Cabin Cover (4)

Attaching the center console brace and beginning to trim window panes was the order for the day.

imgp7261The center brace is clamped in the middle of the forward canopy cover, then match drilled with a #12 drill to accommodate an AN3 bolt.  This is tightened down to fasten the brace, so the the rest of the holes can be drilled.

 

 

 

imgp7263Here is how the top of the outer cabin cover looks after the fastener holes are completed.

 

 

 

 

Here are left/right pictures of the bottom portion of the center brace attached near the firewall.  Two AN3 bolt hole are drilled between an angle bulkhead and a reinforcing plate.

 

 

 

 

imgp7274A set of spacers 1-13/32″ long  are fabricated from 5/16″ diameter tube.  This will eventually be driven into enlarged holes for the center brace.  The cabin cover needs to come off for further processing, so this step will be saved for later.

 

 

 

imgp7265The plans call for fitting the windscreen first, but I wanted some experience dealing with Lexan/acrylic trimming beforehand.  The side windows will be my test platform – if things go south these will be cheaper and easier to replace compared to the windscreen.

 

 

 

imgp7275imgp7276Pull back the protective covering and get ready to power trim!

Cabin Cover (3)

Over the Thanksgiving week off the focus was finishing major elements of the cabin cover.

imgp7192The first step was complete match drilling the mid-skins to the cabin cover.

 

 

 

 

imgp7191imgp7194Next was clamp the rear door frames to the bulkheads and match drill for #10 countersunk screws.

 

 

 

imgp7200imgp7198Here the right side has been drilled and clecoed into place.

 

 

 

 

imgp7206Now for the forward door frames. The gusset  is clecoed to the bulkhead, but match drilling for the #10 screws to the fiberglass frame goes through about 1/4″ of empty space. According to the plans, this space will have structural filler applied.

 

 

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imgp7225Getting the fiberglass trimmed for the front deck took quite some time. (between initial Dremel tool sanding and hand filing).

 

 

 

imgp7211imgp7216Next was measure the door jam bottom, then drill #19 holes for #8 countersunk screws.

 

 

 

imgp7254imgp7257Check for size, then countersink with an angle tool.

 

 

 

 

imgp7258The final product looks pretty good.

 

 

 

 

imgp7221imgp7220Now rough fit the center console brace.  Overall starting to look like an airplane.

 

 

 

 

New Home (3)

Here is progress as of November 24 (Thanksgiving Day)

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New Home (2)

Here is the basement rough-in from November 18.

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New Home

The construction of airplane parts will be taking a back seat to new home construction.  One benefit of the new domicile will be a 25′ x 30′ heated/cooled basement workspace.  Excellent!

All the initial paperwork has been completed. Now the build is underway.  My direct involvement will not occur for another few months.

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Cabin Cover (2)

I had another forced pause from the shop due to business travel overseas.  This weekend was getting back in action with Eric’s help on further cutting, fitting and sanding the fiberglass cabin cover.

imgp7098The door bottom needs extensive trimming to get to the proper thickness.

 

 

 

 

imgp7099Left and right sides need to be notched to accommodate the bulkhead reinforcements at the bottom.  Notice the degree of relief needed to make this fit.

 

 

 

imgp7102The inner section must line up just right with the mid-skin longerons.  Too much taken off will decrease strength for the connecting rivets.  Too little and the fiberglass bottoms out on the longeron and fit will not be proper.

 

 

imgp7127First reduction was with a fiberglass cutting wheel on a Dremel tool, followed by a belt sander, hand file and finally Great Lakes 22″ sanding block with 120 grit paper.

 

 

 

imgp7105imgp7141Fit, trim and refit is the process here. Getting the cabin cover to slide in without too much material removed takes time and patience.  On the right photo the 3/4″ offset for windshield and doors are being highlighted with a Sharpie.

 

 

imgp7143imgp7145Trim the windshield flange…

 

 

 

 

imgp7151Clamp the rear door pillar and bottom flange in place.  Then start the match drilling of the cabin cover to the top tailcone skin.

 

 

 

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imgp7153Eric pushes up on the cabin cover fiberglass while I drill #30 holes down through the tailcone skin. This process will continue on around the whole baggage bulkhead area.

Wingtips / Lights (2)

Continuing with the wingtip preparations…

imgp7063This shows the #4 nutplates for the navigation and strobes being riveted into place. I  used stainless steel and countersunk Cherry nutplate rivets, which are expressly designed for the purpose.  A standard hand riveter can be used, no need for the specialized and expensive Cherry puller(s).

 

 

imgp7065A #4 screw fastens the bracket which will hold the nav/strobe housing.

 

 

 

 

imgp7068Here the nav/strobe housing is shown in final configuration.

 

 

 

 

imgp7081imgp7082Here are the nutplate insertions (outside and inside) for holding the lenses in place.  Next up is final AwlFair application, sanding and priming.

