Today’s update. The tail cone, with the exception of the very aft end, (mounting the TW & empennage) is complete. The vertical stab & rudder are complete, with the exception of the vs end cap. The HS & elevators are in a similar state. The forward fuselage side panels are ready for installation, the firewall and fwd fuselage floor are in progress.
So the plan is to complete the fwd fusealage, mount the tail feathers & tail wheel, install the engine mount, add the mains and add the engine. What could go wrong?
The firewall is waiting for the delivery of some 1/8" centering drill bits. ETA July 5.
The spar tunnel components are in the process of being dimpled and countersunk. I have a rivet squeezer with a set of dimple dies, however there are a half dozen holes that the squeezer won’t reach. That’s on hold until I decide on a plan of action.
Yesterday, I ran into a little Sonex QC issue.
The white part attaches to the grey part. Both parts are Sonex produced. The plans call for 21 spaces. The grey part is in compliance with the plans. The white part has a row of 21 holes. It’s an easy fix with matched hole drilling, but it is an error that should be caught with the FAIR (first article inspection report).
I am experimenting with aluminum stabilizer caps. Mostly because the fiber glass ones were trimmed down by the original builder and I think they look dowdy. Yes, it’s going to weigh more than factory glass caps. However, I have a Corvair engine which provides a forward CG bias. Using a little weight in the tail to manage that bias minimizes any impact to the useful load.
The plan. The leading edge is basically a scaled down motorcycle fender. The sides are fender skirts. There are many YouTube videos on this. https://www.youtube.com/watch?v=XwGroFmWUUc
That covers the the cap to the main spar position. I have extra rudder/elevator material for the aft portion, with the top being formed similar to the leading edge. The leading edge as it now stands.
Due to the amount of stretching my EAA tech counselor advised using soft Al with a thickness of 0.040". I used: Amazon.com: 2pcs 1.5mm x 200mm x 200mm 1060 99.6% Pure Aluminum Sheet Metal Plate : Industrial & Scientific.
Optional treat.
Here’s a video of forming a WW I wheel pant. Notice how much material has been drawn into the form. https://www.youtube.com/watch?v=c_8q2uOGAKc