday.

I began engineering the whole thing by drilling the four under-panel holes and getting them prepped and countersunk for nutplates. Then I fitted some of the attach angles and understructure that will support the console and give it a lot of strength. I'd still like to come up with a way to fasten everything to the original attach angle that's riveted to the skin below. I'll work on that soon.

Finally today, I stripped several parts of the throttle quadrant that I test-painted yesterday. The clear coat I sprayed caused them to bubble in a strange way, so back to the drawing board. I sanded and re-painted them. No clear coat this time.


 
Sep 13, 2007     Cockpit side console; Interior paint test - (.7 hour) Category: Fuselage
I spent some more time filing and carefully fitting my custom side console. I think I have it to the point where I'm happy with the way it fits. I've been trying to get a minimal gap between the console and the side skin, and also between the console and the channel cap. The issue has been that the side skin is concave, and the face of the channel cap is slightly convex. Straight lines do not work here. I've had to file/test-fit/file/test-fit etc.

The second fuselage task involved painting the five components of my throttle quadrant assembly with a certain gray color. Next, I'll paint a sample piece with the lighter gray paint I've picked out for the rest of the cockpit. I'm hoping the the contrast will be subtle, but noticeable and attractive. Some people say gray is boring, but I think it gives a cockpit a military look, which I like. I'll post photos later, when I finalize the colors.
 
Aug 10, 2007     Right side console - (.8 hour) Category: Fuselage
Resumed work after a few weeks off for Oshkosh and other distractions. It feels good to be back at work on the airplane!

Continued filing and fitting the right side console so it fits really well. It still needs some tweaking, but it's getting closer each time I work on it.
 
Jul 11, 2007     Right side console - (3.5 hours)       Category: Fuselage
In order to finalize the exact location, size, and shape of the side console, I had to attach the instrument panel. I cut and filed the F-803CPP attachment flange as specified in the plans, then clecoed the flange to the panel assembly. Next, I drilled and clecoed the small flange segments at the lower corners to the fuselage skins, which established the tilt of the panel.

With the instrument panel in place, I finalized the dimensions of the side console by carefully trimming, filing, and sanding it. As I mentioned in a previous entry, I didn't like how the console extended aft beyond the F-804N channel cap by about 1 inch, so I cut the aft end of the console off and fabricated a new aft end-piece for it. Now it sits flush with the aft edge of the channel cap. I think it looks a lot better -- not to mention the fact that now I'll be able to utilize the space aft of the console for a map case.

Just for grins, I held the WD-814 rollover bar in place on the fuselage longerons to check its fit. It looks like it'll have to be spread by about 1/4".


 
Jul 06, 2007     Right side console - (2.9 hours)       Category: Fuselage
Since the top of the custom right-side console will mate up with the right instrument subpanel, I need to fit the entire instrument panel to the airplane. After doing so, I found that the cardboard prototype of the console I'd made a week ago was a little off. As a result, I spent a couple of hours trimming, test-fitting, and re-trimming the console so it would fit perfectly.

It's not quite perfect yet, but it's getting close. The aft end of the console protrudes past the F-804 channel cap about 1". I think I'll end up trimming the back end off the console, and fabricating a new back-end for it.

My work was interrupted by a great offer to fly my neighbor's Woody Pusher. Of course I gratefully accepted. Nothing like a little open-cockpit flying on a beautiful day to regain some perspective. I love this airport!


 
Jul 05, 2007     Side consoles; Channel cap - (2.0 hours)       Category: Fuselage
Riveted the attach angles to the flap switch console and the top of the throttle quadrant.

Fabricated the sloped attach angle for the stock right-side console and drilled/clecoed it to the fuselage skin . I'll use this as the basis for an attach point for my custom side console.

Fitted, drilled and clecoed the right-side vertical channel cap (F-804).

Since it's almost time to install a bunch of stuff back in the tailcone, I measured the floor of the fuselage near the baggage area in preparation for cutting temporary oak floorboards. I also procured a wooden pallet that might work as the base of a temporary fuselage stand.


 
Jul 04, 2007     Right side console - (1.2 hours)       Category: Fuselage
Fitted and drilled some of the attach angles to the inside of the right side console, then fitted the assembly to the fuselage to check how it fits and what sort of method would be best to attach it all to the cockpit sides and instrument panel.


 
Jul 03, 2007     Right side console - (.7 hour) Category: Fuselage
Fabricated attach angles for right side console.
 
Jul 02, 2007     Right side console - (2.0 hours) Category: Fuselage
Trimmed and finished the edges of the right side console, then made the various bends. Began planning the rest of the installation.

Took measurements off the fuselage and the false wooden spar in preparation for building a floor stand for the fuselage. (I need to have a firm base so I can climb in and begin constructing mounts for the ELT and strobe power units; and installing the static system, rudder cables, elevator bellcrank and autopilot servo.)
 
