Project: Classic181   -  
            Listing for Category : tail feathers
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Builder Name:Kevin Knutson   -  
Project:   Hatz - Classic   -   VIEW REPORTS
Total Hours:2982
Start/Last Date:Sep 09, 2016 - No Finish Date
Engine:Lycoming O-320
 
Friendly URL: https://eaabuilderslog.org?s=Classic181

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Apr 27, 2020     Vertical fin attach - (16 hours)       Category: Tail Feathers
Mounting the vertical fin to the fuselage had to be done prior to mounting the tailwheel. A 7/8" tube had been a stand-in for the vertical fin tailpost, and so all the fishmouthing and tube ends were ready to tack in place once the fin was in position. First ensuring it was square to the fuselage axes, both left-right and fore-aft was essential. Next, the leading edge of the fin is offset 1" to the left to minimize P-factor effects. Once all the locating was complete, the fin was clamped in position and tacked. Finish welding included the 1/4" tubing structure welded to the forward crosstube holding the leading edge of the fin (the dahlstrom) in the offset position. The last photo shows the post finish-welding tailpost excess bottom length prior to cutting off and welding the tailpost bottom fitment in place. That fitment is .090" 4130 steel and serves as the rudder limit stop and tailspring aft mounting location.


 
Apr 27, 2020     Horizontal stab attach - (11.5 hours)       Category: Tail Feathers
Horizontal stabilizers were attached by first locating the attachment crosstubes above the top longerons using wood blocks to determine the vertical dimension. The left and right stabs were positioned on the crosstubes, located properly from centerline and squared to the longitudinal axis of the airframe. Once all the positioning was complete, angled legs were fabricated and tacked to the crosstubes and longerons. Drilling the stabs to the crosstubes and finish welding the crosstube mounts completed the process.


 
Feb 27, 2019     Tail Flippers - (108 hours)       Category: Tail Feathers
Began construction of the tail flippers by bending the trailing edges of elevators and rudder using a Tony Bingelis-designed jig. It looks like a badly-shaped toilet seat. Fabbed from the underside of a junked tabletop, it's about an inch thick Masonite that is cut into various radius' around the perimeter and a hole cut in the center to allow it to be clamped in a vise. The perimeter was routed with a 3/8" cove bit to accept the trailing edge 3/8" tubing and later re-routed to 1/2" for the vert fin leading edge. The jig allows one to choose an area of particular radius to bend the various shapes required. Drew up full size templates to lay the bent bits on to contemplate if further bending is necessary on a given part. Strap hinges fabbed up by cutting tube sections and plate on the bandsaw, heating, forming and rosette welding. Ribs for the surfaces were sheared from flat stock, bent using a benchtop brake, forming channel lengths and tapered ribs for some components. Horizontal stab leading edges are 3/4"X 0.035 4130 steel. Packed tubing with pool filter sand and plugged prior to bending cold. Fabbed bending block from dimensional lumber screwed to the benchtop. Bending block radius is slightly tighter than required to allow for spring back. You need some leverage to do this, so left the tubing long and slipped a length of 1" steel conduit over the yanking-on end of the tube and slid it as close to the bending block as I could to isolate the bend to the block area. Steel bits for bellcranks and control arms were cut on a metal cutting bandsaw. A smart guy would have downloaded the available CAD files off the interwebs and had these parts water-jetted out. Sadly, I'm not that guy. Mongo just simple pawn in game of life. Which, is how I broke my vise, hammering the bends into some of these bits. (note the "toilet seat" bender now clamped to the bench top instead of in the vise for the vert fin bending) A particular joint exists on all the control surfaces and the vertical fin, it is where the 3/4" tube meets the 3/8" or 1/2" tube of the leading or trailing edges and falls on the hinge line. Heat forming the 3/4" tube at those joints required a notch on the hinge-line side of the tube to prevent squeezing that side of the tube toward the hinge line creating an interference. The notch allowed the 3/4" tube to form around the smaller tube but not bulge toward the hinge line. Fabbed tabs to attach tail flying wires (there's four wires) a pair on either side of the vertical fin and a pair each on the top side and bottom of the horizontal stab. Nothing in the plans referencing these at all, but are required. Referenced again Acrosport, Skybolt, Starduster and Cub drawings, settled on 0.090" thickness. Drew up dimensional diagram to determine bend angles required since all three pairs are different; Labeled : Larry, Moe and Curly. Probably ok.


 


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