This is Jack B Hart's Legal(?) Ultralight Firefly Page
Notice to Visitors,
This page is getting out of hand. I started this page, in part, to help others who are building Kolb FireFly ultra lights, as a log of all the things that I have done to my FireFly, and as pay back to all of those who have helped me. When I started this I had no idea that it would become so long, but as time goes on, one keeps coming up with ideas on how to possibly make an incredible little plane just a little bit better and even more safe and fun to fly. I have added a section on flying techniques for people who wish to transition to a FireFly.
The changing of engines is an attempt to increase cruise range. The choice of the Victor 1 may not be the current best choice, but at the time I made the decision it appeared to me to be the best. I suspect the Victor 1 will not be the last engine on the FireFly. The Victor 1 was imported from a Canadian company, Speedwing, {2/28/15 - currently Simonini USA carries the engines and parts} is manufactured by Simonini in Italy. If you do not understand the importing process, you may want to read up a little about US Customs.
So if you are interested in reading and seeing what one old guy has gone through to fly, I welcome you to the rest of this web site. If you like some of the ideas, you are welcome to try them, but remember that with aircraft it is often better to proceed with small incremental change. That way any change that is made will probably make only a small difference in the way an aircraft flies, and this keeps the pleasure to a maximum and the surprise to a minimum. One of the objectives is to live to make another change and to fly again on another day.
Jack B. Hart FF004
Jackson, MO
10/15/2002
Update - December 6, 2009
Soon after mounting the Victor 1+, I realized that both the Rotax 447 and the Victor 1+ produced more HP than required to comfortably fly the FireFly at 55 mphi. I started looking for a smaller and lighter engine. I picked the MZ 34. It is 70cc smaller in displacement than the Victor 1+ and does not use a tuned exhaust system. It is air cooled rather that liquid cooled, and so, it is a much lighter engine. When I purchased the engine, it was rated at 27 HP.
By bulkhead mounting the MZ 34 up side down, one can greatly reduce above the wing engine profile drag, and there is no need for a propeller extension, radiator and coolant, and a separate fuel pump. While retaining the electrical starting system and discarding the mechanical starting system, initial calculations indicated that 42 pounds could be removed from the FireFly empty weight. Also, at cruise speed (55 mphi) the engine will be operating much closer to the torque curve peak. This and a lower AOA at cruise (minus 42 pounds), should enable a cruise fuel flow rate close to 1.5 gph.
To enable MZ 34 air fuel mixture management, the Tillotson carburetor was modified so that the high and low speed jet control needles can be adjusted from the cockpit. Also, the atmospheric vent from below the control diaphragm was fitted with a tubing nipple, and the carburetor throat was drilled and positive and negative dynamic pressure port nipples were installed. These ports will be used to see if the Tillotson air fuel mixture can be effectively controlled by varying the pressure on the control diaphragm much the same way as the pressure was varied over the Bing float bowl on the Victor 1+. If so, one can save another half to one pound by not using the mechanical system on the high and low speed jet needles.
As Winter is just about here, development efforts will be slow. As things are completed I will post the results on this site.
Jack B. Hart FF004
Winchester, IN
KOLB FIREFLY SPECIFICATIONS
|
Item |
Factory |
FF004 - Rotax 447 |
FF004 - Simonini |
FF004 - MZ 34 |
Wing Span |
22 ft. |
<-same |
<-same |
<-same |
Wing Chord |
5.54 ft. |
5.04 ft. |
5.10 ft. |
<-same |
Wing Area |
122 sq. ft. |
111 sq. ft. |
112 sq. ft. |
<-same |
Length |
19' 6"(same folded) |
<-same |
<-same |
<-same |
Height |
69 in. (same folded) |
70 in. |
70 in. |
63 in. |
Folded Width |
|
|
|
cannot fold |
At Wheels |
57 in. |
58 in. |
<-same |
<-same |
At Propeller |
60 in. |
60 in. |
65 in. |
10 in. |
Weights |
|
|
|
|
Empty |
less than 254 lbs. |
248 lbs.* |
252 lbs.** |
210 lbs.*** |
Gross |
500 lbs. |
<-same |
<-same |
<-same |
Fuel Capacity |
5 gal. |
<-same |
<-same |
<-same |
Load Factors |
|
|
|
|
Limit |
+4g, -2g |
|
|
|
Ultimate |
+6g, -3g |
|
|
|
Wing ->103-7 |
3.72 pd/sq ft |
3.98 pd/sq ft |
<-same |
3.57 pd/sq ft |
Speeds |
|
|
|
| |
Never Exceed |
80 mph |
<-same |
<-same |
<-same |
Top |
|
|
|
|
FAR 103.7 |
63 mph |
|
|
57 mph |
103.7 Drag |
|
12.1 |
<-same |
11.0 |
Actual |
75 mph |
74 mph(gps) 6400 rpm~` climb prop |
over 70 mph |
over 60 mph@ |
Cruise |
65 mph (70% power) |
|
|
|
Minimum
(no mushing) |
|
37 mph (gps)`
35 mph (gps)~` |
|
|
Stall |
|
|
|
|
FAR 103.7 |
27 mph |
|
|
26.1 mph |
Clean |
33 mph |
34 mph(gps) +~`/
31 mph |
|
|
Flaperons |
30 mph |
|
|
|
Ground Effect
Flight |
|
25 mphi~ |
|
|
Engine |
Rotax 447 |
Rotax 447 436cc |
Simonini Victor 1+ 382cc |
Comp. Rad. Eng. Inc. MZ34 313cc |
Power |
40 hp @ 6400 rpm |
40 hp @ 6400 rpm |
48 hp @ 6000 rpm 38 hp @ 5200 rpm |
27 hp @ 6250 rpm |
Power Loading |
11.4 pd/hp |
11.2 pd/hp |
|
15.2 pd/hp |
Gearbox or
Belt Ratio |
2.58:1 |
2.58:1 |
2.76:1 |
2.34:1 |
Propeller |
IVO 60 in. |
IVO 60" 2 blades |
Powerfin, B, 65" 2 blades 9.5 degrees |
IVO 54" 2 blades |
Takeoff Distance |
150 ft. or less |
<-same |
<-same |
<-same |
Rate of
Climb |
1000 fpm |
6400 rpm max 800-1000 fpm^~ |
6,000 rpm max 700-800 fpm~
???? | |
Pilot Weight |
|
200 lbs |
200 lbs |
200 lbs |
Cruise Angle of Attack |
|
climb prop 4 Degrees (6400 rpm)~
7 Degrees (5600 rpm)~ |
|
|
*Includes brakes on four inch wheels, nine inch chord ailerons,
strobe lights, vortex generators, oil in B gear box, and cockpit
adjustable trim for pitch and roll.
+Actual/Computed for 170 pound pilot.
~Vortex generators installed
^Summer - Winter with climb prop
`Altitude - 2000 ft. & average of up and down wind runs
**Includes brakes on four inch wheels, nine inch chord ailerons,
vortex generators, 2.7 lbs of coolant, electric start, battery,
cockpit adjustable radiator shutter and trim for pitch and
roll, seat cushion, and fairings on wing struts, rear of fuselage,
aileron torque tubes and push/pull tubes.
***Includes brakes on four inch wheels, nine inch chord ailerons,
vortex generators,electric start, battery, cockpit adjustable air/fuel
mixture control and trim for pitch and roll, seat cushion, and fairings
on wing struts, aileron torque tubes and push/pull tubes. No propeller
extension.
|
|
|