Jun 27, 2007     Left and right side consoles - (2.0 hours)       Category: Fuselage
Prepped and primed all the throttle quadrant pieces, then installed nutplates. I had to turn some platenuts to maintain edge distances.

Laid out and cut the 0.040" aluminum for the right side custom console, and did a bit of planning for the underlying structure that will attach it to the cockpit sidewall.


 
Jun 26, 2007     Left and right side consoles - (2.2 hours)       Category: Fuselage
Today I drilled the nutplate holes in the left console attach angles, then drilled the 29/64" hole for the flap switch into the console itself.

Next, I polished, roughed, cleaned and primed all the parts for the flap switch console and installed the three nutplates. (I also test-fit the flap switch. I couldn't resist.)

Finally, I spent some time messing with the right side console. I had originally thought it would be nice to extend the right console aft, all the way to the aft end of the right armrest, tapering in width the whole way. The problem with that plan is that I wouldn't be able to have a map pocket underneath the right armrest. Since space is at a premium in the front seat of an RV-8, I'll need that map pocket. Therefore, I think I'll extend the console only to the aft side of the mid-cabin side cover (see Photo 2 below). Once I cut off the cardboard template, I took dimensions of the various parts that will have to be built. I'll get started on cutting metal next time. I also need to figure out how to brace the console to the aircraft structure.


 
Jun 25, 2007     Flap switch console - (2.1 hours)       Category: Fuselage
Tonight I partially mounted the flap switch console. First, I engineered how it will be mounted. (It was a little challenging because there's no access to the left or forward sides of the console. I briefly thought about mounting an attach-angle to the fuselage skin, but I figured out a way to do it without drilling any holes in the skin.)

I made two angle pieces for the bottom of it, left and right. One will be riveted to the throttle quadrant, and the other will be riveted to the sloped console itself. Then, screws/nutplates will actually attach it to the throttle quadrant. There was a lot of head-scratching and improvising tonight, because I couldn't put clecoes on the quadrant/console assembly while it was in place in the airplane. I used some tape and creative placement of clecoes.

The outboard attach screw will be a challenge to get to, if I ever need to replace the flap switch, but it'll be do-able with a flashlight, mirror, and a flexible extension bit. It's outboard and forward of the control cable anchor -- not an easy place to get to, but I think it's better than mounting a screw though the skin.


 
Jun 24, 2007     Flap switch console - (1.7 hours)       Category: Fuselage
This evening's work with my custom flap-switch console was very satisfying. I cut out and fitted a thin cardboard template in the cockpit, fitted it with the actual flap switch I'll be using (to check clearance and ergonomic issues), tweaked everything until it all fit well, then transfered the design to .040 aluminum, cut it out, bent it, and began fabricating some angles to attach it. My plan is to attach it with 4 screws and platenuts through two angles mounted on the top of the throttle quadrant below it. The new console is very sturdy, and it doesn't seem like it'll need any additional attach points.

This sloped console looks great, in my opinion. The flap switch seems like it will be out of the way, yet easy to reach. I'm very happy with the results of this mini-project!


 
Jun 20, 2007     Flap switch console prototyping - (.5 hour)       Category: Fuselage
I fiddled with cardboard and scissors again this evening. I ended up prototyping and fitting a small angled console just forward of the throttle quadrant. This console would allow me to mount the throttle quadrant in the stock location, but still allow the flap switch to be in an easily-accessible place (which is one of the main things I wanted to accomplish in the first place with an angled side console).

Next, I'll transfer the design to thin posterboard for final testing, then to 0.032 or 0.040 aluminum.


 
Jun 19, 2007     Throttle cable anchor, v.2 - (2.2 hours)       Category: Fuselage
I received a hunk of replacement aluminum-angle stock from Vans today, so I fabricated a new F-864E Cable Anchor to replace the one I hosed up last week. This one took less time to make than the first one, and it looks great. I drilled and clecoed it into place on the throttle quadrant cover.

Next, I drilled and clecoed the quadrant cover to the left gear tower and the F-804C flange.


 
Jun 16, 2007     Throttle quadrant, left side console and cover - (1.7 hours)       Category: Fuselage
After sitting in the cockpit of a friend's RV-8 today, I made a couple of big decisions regarding the placement of my throttle and the sloped side console. I don't believe the sloped panel on the left will work -- it would place the throttle quadrant too close to my leg and too far aft. In cruise flight, when my leg relaxed outward, it would end up resting against the mixture control, which would not be good. The aft positioning of the engine controls would also be just a bit awkward, especially at lower power settings. Therefore, I decided to leave the throttle placement alone and not install a sloped console on the left. (A lot of thanks must go to Don Pfieffer and Jim Gray, whose advice was very helpful in my decision-making process.)

