Announcement

**jaredyates** · 05-06-2025, 01:46 AM

Glad to see you here Sam! Let me know when you are ready to host a visit.

**SpruceForest** · 05-06-2025, 06:19 AM

Brilliant project. One consideration... the transponder rule exempts aircraft without engine-driven electrical systems from equipage; the ADS-B rule differs a bit in that it exempts aircraft without an installed electrical system from equipage. I don't believe the FAA has a problem with self-contained battery-powered starting systems on powered gliders, etc., but having a panel-mount comm radio might be pushing that interpretation of 91.225e.

I would suggest two things: a) ensure you are on solid regulatory ground with the FAA (FSDO avionics inspector and the ACO) re: what constitutes an installed electrical system, and b) provision for a belly-mount antenna (ground plane; cable access) for operation at 5W or less at 978MHz or 1090MHz to accommodate both future changes to 91.225e interpretation (this stuff happens, and seeing government agencies tends to get expensive quickly) and the pressures that new entrants such as AAM and UAS are placing on the current 'see and avoid' visual separation system.

**rodsmith** · 05-06-2025, 08:40 AM

Welcome Sam, looks like you are off to a great start on the project!

**slscott715** · 05-11-2025, 04:08 PM

My goal this week was to get the tail surfaces mocked up and the elevator and trim control systems put together. This proved to be an overly-ambitious goal.

I leveled the fuselage and got the -2 degree incidence set on the stab tube. I had to remove approximately .150” from each spacer to obtain this, adjusting each spacer individually to maintain level left to right. I did this with a little known tool called a reverse spotface cutter. This made removing material from the spacers with precision a breeze. After installing the stabilizers, I found the stab struts too short and the upper flying wires too long. Also, the elevator hinge bearings that came with my kit were too large, as others have experienced, so I was unable to install the elevators. These problems made me suspicious that something may be dimensionally off with my fuselage/tail parts. After two days of checking all the dimensions against the plans, I’ve not been able to find any discrepancy. I squared the tail using straps to get the required dimensions for struts and flying wires.

I did manage to assemble my shock struts this week after gettin g the springs in from backorder. I started by thoroughly cleaning all parts of the shock assembly. The IDs of the piston tubes were packed with a combination of grease and chips and required extra attention. I urge anyone assembling their shocks to inspect and clean their piston tubes before assembly as fluid does need to pass freely through the ID and at least one of mine was completely blocked. After cleaning, assembly went smoothly with the use of a piece of tubing and a bolt to compress the spring, allowing the snap-rings to be installed. I installed the rod-ends with a bit of EZ-Turn lubricant (previously now as Fuel Lube) on the threads. This acts as a thread lubricant and also seals the thread as hydraulic fluid will be present on the back side of these threads.

As always, Virgil and the folks at Bearhawk have been extremely reliable and swift to help with these issues and it is much appreciated. Hopefully, I’ll have more progress to report next week.

Attached Files

**arborite** · 05-12-2025, 06:20 AM

Have you fit your struts to your gear legs yet? It seems most of this design require some work to get alignment without binding. The newer Patrol and maybe others have heim joints on both ends. The LSA still has the bushing on the lower attach point which makes alignment at the top a big challenge. If I had to do it again, I would have assembled the shock tubes without the springs to allow full range of motion on the gear to check alignment in all positions. one of mine required a hefty bend in the strut to get it to work. There is still a rocking couple in the lower attach point which is not ideal, but I bent the strut enough so it allowed full motion without undue stress on the lower bolt. Time will tell if this is ok. The alternative is to modify the strut and lower attach point to accept the heim joint.

**slscott715** · 05-18-2025, 10:36 PM

A decent amount of progress was made on the LSA this week despite some setbacks.

Continuing on with the tail, I found that my tail brace wires were quite a bit too long on top and just slightly long on the bottom. After speaking with Virgil, I found out that my tail brace wires came from a new supplier and may have been improperly sized. With the help of my flying/build buddy, Randy, we measured everything against the plans to verify there were no issues with the fuselage or tail. All checked out ok so we started looking at ways to make the flying wires work if possible. We determined that I could make new upper flying wire tabs that were shorter than the ones supplied in the kit as well as shortening the kit supplied tabs on the stabilizer upper surface. This allowed me to use the upper flying wires by cutting off the excess threads protruding through the clevis. The lower flying wires were usable after shortening the threads by about 1/4". All the flying wire tabs supplied with the kit had 1/4" holes drilled in them and the flying wire fork ends had 3/16" holes so I made a couple bushings to use in the lower flying wire tabs. This problem was taken care of on the upper tabs when I shortened them and re-drilled the holes. Finally, all the tail brace wires were installed and the tail squared to the fuselage. The bearings for the elevator center hinge were not in my kit, so I used some bearings from a local supplier for mock-up while waiting on the proper bearings to come from Bearhawk.

