Sam Buchanan's RV6

The "Finish" Kit

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Panel Page

Firewall Forward

Interior Installation


11/28/98; installed brakes and wheelpant mounting plates.


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Here is the completed (less brake line) brake installation. I added a washer to each spacer so there would be more clearance between the mounting plate and the brake rotor.

There are several ways to install stuff backwards and upside down (don't ask....suffice it to say that the second brake took one-fourth the time to install...).

You will need to move one of the bleeder valves to the "top" of the caliper. Yes, the wheelpant mounting plate points "forward" (caliper is aft of the axle). Also note the jack point. It is simply a piece of angle and a 1.25" hardware store U-bolt.

11/29/98; 1.5 hrs; installed brake fittings; installed fittings in fuel valve.

12/11/98; 2.0 hrs; installed fuel and vent lines.

12/12/98; 1.5 hrs; prepared canopy for fabrication of fiberglass fairing.

12/14/98; .5 hrs; applied fillet of Super Fil to front of canopy.


finish33.jpg (32066 bytes)Super Fil is a PolyFiber product. It is a sandable, very lightweight filler with an epoxy base. It mixes to create a paste that can be buttered into place without running. Setup time is about twelve hours at 77 degrees. I am using it to form a fillet between the canopy and skin. Fiberglass tape and resin will be applied over the fillet. Electrical tape was applied to define the edge of the fiberglass fairing and protect the canopy from sanding damage.


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12/21/98; 1.25 hrs; sanded Super Fil and made fiberglass lay-ups on canopy leading edge.





12/23/98; 2.0 hrs; sanded fiberglass; remasked; applied Super Fil.


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I sanded the edges of the fiberglass lay-up down to the black tape. The black tape was removed and reapplied 0.25" outside of the original position. This allowed room to feather the edges of the fiberglass.




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Here is the squeegee that will be used for the top coat of Super Fil.







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You can see how the squeegee can be forced to follow the contours of the fairing. I applied Super Fil and pulled it down level to the electrical tape masking...




finish41.jpg (25311 bytes) this. All that remains is sanding, filling minor imperfections, resanding, and finishing up with glazing putty. The whole works will be sanded down to the black tape which will result in a nearly flush finished edge.



12/24/98; 1.5 hrs; sanded Super Fil down to black tape and applied another skim coat.

12/26/98; 3.5 hrs; sanded filler on canopy; remade forward fuse skin (I didn't like the way the first one fit around the canopy).


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The almost finished results. There are still a couple of minor low spots to fill, but this will do it until paint time. The edges were feathered into the canopy deck, and the edge on the canopy is only the thickness of one layer of electrical tape; The overall effect is of flush edges.



1/1/99; 0.5 hrs; used clamps and heat gun to reform cowl.


finish49.jpg (25999 bytes)The cowl surface in the spinner area was really warped. I clamped the surfaces to allow for some springback and heated them with a heat gun. After cooling, the clamps were removed and the surfaces aligned much better. There are still serious problems to address at the outside corners of the front of the cowl.



1/6/99; 1.75 hrs; riveted canopy rain seal flange to forward bulkhead; made cutouts for instruments to protrude through forward bulkhead.

1/7/99; 3.0 hrs; trimmed cowl to improve fit; made Lexan inspection covers; modified fuel valve mounting bracket.


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The outside corners of the cowl had serious misfit problems. On one side, the gap between halves was over 1/2". I decided to make parallel 1/4" trims on both sides of the cowl. This went a long way toward getting the cowl to fit properly. It now matches well enough to begin fitting to the fuse.






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For a change of pace, I fabricated a  Lexan window for the wing inspection cover that fits over the Navaid installation. This will allow preflight inspection of the linkage.

A Lexan inspection cover was also made for the elevator pushrod access cover at the aft end of the fuse.



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Highly recommended modification:

The flanges were removed near the center of the seat pans so the fuel valve bracket can be mounted beneath the pans. This will allow the pans to be removed without disturbing the bracket or control console.

This mod requires the platenuts to be mounted on the bracket instead of the pans. I used AN423AD3-3 rivets to fill the rivet holes in the floor pans.




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1/8/99; 7.5 hrs; mounted top half of cowl; fabricated and riveted firewall hinges for bottom half of cowl.





1/12/99; 3.5 hrs; trimmed and fitted lower cowl half.


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The trimming instructions in the manual worked well. Fortunately I had enough cowl material at the split line to cut out the gross misalignment that cowl had as delivered. Duct tape and a packing strap served as third and fourth hands.



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Ah yes, another big hurdle jumped!

The fit of the cowl turned out better than expected.

I have no explanation....



1/16/99; 1.5 hrs; riveted hinges to upper and lower cowls

1/18/99; 1.0 hrs; riveted more hinges to lower cowl.


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Table of Contents

RV6 Home

Who is Sam? 
The Hangar 

Getting Ready to Build 
     Odd 'n Ends 

Building the Tail 
     Horz. Stab Log 
     Vert. Stab Log 
     Rudder Log 
     Elevator Log 

Building the Wings
     Wing Spars
     Wing Assembly
  Fuel Tanks

Building the Fuselage

The Finish Kit


  Flight of  Rediscovery 

  The Beat Goes On 

The RV Journal
Front Page 

Talk to Sam


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