The right console will remain, but it will extend back only about 9 inches so it doesn't block the map case I'll fashion near my right elbow.

After all that brain-work, I drilled and clecoed the mid cabin cover and the horizontal throttle-attach angle to the fuselage.


 
Jun 14, 2007     Throttle quadrant - (1.75 hours)       Category: Fuselage
Fabricated F-864C mounting angle for the throttle quadrant and left console.

Installed the DJM CT-83 throttle quadrant in the left console and fitted it to the fuselage. I did this mainly to see how the position of the throttle works for my particular arm length and preferences. As I mentioned in yesterday's entry, I've been considering installing a custom-made sloping console on the left side, which would involve re-positioning the throttle. Today's test suggested that I might want to leave the left console alone and not move the throttle from where Van designed it. I have long arms, and moving the throttle aft and inboard might put it a bit too close to be comfortable. We'll see.


 
Jun 13, 2007     Cockpit side consoles - (2.1 hours)       Category: Fuselage
This evening I fabricated the F-864D angle (part of the throttle quadrant).

Next, I spent some time with cardboard, scissors and tape, in an effort to mock-up a cardboard template of my design for a side console on the right side of the cockpit. I've seen these sloped side panels on several RV-8s, and I really like them. As with many the mods I'm doing to this airplane, this one looks like it'll involve quite a bit of work.

The front part of the sloped panel will mate to the bottom of the instrument subpanel, and will be the same width. My initial design has it tapering as it goes rearward, until it's about the same width as the right armrest. I like the design -- it's simple, and there's plenty of room on it for whatever auxiliary controls I'll probably need. I need to determine if it will block my view of anything that might be mounted on the right mid-cabin cover below it. If so, I'll have to trrim it down a bit.

Next, I assembled and test-fit the stock throttle-quadrant support in order to visualize what kind of similar layout I could do there. To make a sloped console on the left, I'd need to move the throttle-quadrant about five inches aft and about two inches inboard. Will this be a comfortable position? I don't know, and I'll have to find out, from some of the people who have done it. I also have to research how I'd mount the throttle and route the control cables. There is very little information on this mod available on the web, so I'm probably going to have to engineer it "on the fly."


 
Jun 12, 2007     Throttle cable anchor (first try) - (2.4 hours)       Category: Fuselage
I have just GOT to stop working on the airplane at the end of a long day, when I'm already tired. For the second time in a month, I wasted almost a whole work period. Tonight, I fabricated the F-864E Cable Anchor, and I built it backwards. Can you spot the problem in the photo below? That dotted line on the drawing became a solid line in my tired mind. That's what I get for trying to work a 20-hour day. I'll reorder some more aluminum angle tomorrow.

On a more positive note, I successfully removed the "trim area" at the front of the F-864BPP Throttle Quadrant Cover. It would be hard to screw that up, since it's pre-notched.


 
Jun 08, 2007     Forward baggage floor - (1.75 hours) Category: Fuselage
Riveted F-870B, the left side baggage floor support angle, to the fuselage skin.

Dimpled the baggage floor and primed along the stiffener rivet lines. Riveted the remaining two stiffeners to the floor skin. Enlarged the screw holes on the floor skin to #8 size.
 
Jun 05, 2007     Forward baggage floor - (1.6 hours)       Category: Fuselage
Prepped, deburred, dimpled and primed remaining stiffeners for forward baggage floor and left side support angle. Installed platenuts on left side support angle and drilled forward support angle for platenuts.

Riveted F-870C attach angle to bottom of F-870PP baggage floor.


 
Jun 04, 2007     Forward baggage floor - (1.8 hours)       Category: Fuselage
Fitted and drilled the forward baggage floor to the support structure.

Fitted and adjusted the F-871PP forward baggage side panel. (The three already-installed platenuts in the front side of the the gear tower seem very, very tight. Even with Boelube and quite a bit of torque, the #8 screws do not want to go in past the halfway point. I'll have to investigate this further. Perhaps I'll need to run a tap through them.)

Countersunk the appropriate holes in the F-870C angle and installed the platenuts.

Dimpled and primed the right edge of the F-870PP floor, where the angle will attach.

Touched up the primer on parts of the aft cabin side covers where they were filed and sanded last week.


 
Jun 02, 2007     Forward baggage floor - (.7 hour)       Category: Fuselage
Positioned, drilled and clecoed the F-870B baggage floor support angle onto the left fuselage skin.

Today I received the smoke system from Smoking Airplanes, Inc. I put the reservoir/pump assembly into the rear baggage compartment and tried to get an initial feel for where it will fit best. The further aft I can get it, the better. (In the RV-8, the Center of Gravity tends to be forward, so I'm being fairly aggressive about moving it aft. Even though the main aircraft battery (an Odyssey PC-680) will be located forward, on the firewall, the 12-pound smoke system aft of the rear seat will more than counter that.)


