Shown with optional type
"E" gearbox
and air intake box.
|
Suggested for use on our Slingshot, Kolbra, Mark III Classic,
or Mark III Xtra
ROTAX 582
2 cylinder, 2 stroke liquid cooled engine
with rotary valve inlet, electronic dual ignition, dual
circuit cooling system with integrated water pump and
thermostat, exhaust system, rewind starter. Single or
dual carburetor options available.
Our Engine Accessory
Packages include Rotax accessories (oil injection tank,
dual radiator) and Kolb Aircraft's accessory package
(Kolb Kit), and inbound freight.
See
installation weights and fuel consumption below.
TECHNICAL
DATA SHEET
PERFORMANCE
DRAWING
|
|
Suggested for use on our Slingshot, Kolbra, Mark III Classic,
or Mark III Xtra
ROTAX 912
4 cylinder, 4 stroke
liquid/air cooled engine with opposed cylinders, dry
sump forced lubrication with separate 3l (.8 gal US) oil
tank, automatic adjustment by hydraulic valve tappet, 2
CD carburetors, mechanical fuel pump, electronic dual
ignition, electric starter, integrated reduction gear i=
2.273 (optional 2.43).
Our Engine Accessory Packages include
Rotax accessories (oil cooler, radiator, stainless steel
exhaust) and Kolb Aircraft's accessory package (Kolb
Kit), and inbound freight.
See installation weights
and fuel consumption below.
ENGINE
DATA SHEET
|
|
|
Suggested
for use on our Slingshot, Kolbra, Mark III Classic, or
Mark III Xtra
ROTAX 912S
4 cylinder, 4 stroke
liquid/air cooled engine with opposed cylinders, dry
sump forced lubrication with separate 3l (.8 gal US) oil
tank, automatic adjustment by hydraulic valve tappet, 2
CD carburetors, mechanical fuel pump, electronic dual
ignition, electric starter, integrated reduction gear i=
2.43.
Our Engine Accessory Packages include
Rotax accessories (oil cooler, radiator, stainless steel
exhaust) and Kolb Aircraft's accessory package (Kolb
Kit), and inbound freight.
See
installation weights and fuel consumption below.
ENGINE
DATA SHEET
|
Typical Installation weights for Rotax 2
stroke aircraft engines
|
|
582 |
|
KW/HP |
48.0 |
64.4 |
|
Items |
Kg. |
Lbs. |
|
Engine with carbs |
29.2 |
64.4 |
|
Exhaust system |
5.1 |
11.2 |
|
Air filter(s) |
0.3 |
0.7 |
|
Dual Rad set |
2.7 |
6.0 |
|
|
|
|
|
No Drive - No E/S |
37.3 |
82.2 |
|
Weight to Power |
0.777 |
1.277 |
|
|
|
|
|
With B Drive - No E/S |
41.8 |
92.1 |
|
Weight to Power |
0.871 |
1.431 |
|
|
|
|
|
With B Drive &
E/S |
46.7 |
102.9 |
|
Weight to Power |
0.973 |
1.598 |
|
|
|
|
|
With C Drive - No E/S |
45.3 |
99.8 |
|
Weight to Power |
0.994 |
1.550 |
|
|
|
|
|
With C Drive &
E/S |
50.2 |
110.6 |
|
Weight to
Power |
1.046 |
1.718 |
|
|
|
|
|
With E Drive
|
48.5 |
106.9 |
|
Weight to Power |
1.010 |
1.660 |
| |
Kg/KW |
Lbs/HP |
|
Specifications and performance data shown is
typical for the engines described and is general in nature. All
information is subject to change without notice. Information shown
is not to be used for flight or flight planning purposes. Consult
the appropriate engine and/or aircraft manual(s) for specific technical
information. |
Typical Installation weights for Rotax 4
stroke aircraft engines
|
|
912UL
|
912 ULS
|
914UL |
|
KW/HP |
60.4 |
81.0 |
73.5 |
100. |
85.7 |
115.0 |
|
Items |
Kg. |
Lbs. |
Kg. |
Lbs. |
Kg. |
Lbs. |
|
Engine with carbs |
55.0 |
121.2 |
56.6 |
124.7 |
64.0 |
141.1 |
|
Exhaust system |
4.0 |
8.8 |
4.0 |
8.8 |
4.0 |
8.8 |
| Air box |
- |
- |
1.3 |
2.9 |
- |
- |
|
Air filter (s) |
0.3 |
0.7 |
0.3 |
0.7 |
0.2 |
0.4 |
|
Radiator |
1.0 |
2.2 |
1.0 |
2.2 |
1.0 |
2.2 |
|
Oil Radiator |
0.5 |
1.1 |
0.5 |
1.1 |
0.5 |
1.1 |
| Engine truss assembly |
- |
- |
- |
- |
2.0 |
4.4 |
| Rectifier / regulator |
0.1 |
0.2 |
0.1 |
0.2 |
0.1 |
0.2 |
| Electric fuel pumps |
- |
- |
- |
- |
0.7 |
1.5 |
|
External alternator |
- |
- |
- |
- |
3.0 |
6.6 |
| |
|
|
|
|
|
|
| Installed weight |
60.9 |
134.2 |
63.8 |
140.6 |
75.5 |
166.4 |
|
Weight to power |
1.008 |
1.657 |
0.868 |
1.406 |
0.881 |
1.447 |
| |
Kg/KW |
Lbs/HP |
Kg/KW |
Lbs/HP |
Kg/KW |
Lbs/HP |
|
Specifications and performance data shown is
typical for the engines described and is general in nature. All
information is subject to change without notice. Information shown
is not to be used for flight or flight planning purposes. Consult
the appropriate engine and/or aircraft manual(s) for specific technical
information. |
Typical Power
Torque and Fuel Consumption for Rotax 2
stroke aircraft engines
|
|
Max
RPM |
Max Power |
Max Torque |
Fuel
Consumption |
|
|
|
KW |
HP
|
NM
|
Ft
Lb. |
g/KW
Hr |
Liters/Hr |
US Gal/Hr |
Imp.
