Monthly Archives: August 2021

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Transparencies and Misc

The templates for masking the window transparencies have finally arrived.  The Avery Dennision BriteLine+ vinyl sheets were custom cut by Moody Aerographics specifically for this purpose.  I originally intended to mask off each window with just one vinyl piece, but matching the template profile on the curved surfaces with the exposed sticky adhesive proved too difficult for an amateur installer.  Instead I chose just to use the corners which lay flat, with electrical tape filling in the straight or slightly curves intermediate sections.

The left photo shows the raw templates on the main roll.  Before applying to the windows, an outline of each corner was traced on acetyl sheets.  The reason for retaining this contour will be shown later…

 

 

 

The left lower windscreen corner was raw fit with epoxy resin and SuperFil before priming.  The corner template mask was laid into the corner with about 1/8″ – 1/4″ offset from the underlaying canopy frame.  This offset will present a clean edge visible from within the cockpit.

 

 

The smoothly cut template mask was covered with two layers of electrical tape.  Each tape layer provided an additional 0.0063″ height for when the AlumiLite black dyed and glass bead infused West Marine two part epoxy resin was applied to the edge gap.  The resin will then be sanded carefully from layer to layer to reach the final height of the template mask.

 

 

TAPING DETAILS

The same general taping process was then applied to doors and windows.  The raw template mask in the corner was connected to other corners with red electrical tape.  The bright colors for the final tape layer were used to enhance visibility while sanding.  Notice the curved black electrical tape second layer.  This shape was rough cut using the acetyl sheet contour described above. Cutting the electrical tape in this manner helps it stay flat, as compared with trying to bend the tape around a tight corner.

 

Additional black electrical tape was applied above the straight sections, followed by general masking and one more layer of vinyl tape roughly laid around the perimeter.

 

 

 

These photos show the before and after initial application of the dyed resin for the front left door.

 

 

 

These photos show the rear left window progressing from taped outline, dyed resin applied, initial rough sanding, and final edge sanding.

 

 

 

The last sanding step levels the lowest tape layer with the resin material.  Since this is only about .006″ thick, the care needed to not rub through to the Plexiglass window is extreme. It took quite some time to achieve this on the windscreen, doors and windows. The sanding outcome so far looks good, but application of the primer and paint will show whether the preparations were sufficient.

 

 

OIL DOOR LATCH BUTTONS

The issue of the push buttons for the oil door has finally been addressed.  A #30 hole was drilled into the Camlock latch plate, then taped for a #6 screw.  A mock-up of the final buttons (yet to be fabricated) are represented by the washers on the right.

 

 

The Delta drill press and a V-block were used to drill a 1/2″ steel bar with a center hole.  That hole was then taped for a #6 screw.  The taped post held a piece of 1/8″ aluminum flat bar for shaping.

 

 

The blank was hand filed and then sanded to exactly fit into each latch hole. The sides were slightly rounded to self-center the button when the latch springs back to the closed position.  The final buttons were polished with 2000 grit sandpaper and fastened with #6 stainless screws. They will probably will be left as-is and not be painted, but that decision will be made later.

 

 

MISCELLANEOUS

The original plans call for an AN3 bolt to hold the steps in their cradle.  I wanted a stronger connection, so the steps and the cradles were drilled and reemed to 1/4″ to hold thicker AN4 bolts. (NAS-

 

 

The door alarm reed switches were connected to the main electrical bundle via DSUB connectors.  They are held together with heat shrink, then laced into place.

 

 

 

The main wiring bundles on left and right sides under the rear seat panels were laced together.  In retrospect I would probably rearrange some of the wire runs for a cleaner look, but the final result is secure and will be serviceable as needed for future maintenance.

 

The control sticks were cut to length to provide the maximum height without touching the instrument panel or switches.

 

 

 

 

Interior (3)

Terminating the headphone and microphone jacks was the last set of main actions needed for the interior fuselage electrical system.  What remained were cable lacing and those connections left for when the engine is mounted.

The center console cover plate and rear face of the armrest are the locations for the jacks.

 

 

 

 

The mounting components for the front plate are shown on the left.  The rear face mock-up is on the right.

 

 

 

 

The inner side of each jack location contains a backer plate with holes for the soldered wires and auxiliary devices. On the front plate are spaces for the Bose LEMO jacks and an auxiliary audio input.  The rear face includes a USB power connector with two ports.

 

 

 

Here the front cover plate is shown under the control quadrant.  Note in this photo the hole for the auxiliary audio input has not yet been drilled.

 

 

 

 

The console parts were laid on their side to trim ins a straight line as shown on the right.  The interior tunnel wiring with fuel pump and transducer wiring is shown on the left.

 

 

 

Preparing the headliner material for covering the fiberglass template included steaming to remove wrinkles and cutting to approximate size.  The attempt to cover the fiberglass with material once spray adhesive applied was a total disaster (no photos shown due to the embarassment factor). Fortunately the fiberglass templates were recovered. The covering job will be left for professionals.

 

 

Final configuration of the push-pull cables for the fore heater box, rear heater box, and oil cooler valve were also completed on both the interior and exterior side.  These were McFarlane MCU224-xx slip resistant cables in all cases.

 

 

 

The main ground wire under the pilot seat was encased in 7/16″ fuel line to further protect against chaffing against bulkhead parts.  This was probable not necessary given the clearance, but extra precautions for this critical matter were taken.