 
May 31, 2007     Forward baggage floor - (1.5 hours)       Category: Fuselage
Fabricated three F-870C stiffeners and one F-870B stiffener.

Marked, drilled and clecoed the C's to the bottom of the F-870PP forward baggage compartment floor.


 
May 30, 2007     Rudder pedals / brake master cylinders - (.5 hour)       Category: Fuselage
I received my flight-adjustable rudder pedal kit from Van's today, so I spent what little shop time I had this evening assembling the pedal assembly and test-fitting the Matco MC-5 master brake cylinders I plan to install. The MC-5s have reservoirs built right in, negating the need for a firewall-mounted reservoir and the associated brake lines that must be run. This evening, I just wanted to see how everything will fit together. The shafts of the MC-5s have different types of mounting holes than the stock brake cylinders, so the installation will obviously require some slight re-engineering.


 
May 26, 2007     Flap motor installation; Floorboard trimming - (.6 hour)       Category: Fuselage
I finished the installation of the flap motor wire tubing. In order to avoid squishing the tubing between the motor and the bottom of the armrest when the flaps are in the "up" position, I had to rearrange the Adel clamps a bit. Added an Adel clamp under the floor supports to lock the tubing into position. Notched the floorboard where the tubing goes through the floor. The flap wires will be tidied up and connected much later.

Now, the tubing does not touch anything as the motor moves. Cool!


 
May 25, 2007     Flap motor installation; under-floor planning - (4.0 hours)       Category: Fuselage
Installed the flap motor and began fabricating a protective wire sleeve out of nylon pitot tubing. I attached two Adel clamps to the motor shaft, and the plan is that I will run the tubing down through the edge of the floor, using one of the unused floorboards holes. I'll cut a notch in the edge of the floorboard at that location. The tubing will be mounted so it doesn't touch anything as the motor extends or retracts. The motor wiring will run through the tube and therefore be protected from chafing and repetitive bending.

I also spent some time planning where I'll install the ELT and strobe power pack. More on this in a future entry.

Photo 1: Initial fit required making the armature hole in the armrest a bit bigger.
Photo 2: I tried several ways to mount the flexible tubing & clamps. This was an early, unsuccessful iteration.
Photo 3: Having a laptop computer with a wireless Internet connection in my hangar is very helpful sometimes.


 
May 24, 2007     Floorboard final trim and dimple - (.5 hour) Category: Fuselage
Trimmed about 1/16" off the inboard edges of the forward-aft floorboards where they slide past the rivets on the front seat belt attach points. Now they don't bind on the rivets going in and out.

I also dimpled the six screw holes in both the footwells and the skin just aft of them, where these items will be attached with flush screws.
 
May 23, 2007     Floorboards; Seat hinges; Aft cabin covers - (3.5 hours)       Category: Fuselage
Installed the rear seat mounting hinges and the three floor stiffeners that are riveted with the hinges. I decided to forego Van's instructions in one area. They call for you to attach two holes in the right hinge to the left floorboard using LP4-3 pop rivets -- rivets that would have to be drilled out in order for the floorboards to come out. Instead (you guessed it), I installed nutplates and #8 screws through the those two holes in the hinge.

I did a test-fit of the floorboards with all the stiffeners finally riveted in place. It's just a little tighter and trickier to get the left-aft floorboard in and out, but it's perfectly do-able.

Installed the rear seatbelt anchors. Since I'm using Hooker harnesses that have steel bushings in the mounting ends, I had to modify the stock anchors by double-bending them a bit. This meant that there was not enough clearance from the aft side cabin covers, so I had to cut bigger slots in the cabin covers.

Every action has an equal and opposite reaction. If you try to build stuff fancy-like, you pay for it in lots of additional on-the-spot engineerin' and cipherin'. I think Pogo said that.


 
May 22, 2007     Floorboards; Cabin side covers       Category: Fuselage
Finished drilling the right F-876 aft cabin side cover. Installed platenuts in the cockpit sides and the right-aft floorboard.

Marked, trimmed, fit, and drilled the left F-876 as above. Installed platenuts in the cockpit sides and the left-aft floorboard.

Primed both aft cabin side covers.

Drilled and clecoed the rear seat mounting hinges on the floorboards. (Note: Drawing 29 shows the left floor-mounted hinge with the eyes at the end of the hinge segment, and the right one with the eyes opposite. Unfortunately, Drawing 32 shows both hinges on the seat having their eyes at the ends. Try assembling that...!)


 
May 21, 2007     Flap actuator arm; Floorboards; Controls - (3.0 hours)       Category: Fuselage
Drilled F-837 hanger and F-838 spacers and attached them to the floor. The control column is nice and smooth.

Trimmed forward floorboards to fit around the control hanger.

