Cabin Doors (1)

While waiting for replacement parts for the flap control rods, I began working on the cabin doors over the holidays.  My intention is prep, align, fit, and sand as many of the door latch parts as possible before bonding the two shells together.  This should make the incorporation of a PlaneAround NEW180 cam door system much easier.  This approach does require a sequence deviation from the original Van’s plans.

First step is scribe lines on the inside of the window frames.  The 3/4″ line will eventually become the edge behind the plexiglass windows.  The other lines are for rough removal and setting temporary clecoes.  The right photo show a few clecoes already installed along the bottom edge.  I started here because the original witness holes are here and should provide excellent alignment between the shells.

 

Next is fasten upright on the workbench and clamp inside the window frames.  This should press the shells together and progressively flatten moving upwards for clecoe holes.  Drill, clecoe, reset clamps, repeat until the inner frame is solidly fastened together.

 

 

Clecoes are now installed at the windows.  The entire door frames is then rough fit to the fuselage via the outer witness holes.

 

 

 

Gaps to the fuselage are acceptable at this stage.  They should become tighter as the door edges are trimmed.

 

 

 

A 3/32″ hole finder is used to align open rivet locations in the fuselage with edges of the door shells. Holes are drilled, then clecoes inserted. Without the hole finder, this process would be nearly impossible to perform accurately via scribe lines!

 

 

The rough fit process is completed with good results.

 

 

 

 

LATCH MECHANISMS

Now the doors are clecoed together, work on the original Van’s latch mechanism can begin.

As usual, the parts are laid out before processing. Following the original plans, the C-RACK 10 was cut to Van’s specifications only to find the lengths need to be different for the PlaneAround kit.  Oh well, another opportunity to order replacement parts.

 

 

In the meantime, the latches are positioned in the middle of the corresponding door pocket both vertically and horizontally. Here are the final drill holes shown inside and out.

 

 

CAM GEARS / BACKERS

Having the door shells apart greatly facilitates working on the cam gear installation. One item of concern is the lack of reinforcement around the gear block.  Access to the inside surfaces allows for creating a custom solution.

 

 

 

This plate made from spare .040″ aluminum sheet is match drilled for the gear block, plus will have #6 nutplates installed for a vanity cover.  These alterations should provide increased strength together with the fiberglass reinforcement blocks from PlaneAround.

 

 

This backer is for the gas strut attachment at the door (a standard Van’s feature).

 

 

 

 

PIN BLOCKS

Now for custom fitting the Delrin pin blocks to the door frame. The white block from Van’s is shaped to fit exactly in the corresponding pocket, then used to match drill attachment holes through to the outside shell.  The black PlaneAround piece has an extended pin guide and will also be custom shaped for the pocket.  The existing holes will provide a template for the new pin blocks.

Empennage Attach (4)

The plans call for numerous parts requiring custom lengths or special fabrication.  I decided to process all the remaining control and push rods together.  This should reduce the alodine batches required, plus get some minor shop efficiency by not changing tools for every single piece.

Here are some follow-up pictures from the last post about how the larger diameter (>1″) aluminum tubes are measured and drilled.

 

 

 

The smaller flap actuator rods (1/2″ diameter) made of steel are much more difficult to handle, as the tolerance and angles are tighter.  Here a dremel tool with small grinder wheel is used to open up the end large enough to accept the screwed fitting.

 

 

Next comes the measure and alignment of the holes.  For these rods, two through holes perpendicular to one another and offset back 1/2 and 3/4 from the edge are required.  Unfortunately, the drilling on one rod end was not correct the first time. This resulted in a hole not aligned properly through the center of the rod.  It was bad enough I will have to make these over again.  Stay tuned for an update.

Empennage Attach (3)

Fabrication of elevator trim components and push rods was the order for this week. The trim motor housing was completed to the point of final riveting.  At this point the alodine/prime sequence will be used to treat the parts before assembly.

