What is it?

Blue Jay 7 is a highly modified Weedhopper USA, Inc Super Single model ultralight aircraft with Model 40 fuselage tubes. A Super Single is a 2-place airframe delivered with only one seat. This plane was originally christened "Misisipi Flier" by its former owner, whom I bought it from on May 11th, 2001 near Meridian, MS.

For the next two months I did a complete tear-down, inspection, and rebuild, replacing all degraded hardware and improving, removing, or replacing questionable attachment schemes for items like the pod, battery, and the owner-made center control stick, changing it back to the factory location on the right hand side of the seat.

After a few flights, I discovering that the fuselage was twisted enough to cause a nasty imbalance in the wing's geometry if the wing struts were swapped one side for the other. I replaced all the old fuselage brace tubes, half of which were bent out of symmetry no doubt from a few too many hard landings by the previous own, with all new symmetrical tubing and trigonomically derived bends.

The 11-rib wing has a span of 28 feet, a surface area of 168 sq. ft., and is made from Dacron polyester sail cloth. It can lift up to 250 pounds of pilot and "cargo," has a maxium, full-throttle speed of 60 mph, a typical cruise speed of 40 mph, lands and takes-off at 30 mph, climbs at 500 ft/min, and has a range of around 60 - 70 miles on a 5 gallon tank of regular auto gas mixed with 2 stroke oil at 50:1.

The frame is tubular aircraft-grade 6061 T6 aluminum alloy with 0.095" walls on the front braces (axle to engine mount brackets) and 0.065" walls for the rest of the fuselage and wing struts. The wing's leading and trailing edge spars at the wing strut attachment points and the central section of the main boom have outer reinforcing sleeves. Everything is held together with 1/4" and 5/16" military-grade (AN) aircraft bolts, nuts, washers, clevis pins.

Weedhopper's are very stable, easy to fly, 2 axis craft (single stick controls rudder and elevator) with no aerilons or flaps. They are so easy to fly that I taught myself without any instruction. Doing so is not recommended. I simply spent a whole day running up and down Mecosta Morton's (27C) 2,000 foot grass runway west of Mecosta, MI learning how to steer on the ground. Then I started making little "crow hops" that grew higher and longer until there wasn't enough runway left to land. When that happened I was committed to the sky and circled back around at 200 feet off the ground for a perfect landing. Great Fun!!

Note: The photo at left is Collegedale Municipal Airport (3M3), not Mecosta Morton.

First Flight

 

On July 15, 2001, I hauled this yet un-named craft to the local airport (3M3) and spent a few hours in the morning practicing slow and high-speed taxiing, turns, and finally crow hops until I was confortably re-acquainted with the way this Weedhopper handled.

The movie to the left documents my first extended, 100 foot altitude 'crow hop' down the 4,700 foot runway. This version of the movie was motion tracked and stabilizated in Adobe After Effects to remove the hand-held camera shake. Right-click here if you want to save this 3.8 MB MPEG movie to your harddrive. Otherwise click on the image to view in a new window.

When a corner of the notch, which was cut out in the wing by hand by the previous owner to accomodate the engine, ripped in flight in late November, 2001, the time had come to retire the red and black sails, even though the previous owner said were only 2 years old. They had become just to weak for safe flight having been exposed during those 2 years to the sun's direct and indirect UV rays while it was hangared in his open-ended hay barn. So, I promptly replaced them with the current Blue Jay tail feather design in February 2002. These new sails were purchased from Ron Gonci, owner of The Ultralight Store in Winchester, CA. He even custom made them with a properly reinforced engine coutout notch at no extra charge!

It was at this time the plane was renamed to "Blue Jay 7" due to the color scheme and because of a personal faith statement where the anagram B = "Because," J = "Jesus," and 7 = the number of perfection.


The Engine
BJ7 uses a 50 horsepower Rotax 503, 2 cylinder, 2-stroke powerplant with a dual electronic Capacitive Discharge Ignition (CDI) system, a GPL electric starter, free-air cooling ram scoop, a single Bing 54 carburetor, and a 65" Model B PowerFin carbon composite adjustable pitch prop that's turned by a 2.58:1 type 'B' gear reduction drive.
The engine is mounted in the upright position, an unconventional orientation compared to the factory standard of hanging the engine upside down underneath the boom.

A heavy-duty, lightweight motor mount is custom made from various 6061 T6 aluminum bar with rubber Barry isolation mounts 9 1/4" apart.

This photo shows the current mount using nylon spacers between the engine and the top mounting bar.

This photo shows the previous owner's mount using aluminum tube spacers with washers. This design allowed the washers to deform and bend down into the tube.