Bolted flap actuator arm and attach blocks to the the floor. The actuator was a bit stiff at first, but after I shot a tad of silicone lube in there, it loosened up a bit.

Trimmed the aft floorboards to fit around the flap mounting blocks, and checked to make sure they can be installed and removed easily with the flap mechanism still in place (after all, that's the whole point of having removable floorboards, right?)

Installed almost all the remaining floor nutplates. (To be precise, I installed the ones in the the F-805B L/R and their spacers.) I had to file the sides of a couple of the nutplates to fit. Not sure why that worked out that way.

Marked, trimmed, and began drilling the right F-876 Aft Cabin Side Cover.

Test-ran the flap motor using a 9V battery. Cool! Moving parts!


 
May 16, 2007     Floorboards - (2.5 hours)       Category: Fuselage
Today I sat back and took stock of a few things. I wanted to reassure myself that I'm on the right track with a couple of issues -- namely, how the nylon flap actuator blocks, floorboards, and cockpit side panels will be installed. Since I want to be able to pull the floorboards out of the plane easily at any time, without removing the control column, flap actuator arm, or anything else, I have to modify a few things.

I ended up cutting out two rectangular notches from each of the forward floorboard segments. One is for the end of the control column hanger, and the other (the one at the corner) will allow the floorboard to slide into place without having to be bent too much. I'll also have to cut out a small part of the aft floorboards, around the aforementioned flap actuator mount.

Installed most of the remainder of the floor nutplates, including a few tough ones. I used a couple of Cherry Max "platenute rivets." I also installed the two right-side flap-block nutplates (the ones that will take the AN-3 bolts). After looking at it for a while, I've decided to simply bolt the left-side blocks to the floor supports, and not use nutplates. My Reasons -- a). Simplicity, and b). I goofed up the placement of the left nutplates. Optimistically, I then decided to re-drill them in a different location. The second pair of holes were too close to the skin. I tried filing off some of the nutplates to make it work, but I wasn't happy with the results. So, no nutplates for that side.

I wanted to drill the control column hanger and spacers today, but I didn't have a long #11 drill bit that would fit alongside the front seat belt attach points. I tried every combination of tools that I had, but I ended up just ordering a 6-inch long #12 bit from Avery.


 
May 15, 2007     Flight controls - (2.2 hours)       Category: Fuselage
Today was one of those days when you just have to sigh. I got involved in the process of building, and forgot to think. The result was that I ended up fabricating a beautiful F-849 Forward Control Column Hanger, only to find that one was already built and installed in the fuselage -- one of the benefits of the Quickbuild kit. It was hidden in front of the spar, and I just didn't see it. So I wasted an hour and a half building a part that I'll have to donate to needy children (or maybe a needy RV-8 builder somewhere.)

After recovering from that embarrassment, I installed the WD-807 control column into the fuselage, and clamped the F-837 rear hanger into place. I decided not to drill it yet -- I need to figure out if I will drill it through the underlying floorboards, or trim the floorboards around the fixture so I can remove them easily later, just like I'm going to do with the flap mounting blocks.

Installed a Cherry Max "platenut" rivet in a hard-to-reach nutplate along the edge of the floor.


 
May 11, 2007     Rear control column hanger and spacers - (1.6 hours)       Category: Fuselage
Finished fabricating the F-837 rear control column hanger and the F-838 spacers. I spent a lot of time filing, grinding with the Dremel tool, hand-sanding, and polishing the hanger angle. It is without doubt the finest piece of work I've done so far on this airplane. Now I'll prime it, paint it, and bolt it in place under the floor, where no one will ever see it. Oh well...

I also test-fit the WD-807 control column to the fuselage. This is the "Tetris" of RV building, because it only goes in one way. It took a few minutes of twisting, turning and head-scratching to get the thing to fit through the hole in the spar.


 
May 10, 2007     Rear control hanger and spacers; Floorboards - (1.1 hours)       Category: Fuselage
Began fabricating the F-837 rear control column hanger amd F-838 spacers. After cutting the large aluminum angle and making the big diagonal cuts in the F-837, I had to stop because the 6" sanding disc on my disc sander has worn down to the point of being ineffective, and I didn't have a backup supply of discs. A quick trip to Lowes fixed that.

Cut the F-838 spacers from 3/4 x 3/4 square aluminum tube. They'll be sanded to final length tomorrow.

I also marked the rear corners of the rear floorboards with the footprint of the flap actuator mounting blocks. This floorboard material will be removed, so the blocks will rest directly on the underlying structure. This will allow the floorboards to be removed without removing the flap mechanism first. Seems logical to me, and several other people on the VAF website have done it already.


 
May 09, 2007     Gear tower access covers; Flap actuator blocks - (3.0 hours)       Category: Fuselage
Completed fabricating and installing left gear tower access cover.

Drilled Nylon blocks for flap actuator bar. Drilled blocks to floor.