The distance between the attach brackets for the trim bellcrank must be measured carefully to ensure parallelism for the faces, properly aligning the pivot bolt with the trim motor.  Here an analog caliper is used to check the distance from the front edge to the back edge.  After a number of adjustments, I was able to get the faces within .005″ of parallel.

 

 

The elevator pushrod is made from a 73″ piece of AT6-035 x 1.5″ aluminum tubing and an appropriately sized threaded insert.  Here the circumference of the tube is measured for accurately drilling six evenly spaced #30 holes. After alodine/prime these parts will be connected with long shanked pop rivets.

 

 

 

A spring-loaded center punch is used to mark the six rivet holes 1/4″ from the edge of the tube.  After processing on the drill press, the clecoed parts are checked for correct alignment.

 

 

 

Also during the week I finished the end cap for the rudder bottom.  Looks nice.

Empennage Attach (2)

Use of paint booth and fabricate custom parts for empennage attach.

Over the last few months, Tal and I have been constructing a paint booth in his workshop.  This was our first run of priming parts in the just finished facility. Here he prepares to apply PPG DP40LF primer to the internal side of his canopy/overhead console, plus my horizontal and vertical stabilizer fiberglass tips.

 

 

 

My tips had to be sanded heavily to get the properly rounded outside profiles to match the elevator tips.  My experience is the fiberglass parts from Van’s are just rough approximations – to get this right requires plenty  of work.  Witness the sanding completely through the gel coat on the left part, this required additional fiberglass/resin layers on the inside to prevent holes.

 

 

Next up is prepare and fabricate additional parts on the empennage attach sequence.  The left photo shows a supplimental cover on the rudder bottom.  Not necessary, but it should help deflect some water from entering.  The right photos shows HS attach shims being made.

 

 

 

Attach points for the elevator trim motor and cables are being prepared on the left.  A 3/8″ spotting drill in a clamped vice ensures the attach rivet and bolt holes for the AN6 pivot bolts are correctly aligned to hold the trim bellcrank.

 

 

Empennage Attach (1)

While the horizontal stabilizer is in the jig for work on the fairings, there are also elements of control surface configuration which can be performed.  Checks on elevator up +30 degrees and down -25 degrees confirmed proper range of motion.  Then both sides are set to the “trail” position for drilling the elevator center bearing and elevator push rod bolt holes. To accomplish these tasks two drill guides were fabricated.

The first drill guide protects the center bearing while the pivot points in the elevator horns are configured.  The outer diameter of the guide needs to be reduced just small enough for a snug fit in the inner bearing.  The Delta drill press and Pferd files did the trick.  Once again I am amazed and happy at the incredibly small runout on the drill press!

 

 

The left photo shows the drill guide inserted into the center bearing for drilling the right elevator horn.  Next comes the actual drilling operation.  The right elevator is then removed and the same process used on the left elevator. The guide aligned everything perfectly and an AN4 bolt fits cleanly between both elevator horns.

 

 

To facilitate proper alignment of the push rod holes, a drill guide is made from a piece of oak sanded to the exact thickness spanning between the elevator horns. Caliper readings were used for initial hand sanding.  Then the piece is aligned and drilled perpendicular to the surfaces with the drill press.

 

 

Here the oak drill guide is clamped into place prior to drilling the second hole.  A piece of 3/16″ stainless rod is inserted to align the first hole for the right elevator with the undrilled face of the left elevator.  After drilling is completed, an AN3 bolt passes cleaning through both horns with perfect alignment.

 

 

 

This week was also some final sanding and fitting of the HS tips. The desired 1/8″ gap between the tips and the elevator fairings look good.

 

Empennage Fairings (6)

The tedious work of sanding, fitting, aligning, and build-up continue on the fiberglass tips for the elevator and horizontal stabilizer.  The nice part about fiberglass is you can add or subtract material as desired.  The down side is having to wait at least 24 hours between operations.