The rest of the engine mount's structure is made up of two long angle brackets mounted to the boom with saddle blocks. Two AN5 bolts go through the whole assembly with the front bolt securing the wing's leading edge root brackets. Attached at the rear of the engine to the flat upper surface of the angle stock are the muffler hangers, Key West voltage rectifier/regulator, and starter solenoid.


The ram air scoop is a two-piece, fiberglass unit bolted to threaded cylinder head bolt extenders using large washers on either side of the scoop to spread the heavy vibration load over a larger area.

 

New Magnecor brand RFI suppressing spark plug wires are used along with resistive plugs and caps to help reduce (but not totally eliminate) radio interference in the aircraft communication band. The spark plug caps are secured from vibrating off the spark plugs by means of a twisted, form-fitting wire device made from a coat hanger. It is held by a bolt and washer to a threaded cylinder head bolt extender.
This red sheet of plastic provides a nice vibration and shock mount for a Mikuni DF52-21-D dual outlet fuel pump. Regular 1/4" automotive fuel line is used for the supply line from the tank and squeeze bulb primer (located above the pilot's head), while blue tinted 1/4" urethane tubing routes the gas up to the Bing 54 carbeurator.
Posi-Lock connectors are used extensively to butt-connect engine wiring. A braided copper strap can be seen just to the right of the yellow wires. It is used to ground the engine block to the fuselage rather than a heavy gauge insulated wire because a braid has more surface area than a wire and RFI currents travel on the outside surface of a conductor. Therefore, a braided strap helps reduce RFI noise. Sheilded audio cable is used for the tach and ignition kill wires.

A plastic project box is used as a junction box for the four temperature sensor leads; 2 EGT and 2 CHT. Shielded, two-conductor audio cable is used to extend the probes down to the instrument panel gages.

The farther two-piece aluminum project box contains a Tomar Neobe Dual-head Strobe power unit that drives two 20-watt strobe tubes. Notice the use of ferrite 'clamshell' chokes here and several other places to reduce RFI, especially on the B+ power supply lines. All this atention to RFI reduction allows my Icom A4 radio to get down to a squelch level of 2 (out of 9 levels) for clear, almost noise-free reception of weak, distant signals.

The Cockpit

Blue Jay 7 has a fiberglass pod faring and plastic seat tank originally made for the Phantom ultralight and a homemade 3/16" thick Lexan polycarbonate windshield.

 

A four-point racing-style seat belt harness keeps you firmly secured in rough thermals (old photos will be updated soon).

A carbon fiber panel made by fellow flyer Keith Murchison holds the following instruments (top left to right):  Magellan Meridian Color GPS, altimeter, dual CHT gage, tachometer, dual EGT gage, 0 - 80 mph airspeed indicator, and an Icom A4 radio. On the bottom (left to right): ignition kill switches, starter switch, carburetor primer, strobe and accessory switches, and coaxial power jack with its B+ lead wire wrapped around a clamp-on torroid choke . The GPS and radio use RAM mounts, each consisting of a RAM201 4" arm, a RAM202u12 ball base, and a RAM231 ball U-bolt tube mounting base.

The carbon fiber panel is about 3/16" thick, therefore needing this supporting framework to give it rigidity and a way to mount it to the pod. Note how the bolts for mounting the RAM ball bases serve double duty by also holding the frame's reinforcing corner joiner plates. The total weight with instrutments is 8 pounds.

A Power Sonic, 12 volt, 18 amp sealed lead-acid battery is strapped to the floor of the pod and to its left is a cigarette-lighter jack to power the GPS.

A plastic go-kart seat replaces the factory sling backrest and foam padded plywood seat. The foam pad from the original seat and another extra layer of foam padding were added under the seat's thinly padded vinyl slip cover to give a good 2 hours of flying comfort.

Modifying the factory nose wheel steering to extend it up into the pod was accomplished by bolting four, 6" extensions of of 3/16" x 1.5" aluminum bar stock to the front and back of the nose fork using the holes where the original steering tube was mounted. The steering tube was then bolted to the front of the extensions with spacers between each extension. This design has proved to be very strong, easy to assembly and disassemble, and required no welding.

The throttle is a standard factory clamp-on lever but uses an extra cut-down wing root bracket to form a cable support and "stop seat."

Brakes and Gear
Blue Jay 7 has drum brakes on the main landing gear, cable actuated by a modified Harley Davidson motorcycle clutch lever mounted on the control stick.
4.5" diameter Azusa brake drums were spot welded by the previous owner to the inside of the main landing gear wheel hub, which in none other than standard Kenda 4.80 x 4.0 x 8 two-ply wheel borrow tires and rims.

The band brake pads are mounted to the fuselage via a 3/8 inch bolt running through the multi-junction bracket and two reinforcing plates. The end of the cable is then clamped to the free end of the brake band.