 
May 08, 2007     Gear tower access cover - (1.9 hours)       Category: Fuselage
Drilled, countersunk, and deburred all holes, then primed right gear tower and installed nutplates in it. Dimpled appropriate holes in right access cover, and installed cover.

Deburred all holes in left gear tower access cover in preparation for installing nutplates.


 
May 05, 2007     Floorboard nutplates and gear towers - (2.0 hours)       Category: Fuselage
I installed about 30 more nutplates in the floor supports. All the ones in the "interior" of the floor are now done, and I got a good start on the ones along the edges. The edges are a lot harder to do, because of the lack of access, but I found that my pneumatic squeezer works pretty well there. I also had a chance to finally use that odd-shaped bucking bar I've had for so long now (Photo 1).

I also drilled out all the screw holes in the gear tower covers to #19 in preparation for installing nutplates.

It seems like I used half of my entire tool inventory installing the nutplates (Photo 2).


 
May 04, 2007     Floorboard nutplates and gear towers - (2.8 hours)       Category: Fuselage
This evening I finished the access hole in the left gear tower by filing/sanding it to size. Next up will be drilling the holes out to full size for the screws, and installing the nutplates. (Tomorrow, maybe.)

Speaking of nutplates, I installed about 40 of them in the floor support angles. Only about 75 to go! There were several places where I used one-lug nuts because of the underlying structure, and a couple of other places where I'm still scratching my head about how I'll make it all work, but overall, I'm pleased with this whole floorboard project. I figure it'll take me about 30-35 hours of total effort to split the floorboards into multiple pieces and attach them entirely with screws and nutplates. Not a bad tradeoff for the great utility I'll get out of it.


 
May 03, 2007     Floorboard nutplates and gear towers - (3.0 hours)       Category: Fuselage
This evening, I flipped the fuselage over on its left side and drilled the mounting holes for the left gear tower access cover. I then cut the remaining access hole.

Then, I drilled all the remaining #8 mounting holes for the floorboards, removed everything, and drilled 98% of the holes for the platenuts (there are 106 of them, so I drilled 318 holes!). Drilled for one-lug platenuts in several locations. I'm not exactly sure how I'll mount the platenuts along the intersection the rear floorboards and the rear baggage compartment floor.

Finally, I removed the three main pieces of the baggage compartment. I'm not sure if I'll be installing the floor again, or if I'll be modifying it and the underlying structure to fit the smoke system pump and reservoir. We'll see.


 
May 02, 2007     Gear tower covers - (3.6 hours)       Category: Fuselage
I decided to tackle the gear tower covers this evening. This is a modification I've seen on several RV-8s, and everyone I've talked to says it's a good one. It removes the material between the two lower lightening holes in each gear tower, and replaces them with a pair of covers fastened with screws and platenuts.

I cut out two 11-3/16" x 4-1/2" covers from a sheet of spare 0.040 aluminum using my new pneumatic shears (see previous "Tools" entry). I then rounded the ends to match the radius of the lightening holes, marked the covers for the location of the 20 screws, drilled #40 holes in them, positioned and taped one of the covers to the right gear tower, drilled matching holes in the gear tower, then removed the cover and cut out the access hole.

I'll do the left one when I get a chance to flip the fuselage over on its left side in the rotisserie.


 
May 01, 2007     Floorboards; Gear tower access covers - (4.5 hours)       Category: Fuselage
Deburred, cleaned, dimpled, primed and riveted F-830C stiffeners to bottom of "foreward aft" floorboards.

Installed and began drilling in the floorboards. Planned locations for #8 platenuts and marked floors appropriately. The screws along the edges will be non-countersinked. Only the ones that will be subject to foot traffic will be countersunk. I'm really happy with the floorboard split. It looks great and sits perfectly flush. I'm really glad I did this!

Drilled out the temporary pop-rivets that were holding the baggage compartment floor in.

Began cutting the access holes in the gear towers. (My plan is to connect the bottom pre-existing two holes and cover the larger holes with 0.040 aluminum access covers, using 20 screws and platenuts for each.)

Yesterday, I received an order of assorted AN hardware from Aircraft Spruce to add to my supply. (You can't have too much AN hardware!) Today, I organized most of it into plastic hardware drawers, and made new labels for the drawers.


 
Apr 29, 2007     Floorboards and stuff - (1.2 hours)       Category: Fuselage
Today was sort of a frustrating day. I returned to work on the rear seat attach hinges in earnest, only to have my progress thwarted by an apparent error on the drawings. Dwg 32 shows the hinges on the bottom of the rear seat-back. These attach the seat-back to the floor. The drawing shows the hinge eyes at the outboard ends of the hinges. Dwg 29, meanwhile, shows the other half of the hinges, the halves mounted to the floor. On this drawing, the left hinge segment is clearly drawn with the hinge eyes also at the outboard ends of the hinges. This clearly won't work, as the hinge eyes will line up and prevent the seat from being mounted. I decided to lay the hinges aside and call Van's tomorrow for verification before I drill any holes.

