by Darick » Tue Jan 16, 2018 10:29 pm
Bryan, page 12 on my photo album. Holding the factory aft edge of the cowl firmly against the firewall, I drew a reference line on the cowl, 2 inches forward from the firewall. That way I could keep track of how much I was removing.
The cowl instructions show the bottom of the cowl blending into the fuselage. Before removing material, the cowl is way below the fuselage side. After cutting the material off the cowl, the fuselage and cowl blend nicely at the bottom. I forget exactly, but my first cut was about 1/2", I think? Every time I took some off the side, the top came down so that it was closer to the windshield line.
When I took material off, it was a consistent amount from the bottom to the top longeron. From the top longeron to the gas cap, it was tapered. Let me say that a another way. Let's say I took off 1" from the cowl side...the cowl top amount, to be removed, was 1" starting at the side corner (where the windshield starts) tapering down to 1/2" at the gas cap. The point is...I removed less material along the top than the side. You have to be sure to maintain the distance from the prop spacer to the center of the windshield.
After I was done, the cowl top still sprung up about 1/2". I didn't remove anymore material, being afraid some other dimension would be too "far out". As it ended up, the carb air filter and cowl were rubbing and had to be modified...but that's another story.
I can't remember when, but at one point I had to remove material off the aft bottom cowl or call it the trailing edge, maybe 1/4 to 1/2" because there is a slight up turn in the fiberglass at that point. By removing that material, the cowl was able to move up slightly.
If this is not descriptive enough, PM or call me.
Darick Gundy
Sonex #1646
N417DG
Taildragger, Aerovee, center stick, Prince P-Tip Prop
MGL E1, F2, V6 radio, Sandia Xponder, Reserve lift indicator (AOA), iFly 520
First flight! 10/21/2017