by builderflyer » Fri Oct 29, 2021 10:57 am
The part of the Sonex that is most structurally abused in the entire airplane is likely along the "spine" of the seat pan. Originally, the hinge along the spine was attached to an unreinforced channel section. Before long, through a Sonex service bulletin, an extruded aluminum angle was added to the top of the channel section for additional strength in that area. So the next failure on my particular Sonex was the hinge material itself that is attached to the extruded angle. Some of the hinge loops began to break off and sections of the hinge had to be replaced. The next point of failure, which has just occurred, is a crack in the seat material itself along the bend of the spine adjacent to the hole through which the seat belts pass. I've added a couple of reinforcements in this area and we'll have to see how long before another failure occurs here.
If I were to rebuild the entire seat pan on my Sonex, or if I was building a new Sonex it would be my intention to do two upgrades and they are: (1) add a doubler skin along the entire length of the spine, bent to match the corner of the pan and riveted to both the bottom and back of the pan (note that some builders have used a thicker material for the entire seat pan but they haven't said how that has worked out for them) and, (2) use a structurally upgraded hinge material along the entire length of the spine. The remainder of the seat pan installation has never been an issue.
Just my opinion,
Art,,,,,,,,,,,,,,,Sonex taildragger #95 (800 hours),,,,,,,,,,,,,Jabiru 3300 #261