With the tail all installed and rigged, I next began working on the elevator & trim control systems. I installed the torque tube, control sticks, elevator pivot, and the fwd and center elevator pushrods. When I got to the aft elevator pushrod, I discovered that the threads in the pushrod were 5/16"-24 and my rod-ends were 3/8"-24. I referenced the plans to see how it should be configured and was not able to find a specific callout on the aft elevator pushrod for thread sizes or rod ends used. Assuming the rod ends are the same as the center pushrod, it should be 3/8" and being that those were supplied in the kit, I concluded that the pushrod must have the wrong threads. I ground away the nuts welded on the ends of the pushrod, opened up the holes to 3/8 and welded AN315-6R nuts to each end. The rod-ends did not have bushings so I turned a couple out of brass that I had on hand. I was then able to hook up the elevator pushrod and make adjustments to get proper travel.

With the elevator controls in, the trim controls were next on deck. I mounted the trim lever, shortened the trim torque tubes as required for proper placement of the control horns, installed the trim tab push/pull rods and set everything at mid-travel. With the system mocked-up, I drilled the horns to the torque tubes and installed bolts. I made bushings to go on the threaded studs of the trim lever and made links out of .090 4130 to attach turnbuckles to. Fairleads were installed and the cables fabricated in place. With the trim system all mocked up, I cut the trim tabs loose from the elevators and tried it out. Some adjustments to the turnbuckles to obtain proper cable tension and placement of the lever finished off the trim system.

With the tail and fuselage controls all completed, I turned my attention to the landing gear. Per Arborite's suggestion, I removed the springs from the shock struts, installed the gear legs and and checked for issues with alignment and binding throughout the range of motion. After the issues I had with the tail, I was happy to find that everything moved freely without modification. I reinstalled the springs in the shock struts and attempted to fit the wheels to the gear legs. The bearings would not go on the axles beyond the threads so I mic'd the ID of the bearings and the OD of the axles and found that there was only about .0007" clearance between the two. A little work on the axles with emery cloth did the trick so I installed the brake torque plates, spacers and wheels/tires on the gear legs for the first time. There have been others that had issues with the Matco nuts being too tight on the threads but mine went on ok, luckily.

At this point, the airplane is entirely too close to being ready for "hangar flying" status so I turned my attention to the tailwheel. The tailwheel spring would not insert fully into the socket on the fuselage because of some weld penetration into the ID of the socket. A 3/4" flap disc in a die grinder made quick work of that and the tailwheel spring was installed. The tailwheel slid onto the tailwheel spring and with a little reaming to remove paint from the holes, it was bolted on. I was then able to set the airplane down on its own wheels, install the seat with a bottom cut out of some scrap OSB and cushions made from shipping blankets and try the airplane on. Stick and rudder pedal geometry felt great and notes were taken for positioning of the throttle controls.

This weeks progress was very rewarding and felt like a big step forward. It was neat to be able to sit in the cockpit and make airplane noises for the first time. I will upload pictures associated with this post in the next day or two.

**slscott715** · 05-19-2025, 05:56 AM

Here are the pictures from last night’s post. I guess I was more focused on building than pictures this week. If there’s any details that someone would like to see, let me know and I’ll try to take some more photos.

Attached Files

**slscott715** · 05-26-2025, 09:52 PM

Between working and a couple flying adventures this week, I was able to make some progress on the LSA.

Having the tail feathers, trim and elevator control systems all rigged, I marked the hinge locations, noted the exit points of the rudder cables and trim horns through the fabric and removed the tail feathers. This helped a lot with getting around my cramped workspace.