Here is a case of trying to level the HS tips, then fill as needed with resin/glass beads (white) or Awl Grip fairing compound (pink).  The same operations apply to the elevatore tips.  Sand, fit, fill, rinse, repeat…

 

 

 

The left shows backing washers clecoed for superglue attachment to the elevator tips. These are not required, as these holes are supposed to be countersunk, then pop riveted onto the elevator.  However, experience has shown the fiberglass gets very thin after the countersink operation, so this attempt should reinforce the connection.

 

 

… and while waiting for the next round 0f build-up to cure, I started adding the nutplates to the horizontal stabilizer.  Eventually these will fasten a custom fairing which sits between the horizontal and vertical stabilizers.

Empennage Fairings (5)

Work on the vertical stabilizer and rudder fairings was recently completed – at least for the time being and until final preparations for paint are underway.

My overall satisfaction level is good with the overall fit, gaps and blending of skins to fairings.

 

 

 

 

The upper and lower elements are clecoed in position to check the final rudder angles, gap tolerance on the upper rudder swing and rudder/vs skin clearance.  All within tolerance and acceptable for now.

 

 

 

The next fairings to be addressed are on the horizontal stabilizer.  To properly fit these, Section 11 Tailcone Attach elements must first be completed.  The elevators are fastened to the rod end bearings of the HS, then angles and clearances checked for free movement.

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Here the HS cradles in the jig built many moons ago with the original construction.  The elevators are in position to begin work on the fairing alignment.

 

 

 

Close-ups of the gap between elevator tips and horizontal stabilizer, then the rod end bearding and the hinges.

 

 

 

 

Initial fiberglass filling of the HS end caps after rough trimming to shape with the elevator tips.  These are not straight – bending backwards at an 8degree angle. This is enough to  prevent the fiberglass molding from being simple.

 

Empennage Fairings (4)

More sanding, fitting and filler on the fiberglass parts. Plus the addition of nut plates at various locations to complete some of the parts.

This photo shows the lower rudder fairing with #6 nut plates soft riveted into place. I made this fairing removable, as the AeroLED Suntail nav/strobe light wiring and electonics still needs to be added. A machined spacer from Cleaveland Tools provides a stable surface for fastening the Suntail afterwards.

 

 

 

Final filler and smoothing on the bottom rudder skins.  These parts hold the bottom fairing.

 

 

 

 

Nut plates for #6 screws are also install on the vertical stabilizer top.  These will allow removal of the top to access the VOR bracket made earlier.

 

 

 

The bottom of the vertical stabilizer skins also takes #6 nut plates.  These holes will later be used to fasten the fairing which bridges  between the vertical and horizontal stabilizers.

 

 

 

Empennage Fairings (3)

This week was about sanding and fitting the rudder top and bottom fairings.

This shows the top fairing pop-riveted into position on the rudder.  The end cap with the lead counter-weight needed some additional material to match well with the VS top.

 

 

 

 

Plastic electrical tape is applied to keep the resin off unwanted parts.  Then the end cap is sanded and cleaned for fiberglass layers.  These are probably not necessary, but I wanted to ensure the overlapping metal parts are held rigidly in place (should help prevent cracking along the seam)

 

 

 

Multiple layers of fiberglass and resin are applied. Because the resin is quite fluid at the start, some droops down the lower face.  This will later be sanded smooth and covered with Awl Grip D8200 for the final finish.

 

 

 

The basement shop was also enhanced with a new single stage, 12.8cfm air compressor made in USA by Quincy. Next steps are get the electrician to wire a dedicated circuit, then fire up for plane building usage.

Empennage Fairings (2)

Further fitting the VS top and rudder bottom fairing were the activity for this week.

 

The VS top fairing did not fit properly in the metal opening.  Throughout this build I have found all the fiberglass parts to only be approximations, much work on proper alignment and sizing has been needed.   Here the rear profile is being sanded to shape and the back panel straightened to match the rudder top fairing.

 

 

The AeroLED Suntail NAV/strobe will be attached to the lower rudder fairing via a machined aluminum spacer purchased from Cleaveland Tool.  The fiberglass from the fairing at this point is fairly thin, so fabricating a backing plate for the six pull rivets was chosen. This photo shows interim progress.