While my main effort was to complete all the welding on the fuselage I had to re-focus my attention to the wood floorboards and seating attachment issues. That’s because metal tabs and seat mounts had to be welded on the fuse to hold them down. I chose 5/16″ exterior grade plywood and carefully cut it out to fit around tube joints and around the control sticks. This was not to be the final finished floorboard. In fact I ended up fabricating three different floorboard patterns until I ended up with a suitable design that evolved with other changes I made along the way.
During this early phase of construction I was reminded of the labor intensive method used for annual inspections for my Cessna Skyhawk. My A&P (Airframe & Powerplant) Mechanic at the time had the complete cockpit interior removed including the seats and carpeting and all the floorboard inspection panels were also off. This close up inspection is to check for airframe corrosion, control cable integrity, pass through wiring integrity, fuel line integrity, etc. But my mechanic also found a large mouse nest which certainly did not belong there!
This led me to think how easy or difficult it would be to inspect my homebuilt when it was finished. The plans specified that all interior sidewall sheet metal panels have a lip or 90 degree edge to be used to attach to the wood floorboards. This would require me to completely remove all the metal sidewalls just to get to the floorboard removal and that would be incredibly difficult and time consuming. The plans also specified a fabric belly and Yes, I could have added several removable inspection rings but they are very small and difficult to get into. Thus I decided in the months ahead to design a system of easily removable full width belly panels and omit the fabric belly altogether.
During this phase of building was the time I also purchased and modified a pair of Cessna 172 seats and removed the upholstery and removed 3 inches of metal frame width and re-welded them back together.
- Tagged aircraft, airplane, aviation, cockpit, experimental, experimental aircraft, floorboards, fuselage, homebuilt, homebuilt aircraft, pilot, Piper, welding
The Wag Aero “2 + 2” model designation refers to the airplanes seating arrangement which means there are two seats in front and two seats in back. However the seats in back are really only suited for children of 12 years old or less or one adult passenger. The fuselage measures only 5 inches wider compared to a Piper Super Cub which makes one wonder why the Sportsman designer thought the extra five inches would allow side by side seating versus the tandem seating arrangement for the Super Cub,
I soon realized this cozy seating arrangement when I jury rigged a couple of front seats using cement blocks and 2 X 6 board seat backs and also placed a fabric sling in position for the back seat. I also made a cardboard template of the instrument panel and for the first time I could sit in the cockpit and feel for myself the interior layout of the aircraft.
I was struck with just how narrow the cockpit was. I immediately rechecked the plans to see if there was any error, but it checked out right. I then measured the interior width of my Cessna 172’s cockpit and was quite surprised to find it was only one inch wider than the Sportman. These measurements were taken at the width of the instrument panel. The major width difference between these two airframes is because the Cessna’s cockpit width remains mostly constant all the way down to the floorboard where as the Sportsmans cockpit width tapers down from 38 inches to 30 inches nominally, thus affecting the seat width. It was now no surprise why Wag Aero specified to remove 3 inches of seat/back width from a Cessna 172 seat and reweld them back together. Using standard Skyhawk seats would never have fit.
My concern for this ergonomic issue was not over and many months later I would develop a solution for this narrow width problem by designing special plexiglas bubble doors that would add 8 inches of interior elbow room to the cockpit without modifying the airframe. In later posts I will describe the tooling and fabrication methods used.
- Tagged aircraft, airplane, aviation, cockpit, experimental, experimental aircraft, homebuilt, homebuilt aircraft, pilot, Piper, seating, Super Cub
A few years ago my wife Diane and I combined her expert graphic design talents with my passion for Aviation and opened our first online “Cleared To Land” store on Zazzle which is a “Print on Demand” online merchandise source that prints graphics on a wide variety of men’s and women’s apparel and miscellaneous items in quantities as little as “one at a time”. If you click on the “Store” tab on the top of our home page it will take you to 60 of our most popular product designs but there are literally 100’s of more designs if you link directly to our complete Zazzle “Cleared to Land” Store.
There you will find exciting General Aviation, Military, Aircraft Make & Models, Pilot and other themed graphic merchandise available on T-shirts, Hoodies, Hats, Ties, Totes, Mugs, Bumper Stickers, Keychains, Address Labels, and even Postage Stamps. Also, most of our designs can be personalized with Name, Pilot Rating, N Number, Airport Identifier, etc. We would also be happy to add a new design at your request.
We are always updating our store with new designs so please check back occasionally to see what’s new.
- Tagged Air Force, aircraft, airplane, airport, aviation, aviation shirts, Cleared to land, co-pilot, flying, general aviation, military, pilot, pilot gifts, runway, wings
Let’s look a few years ahead at a three minute flight video showing the Aircraft Tail behavior during Cruise, Landing and Side slip maneuvers. A noticeable misalignment of the Elevator and Horizontal Stabilizer occurs in these various flight control movements. An adjustment to the Forward Spar will be needed to realign these surfaces.