I set my sights on the landing gear next. I clamped the brake caliper torque plates to the mounting plates and, once satisfied with the placement of them, I put an index mark across the two. The gear legs were then removed from the airplane for jigging and drilling. I used the spacer supplied with the kit to center the torque plate around the axle. The torque plate ID is 1.5” and the spacer OD is quite a bit smaller so I wrapped masking tape around the spacer until the OD would fit snugly inside the ID of the torque plate. This held the torque plates centered while I lined up the index marks and clamped them tightly to the mounting plates. I used a 12” drill bit to drill the holes, installing temporary bolts in each hole as they were drilled to maintain alignment. Once all the holes were drilled, I had to use a pencil grinder to remove weld near the backside of the bolt holes to allow the nuts to sit flat against the mounting plate. I seem to recall an engineering change from a while back that recommended stitch welding the mounting plate to the axle to alleviate this issue but the gear legs supplied with my kit were welded all the way around. If anyone is familiar with this, let me know. After a little de-burring and touch up paint, the brakes were mounted.

I noticed when I installed the wheels, I couldn’t quite get the bearings fully seated before the nuts got tight. With the wheels removed and the nuts threaded onto the axles, I found that they got tight about 1/4” from the end of the threads. I used a 1-1/4“x16 split die to cut the threads a little deeper until the nut would run all the way down to the end of the threads. Reinstalling the wheels proved this to be successful so I torqued the axle nuts according to Matco’s instructions and marked the hole locations for the axle nut cotter pins. The wheels were once again removed and the holes drilled. I reinstalled the gear legs, shock struts, wheels and brakes.

I focused on mounting throttle quadrants next. This led me into a neat little side project. The throttle quadrants I got with the kit are beautiful, anodized aluminum, two-lever units popular with the RV crowd. The only issue is I don’t really want a mixture control in the back seat. I couldn’t find a single-lever quadrant to match the ones I have so I decided I could make one. I disassembled the extra two-lever quadrant and rough-cut the mixture side off the machined top cover with a bandsaw. My friend Randy has access to a milling machine at his work, so we used it to remove the remaining material from the top cover, allowing the side cover to sit flush against its side. The bushings at the bottom bolts were shortened to match the width of the top cover and the bolts were all exchanged for shorter ones. The mixture lever and additional spacers were removed from the buildup. To retain the functionality of the friction lock, I had to cut additional threads on the shank of the replacement AN3 bolt before installation. With all the parts modified as needed and painting the exposed aluminum to match the black anodizing, I reassembled the throttle quadrant. It worked out perfectly and looks exactly like I wanted it to.

There are no provisions for mounting the throttle quadrants so I had to figure out where and how to mount them. I mocked-up the front and rear seats, floorboards and rudder pedals. I stacked shipping blankets in the seats to simulate my future cushions and sat in each seat, trying different throttle positions until I settled on my preferred locations. Now that I established the “where”, it was time to figure out the “how”. I used poster board to make templates for mounting brackets for each throttle and translated that onto some .040” 2024 aluminum sheet. After cutting and bending the aluminum brackets, they were test fit and drilled to their final locations. Once satisfied with the fitment, I drilled the mounting holes and installed the throttle controls to the brackets. These assemblies were clecoed back into their respective positions. With all of the primary flight/engine controls mounted, hangar flying commenced. Man, does this thing sit good!

Attached Files

**slscott715** · 05-26-2025, 09:55 PM

Additional pictures from this weeks progress…

Attached Files

**slscott715** · 06-01-2025, 09:10 PM

A little more progress to report this week. I covered the seat frames with heavy duty fabric in preparation to drop them off for upholstery. I bolted the engine mount on and installed the engine so I could begin mounting components on the firewall. I started with the brake reservoir, then started mocking up the cabin heat box. I ultimately decided to order a different cabin heat box because I couldn’t get “push-off/pull-on” controls with the inlet/exit holes oriented like I needed. From there, I moved on to the oil cooler mounting. I found a location that would place the mounting holes adjacent to the fuselage tubing behind the firewall. I fabricated clamps that would transmit the load of the oil cooler directly to the tubing rather than relying on the thin firewall to support it. I mocked up an oil cooler shroud/brace out of poster board and after a few iterations, I transferred the layout to .040” aluminum and cut/bent up the final part. I will be riveting on an 3” duct flange to the brace once it arrives from ACS. All of the associated mounting holes were drilled through the firewall and all parts installed with temporary hardware to check fitment. While everything was in place, I made up the oil cooler hoses. The oil cooler mounting parts were then removed to be prepped and primed with EP-420 epoxy primer.