Gal/Hr |
|
582 |
6800 |
48.0 |
65 |
75 |
55.3 |
410 |
27.3 |
7.2 |
6.0 |
|
Specifications and performance data shown is
typical for the engines described and is general in nature. All
information is subject to change without notice. Information shown
is not to be used for flight or flight planning purposes. Consult
the appropriate engine and/or aircraft manual(s) for specific technical
information. |
Typical Power,
Torque and Fuel Consumption for Rotax 4
stroke aircraft engines
|
|
912
UL |
912
ULS |
914
UL |
|
Power setting (%) |
65 |
75 |
100* |
65 |
75 |
100* |
65 |
75 |
100* |
|
RPM |
4800 |
5000 |
5800 |
4800 |
5000 |
5800 |
4800 |
5000 |
5800 |
|
|
|
|
|
|
|
|
|
|
|
|
Power |
|
|
|
|
|
|
|
|
|
|
KW |
37.7 |
43.5 |
59.6 |
44.6 |
51.0 |
73.5 |
47.8 |
55.1 |
84.5 |
|
HP |
50.6 |
58.4 |
81.0 |
59.8 |
68.4 |
100.0 |
64.1 |
73.9 |
115.0 |
|
|
|
|
|
|
|
|
|
|
|
|
Torque |
|
|
|
|
|
|
|
|
|
|
NM |
75.0 |
83.0 |
98.1 |
88.7 |
97.4 |
121.0 |
95.1 |
105.2 |
139.1 |
|
Ft Lb |
55.3 |
61.2 |
72.3 |
65.4 |
71.8 |
89.2 |
70.1 |
77.6 |
102.6 |
|
|
|
|
|
|
|
|
|
|
|
|
Fuel
Consumption |
|
|
|
|
|
|
|
|
|
|
Litres/Hr |
15.8 |
19.2 |
23.8 |
18.0 |
20.0 |
27.0 |
18.3 |
21.4 |
34.0 |
|
U.S. Gal/Hr |
4.2 |
5.1 |
6.3 |
4.8 |
5.3 |
7.1 |
4.8 |
5.7 |
9.0 |
|
Imp.
Gal/Hr |
3.5 |
4.2 |
5.2 |
4.0 |
4.4 |
5.9 |
4.0 |
4.7 |
7.5 |
|
*Maximum take off power.
Specifications and performance data shown is
typical for the engines described and is general in nature. All
information is subject to change without notice. Information shown
is not to be used for flight or flight planning purposes. Consult
the appropriate engine and/or aircraft manual(s) for specific technical
information. |
The
IVO PROP operates on a COMPLETELY NEW AND UNIQUE adjustable
pitch system that allows for substantially less hardware and
rotating mass than any other ground pitch adjustable prop. The
unique pitch adjustment design operates on the principle of
twisting the blades through the chrome-moly alloy steel
torsional rod cast inside the blade. The outer end of the
torsional rod is firmly anchored inside the outer blade
section. The round torsional rod is capable of rotating inside
the blade, except for the outer end.
Adjust
the pitch on the ground in a matter of seconds by turning the
screw adjustor in the center of the prop. The super cams are
installed on the end of the torsional rod. Each super cam fits
into the groove in the screw adjustor. Turning the screw
adjustor causes each cam to rotate and turn the torsional rod
twisting the blade changing the prop pitch.
 |
IVO PROP Ultralight Model (2 or
3-blade)
For engines up to 100 hp
18"-52" or 35"-70" pitch range
48"-72" diameter
- in flight
or ground adjustable pitch
- for
engines up to 100 H.P.
- carbon/graphite
fiber/composite
- 30 day
money back guarantee
- all blades
protected by stainless steel leading edges
- light,
strong, efficient, quiet, smooth
- low drag
hub
|
- unique
pitch adjustment design no protractor or pitch
blocks required for ground adjustment
- beautiful
high gloss black gel kote finish
- easily and
quickly converts from 3 blade into 2 blade
configuration - giving you a spare blade
- blades
individually replaceable
|
|
| Warp Drive carbon fiber propellers
These props are made of a solid carbon fiber matrix
(no foam core), have ground adjustable pitch and can
be configured with 2 to 12 blades. They may be used on
most home-built, experimental and ultralight aircraft,
including airboats and hovercraft. These props are
compatible with most engines. Warp Drive manufactures
propellers for applications where engine horsepower
far exceeds 115 hp unlike some sport propeller
manufacturers. Warp Drive, Inc. offers a lifetime
guarantee of complete satisfaction to the
original purchaser on all of their propellers.
4" prop spacer is required with Rotax 912/912S
engines. |
3-Blade
Prop with HPL Hub.
Shown with Optional Nickel Leading Edges,
Painted Tips and Tapered Tips. |
 |
Tennessee 2-Blade Wooded Prop
Each Tennessee propeller is solidly built by
skilled craftsmen from the finest selection of
hardwoods. The laminated propeller is carefully
assembled, carved, balanced and finished. Standard
Rotax hub bolt pattern.
This is your basic, least expensive propeller
choice. |
 |
 |
EIS Package
2-stroke with built-in altimeter/ROC, wiring
harness |
EIS Package
4-stroke with built-in altimeter/ROC, wiring
harness |
|
 |
|
3" Airspeed Indicator
Need information about this. |
Voltage Regulator
You will only need this if your installation has a
battery.
|
 |
 |
|
Altimeter
2-1/4", 10,000 |
|
|
|
|