- Tagged airplane, aviation, elevator, experimental, experimental aircraft, flight, flight test, homebuilt aircraft, horizontal stabilizer, pilot, Piper, stabilizer, test pilot
With the tail parts re-attached to the fuse it was time to re-check control movement of the elevators, trim tab and rudder. When this checked out, the elevators and horizontal stabilizers were removed for sandblasting and priming. A strobe light bracket from Univair was welded on the top of the rudder and later wired with a quick link harness prior to fabric cover.
The vertical stabilizer remained attached to the fuse and all the remaining tail parts were then hung from the rafters until the rest of the fuse was ready to cover.
Making the tail parts require accurate welding fixtures. Plywood panels were purchased and painted flat white. Then a 2″ pencil grid was drawn on the entire face of the panels. I then transposed the full size shape of the stabilizer, elevator and rudder on the plywood panels and located each rib location, hinge knuckle, cross brace etc. per the plan. The tubing was bent using a spring and soft rubber hammer and plenty of hand persuasion. Gradually I got the metal to agree with my curvy drawing. The horizontal stabilizer had a tricky leading edge taper that required spliting the last outboard length a few inches from the end and then removing sufficient material and then squeezing the ends together and re-welding the seam back together. The seam was then ground smooth.
The metal tubes and ribs were cut to size and fitted tightly together on top of the plywood pattern. Wood blocks were used to keep everything in their place during welding. Only tack welds were used to temporarily hold parts together. The assembly was then removed and finish welded on a welding table.
Welding the thick hinge knuckles and bushings was the most difficult due to the differental thickness of the knuckle and the parent tube. It was important to keep the heat directed to the heavier wall tubing and avoid burning through the adjoining thinner parent tube. Also keeping the hinge knuckles aligned was done with sacrificial bolts that sometimes became unknowingly welded to the finished assembly.
The plans also called for small 1/8″ rods in certain end locations. This was used as a anti bending brace to avoid end deformation during the later fabric cover and shrinking process.
- Tagged aircraft, airplane, aviation, elevator, experimental, experimental aircraft, pilot, rudder, stabilizer, trim, trim tab, welding
After the metal fabrication and system testing of the lift and lock mechanism was complete it was time to finish and protect the metal. A backyard sandblasting set up was used to clean and prepare the metal for paint. This set up was used for all smaller parts like tail pieces, rudder, landing gear legs, etc. I found out that sandblasting is very messy and its impossible to recover used blasting material when you do it outside. All future sandblasting was done by Southwest Sandblasting in Grand Rapids who do an outstanding job.
After the turtledeck was sandblasted it was cleaned with MEK and hand brushed with a 2 part epoxy primer from Randolph Coatings quickly followed by a 2 part epoxy J-3 yellow finish color. The 2 part epoxy paint protects the metal from corrosion and is impervious to MEK and all other Poly Fiber chemicals used for fabric attachment and finishing.
Because the inside fabric of the turtledeck can be seen when it is raised I used untinted Poly Brush to avoid having pink brush marks visible.
Let’s look ahead a few years and view a short 2 minute video taken from a belly camera during a 2012 test flight. This video was made after the aforementioned landing incident and was created to instill a sense of confidence for the test pilot…Me!
A bounced landing can feel especially severe but after reviewing the video I was quite surprised that the bounce was not nearly as high as it felt.
There are 4 cameras used in various locations on N728DC and in future posts I will describe their purpose and demonstrate their capabilities for both aircraft performance review and Pilot flight test analysis.
- Tagged aircraft, airplane, aviation, Belly Camera, Determination Video, flight, flight test, Flight Test Video, N728DC, pilot, test pilot
With the fuselage securely attached to the rotisserie it was time to learn to weld the 4130 steel tubing. Using a oxygen/acetylene gas rig and jewelers torch I test welded several scrap pieces together but it was’nt until I got expert instruction from Chuck & Craig Garret from my local EAA Chapter 145 that I finally gained some confidence.
I started welding on the fuselage lift handles and then the wing spar brackets, elevator bell crank assembly, floorboard mounts, rudder pedal mounts, engine mounts and landing gear and wing strut brackets. They say the best way to test a weld is to try to tear or break it apart. Unfortunately that destroys your weld. Sadly, a few years later I put some of my welding to a real world test during a bad landing/ground loop event. The good news is, the welds survived – the bad news is, the landing gear did not.
I will post more about that event in a future post including photos of the damage and the repairs made to the aircraft.
- Tagged aircraft, airplane, aviation, EAA, EAA Chapter, EAA Chapter 145, experimental, experimental aircraft, fuselage, landing gear, pilot, weld, welding, wing spar. engine mounts
Welcome to the Cleared to Land FLIGHT bLOG. This is the first post of hopefully many posts that will describe with text, photos and videos the building and flight testing process of Experimental Aircraft N728DC. Your comments are always welcome.
- Tagged aircraft, aircraft builder, aviation, aviation briefing, Chuck Helmholdt, Cleared to land, experimental, experimental aircraft, flight, Flight Blog, flight briefing, flight test, homebuilt, homebuilt aircraft, N728DC, pilot, Super Sportsman, test pilot