Next, I picked up the F-810A Aft Bulkhead and took some measurements. It's exactly 7/16" too narrow, leaving a nearly quarter-inch gap from the fuselage skin on either side. A couple of days ago, I called Van's and told them about the fit of the part, and was essentially told: "That's impossible -- these are CNC-cut parts. And besides, we've never heard of this before." (Several other builders I've talked to have also notified Van's of identical problems with the F-810A, so the denial was kind of odd.)

I narrowed my options to three. I'll either a). split the bulkhead in two (vertically), then spread the two pieces apart slightly and rivet on a connector, b). cut off some of the flanges and fabricate new ones, bent to match the existing skin curve, or c). fabricate a completely new aft bulkhead from scratch. I'm leaning toward the latter option.

Finally, I decided to do something productive. I installed three nutplates in each of the aft rear floorboard connectors. I also drilled and clecoed the stiffeners in the "forward aft" floor skins. The manual says not to install these stiffeners yet, but that's because they're assuming each floorboard will be in one piece. Since my smaller floorboards can easily be installed without bending them at all, the stiffeners are going on


 
Apr 27, 2007     Floorboards - (2.3 hours)       Category: Fuselage
Sanded, cleaned, dimpled and primed aft floorboards.

Sanded, cleaned, dimpled, primed and riveted most of the stiffeners to the F-830 and F-831 floorboards.

Riveted connector plates to the aft floorboards.

Marked aft floorboards for attaching hinge segments.


 
Apr 26, 2007     Floorboards - (2.5 hours)       Category: Fuselage
After studying the floorboard drawings for a while, I noted that Drawing 29 shows pre-punched holes along the right edge of the F-830 floorboard that will fasten it to the underlying support angle. In reality, these holes are pre-punched in the left edge of the adjacent F-831 skin. It's not a big deal -- I'll just lay the F-831 over the F-830 to drill the holes, instead of the other way around. I can't tell from the drawings which skin will actually go over the other. I'll have to research that a bit.

Drilled the connectors for the fore/aft skins, and drilled the six holes for the nutplates that will actually connect the fore and aft skins in the rear cockpit. Due to a layout mistake last night that I didn't catch this evening, I initially drilled one of the skins in the wrong place. I'm not sure this mistake will even show, but even if it does, it'll be an easy one to cover up because I think it'll be under the rear stick boot.

Spent some time trimming and fitting the floorboard skins into the fuselage. There are several places where I had to trim small notches or remove some material, but after a while, I got the skins to just slip right in and lay down perfectly flat. Most gratifying, though, was the way the screw holes in the skin connectors lined up perfectly. I am really glad I decided to split the skins! The floor is going to be a piece of cake to take in and out of the airplane, if/when I need to.

Fabricated the rear seat mounting hinges and began locating them on the floor. Almost got tripped up by another error on the drawings: Drawing 29 is missing a pre-punched hole on the F-831 floorboard, which initially caused me to mis-mark the mounting holes for the right hinge segment. I caught it before drilling any holes.

Marked floorboards for rivets.

Clecoed the stiffeners to the rear floorboards.

Photo 1: The connector plate I made to connect the fore and aft floorboards in the rear seat.
Photo 2: You've got to file and sand off quite a bit of material so the harness attach point will fit through.
Photo 3: The floorboards and foot wells, fitted to the fuselage for the first time. (Nice alliteration, huh?)


 
Apr 25, 2007     Floorboards and foot wells - (3.4 hours)       Category: Fuselage
Drilled, deburred, sanded, dimpled, cleaned, primed and riveted R foot well.

Split F-830 and F-831 floorboards into two pieces each. Filed and polished edges. Began fabricating doublers (7-3/4" x 1") which will join each half together.

Laid out F-830 B/D/E/F stiffeners on the bottom sides of the floorboards.


 
Apr 24, 2007     Floorboards and foot wells - (4.5 hours)       Category: Fuselage
Riveted F-805C angle to front seat floor.

Fabricated rear seat L footwell assembly. Filed, polished, sanded, cleaned, dimpled, primed and riveted all parts together, then clecoed assembly to floorboard.

Test-fit floor and L footwell in fuselage. Noted locations for nutplates (34 of them) that will attach the footwells and front seat floorboard to the fuselage. Filed and trimmed L footwell and floorboard for a perfect fit. Will do some research on which type of screws I'll use to secure the floorboards.

Fabricated rear seat R footwell assembly. Clecoed all parts together.

Marked gear tower sides in preparation for cutting out access hole. (The hole will connect the two lower lightening/access holes. It will be covered by a single access cover fabricated from 0.043 aluminum fastened with approximately 20 screws and nutplates.) Took measurements for fabricating the cover plate.


