Remarques
. Tuesday, 01 June 2010    -    Temps  
Changes
  • Edges. I opted for the leading edges of plywood instead of aluminum. To stiffen the part between the veins, I added reinforcements between two ribs.
  • Fastening low wing. The holes on the spar diameter is 5 / 16 so that the hole for the attachment on the fuselage diameter is 1 / 2. I also extended it to 5 / 16.
  • Washers welded to the fuselage station (1) in the engine mounts. I preferred to use steel triangles which follow the shape of the tubes.
  • Tension wires in the wings. In the wings of the above, I inadvertently made the holes at the line of rope instead of the center line. Many manufacturers have done the same and this does not result.

Advice
  • Do not trust the drawings of plans, they are often wrong.
  • Think for yourself and do not hesitate to question the plans.