Europa
N55XS
May, 2004

Europa A-055

May 1st

Checked cockpit module one final time and bonded it in place.  My wife was very helpful in this phase.  No way to do it alone.  Once in and riveted/screwed down, with weights holding the awkward parts down, we allowed the Araldite/flox fixture to set.  Once set, I opened the lower fuselage to get at the aileron bellcrank brackets.  Sanded well around the inside of the brackets and the outer skin of the fuselage.  Laid up three layers of BID and epoxy on three sides.  Will complete the forth side when the rivets, holding the cockpit module, firm, are drilled out.  Applied a mixture of epoxy and flox to the joint, where the rear cockpit module bulkhead meets the lower fuselage floor, then laid in two layers of BID and epoxy.  Installed pitch rod.

           
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Time: 4 hours
Total: 174 hours

May 2nd

Drilled out rivets and removed screws used to hold the cockpit module in place, when bonding.  Laid up BID on the forward edge of both wing spar entry holes, in fuselage.  My wife installed the pitch rod lower containment stop while I trimmed the trim tabs, which had been previously marked for rudder clearance.  Sanded and touched up the edges with micro and set aside to cure.  Performed mod 62 on tailplane torque tube.  A lot easier to do now, than when the top fuselage is bonded in place.

     
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Time: 3 hours
Total: 177 hours

May 3rd

Fabricated rudder pedal floor plates and fitted, temporarily into place.  Finished opening rudder pedal pass-through holes.  Sanded Tufnol bushings to proper fit on shafts and assembled rudder pedal assembly in place to check clearances and operation.  Can't fit them permanently until nose gear mount arrives.

        

     
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Time: 3 hours
Total: 180 hours

May 5th

New swaging tool arrived today, so I made up the cables that stabilize the mass balance arm.  Tool  does a very good job...

     
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Time: 1 hour
Total: 181 hours

May 6th

Fabricated port aileron push rod.  Cut out mass balance slots in port wing.  Riveted port aileron blind nuts onto hinges, trimmed and fitted aileron  and mounted it to the wing.  Fitted and bonded port aileron mass balance horn sockets...

           
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Time: 4 hours
Total: 185 hours

May 7th

Cut, installed and bonded the the polycarbonate tubing that will house the wiring for the port wingtip.  Installed and glassed the port flap mounting brackets Opened the port wingtip, in preparation for installing the position and landing lights...

        
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Time: 5 hours
Total: 190 hours

May 8th

Finished the flap mounts on the port wing.  Started building up the port wingtip for installation of lights and clear lens.  Pulled wiring for port wing lighting...

        
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Time: 3 hours
Total: 193 hours

May 10th

Fabricated the lens cover attachment points for the port, clear, wingtip.  Assembled the port (red) nav light/landing light.  Trial fitted to the wing.  Everything looks good.  Fabricated mounts for the port and starboard strobe assemblies...

        
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Time: 4 hours
Total: 197 hours

May 20th

Fabricated access panel for port tip lighting and permanently installed port light assembly.

     
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Time: 3 hours
Total: 200 hours

May 21st

Installed polycarbonate tube in starboard wing to accommodate wingtip wiring.  Reduxed aileron mass balance boxes into starboard wing...

  
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Time: 1 hour
Total: 201 hours

May 22nd

Opened up starboard wingtip and fabricated and laid up support for new, clear, wingtip.  Started cleaning up the starboard aileron mass balance boxes.  Opened wingtip lighting access panel and fabricated panel cover.  Finished fabricating starboard strobe mount. Pulled wiring for landing light and nav lights...

     

         
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Time: 4 hours
Total: 205 hours

May 23rd

Started filling the starboard aileron mass balance boxes.  Finished the starboard strobe mount and installed strobe tube.  Assembled the starboard nav light board and tested.  Began assembly of the starboard landing light.  My wife, Mary, installed the starboard wing strobe cable and secured it in place.  Then she coated the finished nav light assembly.  I did a bit more work on the starboard wingtip light access panel.

         

        
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Time: 4 hours
Total: 209 hours

May 24th

Made up wiring ends on starboard wing.  Finished starboard wingtip lighting access panel.  Assembled wingtip lighting components and installed into wing.  Hooked up wiring...

        
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Time: 3 hours
Total: 212 hours

May 25th

Control surfaces came back from the paint shop, after post curing.  Spent the bulk of the day sanding and priming.  Once primed, I started fine sanding one of the stabilators.  Looks like the surface will be extremely smooth for painting.  Some minor touch up and one more coat of primer, should do it...

        
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Time: 5 hours
Total: 217 hours

May 26th

Sanded on the stabilators.  They will require a little more touchup and another light coat of primer, but will be ready for paint, soon.  Projected painting is late next week.

Time: 4 hours
Total: 221 hours

May 27th

Finished the initial sanding on all parts.  Touched up all nicks and scratches and sanded them out.

Time: 5 hours
Total: 226 hours

May 29th

Sprayed final coat of primer on flying surfaces, then touched up remaining scratches and nicks.  They are ready for final sanding and then painting.  Fabricated a fuel sump system by installing a "T" in the fuel gage and fuel return lines, where they enter the fuel tank.  Opened a hole in each of the access covers to allow the drain valves to exit the fuselage.  I can now take fuel samples with a standard sample cup.  Arranged the tank gage and fuel return lines so that they create a low spot at the drain valve location.

        
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Time: 4 hours
Total: 230 hours

May 30th

Fabricated seat pans.  Once they were assembled, Mary applied a flox fillet and then a single BID reinforcement.  Once the bottom side was done, She applied a single BID layer to the top surface...

        
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Time: 3 hours
Total: 233 hours

May 31st

Finished seat pans.  Fitted upper fuselage to lower fuselage to check for placement of  components in the overhead panel.  Laid out components in respective places to check fit.  Laid up two layers of bid to both sides of card stock to fabricate panel.  Installed 3/4" vinyl tubing in upper rim of windscreen support, to act as a tunnel for running the wiring for the overhead panel.  Molded it in with flox and laid up two layers of bid.  Mary finished out the bid and applied peel ply...

     

     
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Time: 3 hours
Total: 236 hours

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