Cabin Cover (1)

The weather forecast called for beautiful skies and temperatures over the weekend, so I enlisted Eric’s assistance in starting to trim and fit the cabin cover to the fuselage. The idea is get everything aligned properly, then finish the interior metal painting.  This way scratches produced during the fitting process will be reduced.

imgp7040Faint scribe lines are on the fiberglass mold from the factory, but difficult to see under most conditions.  I added electrical tape along the edge for a better visual reference when rough cutting with a Dremel tool.

 

 

imgp7043imgp7047The process is easy, but takes time.  Rough cut near the scribe line, then hand sand until smooth.  Then fit on the plane and continue sanding until everything lines up perfectly.

 

 

imgp7051Here is a closer look at the rough out process.

 

 

 

 

imgp7052A long wooden dowel is attached to a 22″ Great Planes sanding block.  Eric guides the dowel along the opposite end while I smooth sand and get closer to the the scribe line.  The dowel extension will approximately make the surfaces parallel on both sides.

 

 

imgp7055imgp7057The first rough fit shows additional material needs to be removed. Sand and refit until alignment is correct.

 

Wingtips / Lights (1)

My first foray into fiberglass is modifying the wingtips to accept special inserts for the AeroLED VX landing lights and Pulsar PS position/strobe lights.

imgp6848imgp6852Measure twice…

 

 

 

 

imgp6854Cut once, twice, three times…

 

 

 

 

imgp6857imgp6856Inserts rough fit in the new openings.

 

 

 

 

imgp6863imgp6865Layout of West resin system components.

 

 

 

 

imgp6874imgp6885imgp6884Mix, and brush on both surfaces.

 

 

 

 

imgp6890imgp6894Position insert and cleco together.

 

 

 

 

imgp6897imgp6903Fill inside edge with remaining resin to ease the sharp angle (will help later when fiberglass cloth is applied). Let this combination dry overnight.

 

 

 

imgp6907Now add three layers of fiberglass cloth on the inside to reinforce the insert seams. Let this cure overnight.

 

 

 

 

imgp6910Fill in the outside gaps, let cure overnight, then sand roughly smooth.

 

 

 

 

imgp6912imgp6914Position template, drill adjustment holes and rough fit the taped landing light lens to the initial opening. Sand, sand and more sand until lens fits perfectly in the opening with sufficient clearance for later alignments with airplane axis.

 

 

 

imgp6915Rough fit is done, need some additional build-up in certain areas. This will be done later.

 

 

 

 

imgp6920imgp6934Place pivot point and drill fastening holes.

 

 

 

 

imgp6933imgp6937The internal section of the pivot is stuffed with a cotton plug. Use E6000 structural adhesive to hold the pivot point, plus add pop rivets for additional stability. The cotton keeps the adhesive from filling the pivot cavity.

 

 

 

imgp7027Build-up needed, as the dimensions of the fiberglass inserts obtained from AeroLED is very poor.  The left side is a good 1/4″ bigger top-bottom and 1/4″ left-right compared to the other side.

 

 

 

 

imgp6922imgp6927Measure the lexan lens for rough cutting. Use a dremel tool for approximate size, then hand sand to closer dimensions. Electrical tape is applied around the edges to prevent scratching during the fit process.

 

 

 

imgp7031The fit process took a long time with hand sanding.  The edges still protruded a bit from the wing surface.

 

 

 

 

imgp7033imgp7034AWLFAIR 8020 resin and AWLFAIR 7007 red hardener are 1:1 mixed together to create a creamy fairing compound. Tape covers the entire lens.

 

 

 

imgp7035Coat number one is applied to the fitted lens.

 

 

 

 

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imgp6930An additional job for the week is rounding over some cable fairings.  A dime was perfectly sized for measuring the distances.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Baggage Area (3)

After a week traveling overseas on business followed by a week at AirVenture 2016, I finally got back to the actual building process.  During the off period I had ordered #2 Tefzel wire for three battery cables running from behind the baggage area to the firewall.  Two were for hot leads for the dual battery, dual alternator configuration I am building and one for a solid ground lead.  My concern before final riveting the left seat and baggage floors was being unable to pull the heavy/stiff wire through the already installed black plastic conduit (see previous posts on these).  So after receiving the wire, a test pull was in order.

IMGP6838A cheap ($20) wire grip was purchased from Amazon for this test. Though inexpensive, this one has an end swivel to help guide the head assembly through the conduit.  This picture shows beginning to thread the wire mesh from the grip onto the #2 Tefzel wire. Eventually about 2″ overlap was achieved.

 

 

 

IMGP6840No pictures are available from the test pull, but the Tefzel went through the conduit with no problems. Now having peace of mind about cable runs, I proceeded to use a pneumatic puller to set the rear floor and baggage compartment. Here all the central pop rivets are in place.

 

 

 

IMGP6841This view show all the edge rivets and nut plates squeezed along the main tunnel.  The baggage frames and support angles are clecoed in place ready for Eric’s availability to drive while I buck. There some final adjustments to the baggage door itself I want to complete before final assembly of the frames.

 

 

 

IMGP6844The right side wire cover is also clecoed in place waiting for final installation.  Next up on the to-do list is deburr and prep the tunnel covers.