Attached Files

**slscott715** · 06-09-2025, 08:39 AM

I started this week with priming a batch of parts with EP-420 epoxy primer. After the primer cured, I installed nutplates on all parts that required them. I decided on a location and mounted the cabin heat box. The eyeball pass-throughs for the throttle, carb heat and cabin heat controls were then located, drilled and mounted. I would suggest to anybody installing the eyeball pass-throughs to buy the drill jig P/N AS-231. This makes locating and drilling the holes much easier and more accurate. I punched out the large holes in the center with a Hougen Rotacut hole cutter. If you don't have this set, do yourself a favor and pick one up. It's one of those rare tools that does its job so well, I'm amazed every time I use it.

The tubing arrived for the throttle slave rod to connect front and rear throttle controls so I turned my attention to that. I started by removing the throttle levers from the quadrants and drilling new holes for the slave rod to attach. These holes were drilled the same distance from the pivot on each lever so the throw of the levers would be the same front and rear. The quadrants were reassembled and measurements taken to determine slave rod length. I initially thought about welding nuts on the ends of the tube and using clevises for adjustability but I found it just as easy, cheaper and lighter-weight to form each end of the tube into a clevis. After installing it and verifying throttle operation, I removed the slave rod, throttle quadrants and throttle mounts for priming/painting.

Planning for removal of the gear legs, I went ahead with plumbing the brake system. A few of my fittings are on backorder but I had enough on hand to do one side up to the master cylinder. I installed all the fittings in the right-side caliper and master cylinder, located and drilled a hole in the top of the gear leg for a 90 degree bulkhead elbow and installed said elbow. I fabricated and installed the line inside the gear leg with rigid 5052 tubing. The flex hose from the gear leg to the master cylinder was then fabricated and installed to check fit. I was happy with how that turned out, so I duplicated the parts for the L/H side. The rest of the fittings should be here this week to finish the brake system between the master cylinders and the reservoir.

Saturday morning came around and we flew the Cubs to a nearby grass strip for a pancake breakfast. Fellow Bearhawker Jared Yates was also in attendance so we were able to talk Bearhawks and flying in general for a while. After eating too much and socializing a while, we made the short trip back to Boonville. Jared swung by our strip afterward to check out the project. I've spent a lot of time alone in the hangar working so it was great having a visitor who is as enthusiastic about Bearhawks as I am. Thanks for coming by Jared!

The last item on my goals for this week was to mount the battery box. After a lot of back and forth on battery choice, I've decided on using the Odyssey PC680 to run the starter and com radio. I plan to leave the airplane on a maintenance charger while the airplane sits in the hangar and while the lithium batteries are much safer than they used to be, I don't think I'd be comfortable leaving a lithium battery to charge unsupervised. Between the peace-of-mind that comes with using an AGM battery and the much lower cost, I'm willing to accept the weight penalty. With the firewall space filling up, I looked at alternative mounting locations for the battery box. With the help of my flying/building buddy, Randy, we decided to mount the battery in front of and below the instrument panel on the bottom side of the diagonal braces from the firewall to the fuselage sides. We fabricated a tray from .063" 2024-T3 that is secured to the tubes with adel clamps to which the battery box will mount. A flange was bent on the rear edge of the tray for rigidity and holes drilled to mount the box. After finalizing the mounting and fitment of the tray, the excess material was removed to lighten the part. The battery box will mount to the tray with a combination of 1/4" bolts and Camloc fasteners. This is to make installation and removal of the battery easier while still having the tensile strength of mounting with bolts. The battery can be inserted into the box, the assembly lifted up and secured with 2 camlocs to hold it in place while the 4 bolts are installed. The assembly weighs about 16 lbs so counting on 4G positive loading with 1.5x margin, it needs to support 96 lbs of downward force. This was tested with a force gauge to 100 lbs and showed no signs of deformation, let alone failure. The parts were then removed and prepped for priming. The location allows for convenient routing of wiring and installation of electrical components and saves a lot of real estate on the firewall. I feel that its an ideal spot for mounting the battery and I'm very happy with this setup.

That's it for this weeks progress report. Pictures incoming...

**slscott715** · 06-09-2025, 08:42 AM

A few pictures of this weeks work. Again, I was too preoccupied with building to take many pictures. I’ll try to take more and post them later.

Attached Files

Announcement

North Carolina LSA Kit Build Underway

North Carolina LSA Kit Build Underway

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