 

The factory nylon bushings were replaced with 1" ID x 1 3/8" OD x 1 1/2" long oil-impregnated sintered bronze bearings. Two were needed for each wheel to span their 3" long hub/spindle. They are kept from spinning by hex-head set screws threaded in to each bearing with a matching hole in the standard 54" axle (solid aluminum or 0.120 wall 304 stainless steel tube).
Lighting and Miscellaneous

This 20-watt xenon strobe head, mounted on the front of the pod, is home-made from a 2" ID PVC plumbing pipe end cap, a Perko marine fresnel lens, and a 2" disc with a 1" hole to hold the strobe tube.
This one is mounted at the top of the rudder.
Close up view of the faired wing struts and method of attaching them to the main axle with stainless steel tangs. The fairings are made from 4" thick blue Dow builder's foam cut with a home-made "hot knife" and covered with vinyl house roof flashing. Click "Strut Fairing" in the menu above for construction details and methods.
I didn't like the wear and tear of the tail skid, which is actually a rudder sail protector to prevent the rudder from scraping on the ground and shredding the Dacron sail cloth, so I added this litle caster wheel.
This airspeed pitot (pee-toe)/static pickup uses 1/4" galvanized steel automotive brake line mounted in a small length of 1" C-channel stock bolted to the left wing's wing strut junction bracket using a quick disconnect wing nut. The plugged upper static tube has eight tiny holes drilled in its side and a rubber disc to adjust ambient air pressure. The lower pitot tube has a larger 3/8" tube added to help minimize changes in ram air pressure due to changes in wing angle of attack. 1/4" ID clear vinyl plumbing line is used to route the two pressures to the ASI gage in the cockpit.

When the wings are folded for transport and storage, the whole assembly simply lays in the sails as they are wrapped around the wing spar tubes.

The adjustment collar on the static tube is used to adjust static pressure to compensate for inaccurate readings. Air moving over the disc creates lower pressure behind it and higher pressure in front of it. When placed in front of the static port holes, the lower pressure behind the disc increases the indicated airspeed. When placed behind the holes, the higher pressure in front of the disc decreases the indicated airspeed.

Here is a simple, but very effective in-flight adjustable elevator trim tab. The tab/flap was made from a single sheet of thin aluminum, bent and riveted to form a wedge shape with upward and downward protruding 'ears' at each end used for attaching a return spring and an actuation cable.

The hinge is a 1" OD tube riveted to the tab/flap. 1" ID PVC plumbing fixtures serve as bushings on each end of the tube, while 1" wide straps of sheet aluminum bent around each bushing and bolted to the trailing edge of the elevator with 10-40 machine screws holds the assembly in place.

The actuator cable is nothing more than a common bike shift or brake cable with a shift lever mounted on the center fuselage brace in the cockpit. A cable adjuster is mounted to a 1" 'L' bracket to provide a seat for the cable housing.
A return spring that doesn't overpower the friction of the shift lever is the last part of the system.
All low speed aircraft exhibit what's known as P-factor, a propellor inducted yawing to the right or left that can be "tuned out" by this in-flight adjustable rudder trim system. Instead of a tab/flap, a simple tension spring is used pull the rudder in the direction that compensates for the "automatic" turn. Its tension (pulling force) is adjusted by another bike shifter cable with its shift lever mounted near the elevator trim lever. Varying the position of the 'L' bracket with its cable adjuster tunes the base amount of tension needed to keep the plane in a hands-off trim condition at the minimum cruise engine power and by adjusting the trim lever the spring tension is increased to trim for higher engine power.
To transport BJ7 from my home garage "hangar" to a suitable airstrip, I use a 5 x 8 wire mesh floor utility trailer, two 5 ft 2 x 6 planks for ramps, four friction-type clamp tie-down straps with hooks at each end to secure the axle to the front and rear of the trailer, and 2 rachet-type tie-down straps, one through the engine mount, the other at the rear just before the sub-fin. Nylon ropes bundle the ribs together and the wing struts are tied down to the floor of the trailer. The prop is kept from windmilling with another length of rope. The rudder and stabilizer are removed and placed on the floor of the trailer when going over 55 mph (if you have one of these expanded wire floor trailers, lay down some carpet first so your sails don't get chewed up!).
Transportation and Storage


Here's a time lapse view of my wings being folded up for transport. Even though the plane was never designed to do this as a feature, no modifications were required for it to be done, except for the addition of milk-jug plastic washers under each LE root bracket so they could smoothly rotate without grinding against the engine mount.

My fastest setup time from trailered to fully "assembled" is 25 minutes (one person hustling without distractions). Add 10 minutes for pre-flight and engine warm-up and I'm in the air in about 30 to 45 minutes after arriving at the airport. Tear-down takes about the same amount of time.

BJ7 has been and is currently being stored in my two-car garage just 2 miles away from the airport, many times trailer and all.