 
Apr 20, 2007     Floorboards       Category: Fuselage
Prepped and riveted the F-830B(PP) stiffener to F-829 Front Seat Floor.

Fabricated, prepped and riveted the F-832E Seat Back Hinge to the floor skin.

I recommend that anytime you're riveting hinge material, you lower the pressure on your rivet gun to the minimum practical--say 30 PSI or so--and use a 2X gun instead of a 3X or larger gun. I seem to re-learn this lesson every time I deal with hinges. The hinges are very soft aluminum, and it's easy to over-drive the rivets and cause ripples in the hinge. I over-drove mine, and the seat-back hinge came out slightly wavy -- not enough to cause problems with inserting the hinge pin, but just enough to annoy me.


 
Apr 19, 2007     Floor supports - (2.0 hours)       Category: Fuselage
Fluted and filed the aft, F-810A bulkhead to try to get it to fit. (I plan to either make a new bulkhead, or send this one back to Vans and get a replacement part. As I mentioned back in December, this bulkhead is grossly undersized on the sides. There's at least a 1/4" gap between the bulkhead and skin on each side.)

Fabricated F-805C and F-805F floor support pieces.

Installed a #8 platenut in each of the already-existing F-805D tabs.

Taped the F-805F shims in place on top of the F-805Bs.


 
Dec 07, 2006     QB Quality Control inspection - (1.0 hour)       Category: Fuselage
I spent some time going over the fuselage in detail, now that I have it mounted in its rotating stand (see previous entry). I noted several places where the quality of the QB construction is not exactly up to my standards. None of these discrepancies is serious enough to have to re-do, but they're slightly surprising, considering the overall quality of Van's kits and reputation.

The first photo shows one of about six locations in the belly where rivet edge distance has not been merely pushed, but murdered. It's not worth it to me to drill out the offending bulkheads, match-drill new holes, dimple the skins, and install new rivets. They're not structural, and the judges will certainly never see these rivets, so I suppose I could still be a contender at Oshkosh ;-)

The second photo shows some rather severe gouge marks in the bottom of a gear tower weldment, left by God-knows-what kind of tool or process in the Philippines. I can fix this pretty easily, but it's an annoyance that I shouldn't have to deal with.

Third photo: On the advice of an award-winning RV-8 builder buddy of mine, I dug out the F-810A upper bulkhead and put it in place in the tailcone. Holy cow. It fits like a square peg in a triangular hole. The distance between the bulkhead and the skin (right side is shown in photo 3) is about 1/4" on each side! That bulkhead is going to require some serious re-work. (It's obviously a bulkhead issue because the skin curve is flawless...)

My general opinion of the Quickbuild kit is this: It is still VERY worth the approximately $8,000 surcharge (especially if time is money) but don't expect utter perfection. There will still be workmanship issues and imperfections that you'll have to deal with. Perhaps that's all part of "Van's Master Plan to Make You a Better Builder."

And that's OK with me.


 
Dec 07, 2006     Fuselage stand - (.4 hour)       Category: Fuselage
Installed a 5/16" hitch pin (from Lowe's) in the fuselage stand and drilled the holes that will allow the fuselage to be locked into several positions (upright, laying on either side, or inverted.) Working inside the fuselage will be a pleasure with it rotated like this.

For those of you interested in this awesome rotating stand, I'll re-post the manufacturer's information: Jeff Bordelon (http://www.jeffsrv-7a.com/FuselageStandsForSale.htm). Give it a look. Jeff's a great guy, and his products are top-notch! [Addendum: Jeff has since stopped manufacturing and selling these stands.]


 
Nov 29, 2006     Fuselage stand - (.4 hour)       Category: Fuselage
Completed assembly of fuselage stand, with the help of a friend. The fuselage is now mounted and awaiting the purchase of a short hitch pin to lock the rotator arm.


 
Nov 27, 2006     Fuselage stand - (.7 hour)       Category: Fuselage
Nearly completed assembly of my Jeff Bordelon fuselage rotisserie -- which is a nicely-engineered product. I had to file the holes on the aluminum firewall angles slightly oblong, and also the center hole through the front mount arm, in order for the bolts to fit.

All that remains is to lift the fuselage up, swing the front stand upright, level the back end, clamp and drill rear attach fitting, insert rear bolt, then drill various rotation-lock holes in the front mounting arm. I also need to buy an eye pin as specified in the instructions. I'll have to enlist the air of three friends to help me lift and mount the fuselage.


 
Nov 26, 2006     Fuselage stand - (.4 hour)       Category: Fuselage
Began assembling rotating fuselage stand. Drilled holes in rear bulkhead and bolted fitting to it. Hand-tightened angle brackets to firewall.


 


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