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Rans S-6ES
Coyote 2
The S-6ES went into production in
April 1990. It is the second generation of the original S-6 design.
Increased wing span through a fuselage re-design resulted in
improved performance and appearance. The ES denotes "extended span".
The design goals that the S-6 achieved represented a significant
advance in quick-build kit planes. The S6ES series takes this goal
even further. Using all pre-finished parts and pre-sewn skins, the
build time averages between 250 and 300 hours on the smaller
engines. Coyote II's can be built in the confines of an average
garage using normal shop tools and skills.
RANS offers two different wing sizes for the Coyote II. The
standard wing is constant chord and 34.5 feet in span with constant
chord ailerons and flaps. Area Two wings use the standard wing with
larger tapered ailerons and flaps. Take off and climb performance is
best with the stock wing. For 10 to 15 MPH higher cruise consider
the 116 wing. Stall is increased by 5 to 8 mph and take off roll is
60 to 100 feet more. The standard wing is best for floats and high
altitude applications.
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SPECIFICATIONS |
52 HP |
65 HP |
80
HP/100 HP |
|
Wing Span |
34.5 ft |
34.5 ft |
34.5
ft |
|
Area * |
155.25 sq ft |
155.25 sq ft |
155.25 sq ft |
|
Mean Chord |
4
ft 6 in |
4
ft 6 in |
4 ft
6 in |
|
Aspect |
7.66:1 |
7.66:1 |
7.66:1 |
|
Length |
20
ft |
20
ft |
20
ft |
|
Height ** |
9
ft |
9 f |
9 ft |
|
Cockpit Width |
42
in to 45.5 in |
42
in to 45.5 in |
42
in to 45.5 in |
|
Headroom |
39
in |
39
in |
39
in |
|
Legroom |
41
in |
41
in |
41
in |
|
Number of Seats |
2 |
2 |
2 |
|
Doors |
2 |
2 |
2 |
|
Landing Gear*** |
F/TD/TR |
F/TD/TR |
F/TD/TR |
|
Baggage Volume **** |
6
cu ft |
6
cu ft |
6 cu
ft |
|
Baggage Capacity |
50
lbs |
50
lbs |
50
lbs |
|
Auxiliary Baggage Volume |
7
cu ft |
7
cu ft. |
7 cu
ft |
|
Auxiliary Baggage Capacity |
30
lbs |
30
lbs. |
30
lbs |
|
Fuel Capacity |
18
gal US |
18
gal US. |
18
gal US |
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POWER PLANT |
503 |
582 |
912/912S |
|
Engine |
Rotax 503 |
Rotax 582. |
Rotax 912/912S |
|
Output |
52
hp |
65
hp |
80
hp/100 HP |
|
Oil
Capacity † |
n/a |
2.5
qts |
3.0
qts |
|
Coolant Capacity |
n/a |
4.4
qts |
4.4
qts |
|
Propeller Diameter |
66
in to 72 in |
66
in to 72 in |
66
in to 72 in |
|
Propeller Type |
Wood |
Wood |
Wood |
|
Gear Reduction |
1:2.58 |
1:2.58 |
1:2.27 |
|
Fuel G.P.H. |
4.0
gal @ 85% |
5.75 gal @ 85% |
4.1/4.5 gal @ 80% |
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PERFORMANCE |
|
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Take Off Roll |
235
ft |
160
ft |
190
ft/180 ft |
|
Rate of Climb |
500
fpm |
900
fpm |
1000
fpm/1400 fpm |
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Service Ceiling |
12,500 ft |
17,000 ft |
17,000 ft/17,500 ft |
|
Cruise |
80
mph |
95
mph |
100
mph/108 mph |
|
VNE |
120
mph |
120
mph |
120
mph |
|
Stall Clean |
38
mph |
39
mph |
41
mph |
|
Stall Flaps |
33
mph |
34
mph. |
36
mph |
|
Roll Rate |
70°
/sec |
70°
/sec. |
70°
/sec |
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Glide Ratio |
9:1 |
9:1. |
9:1 |
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Landing Roll |
250
ft |
250
ft. |
250
ft |
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Endurance |
4.5
hrs |
3.1
hrs |
4.4
hrs/4 hrs. |
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Range |
360
miles |
295
miles. |
440
miles/432 miles |
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WEIGHTS AND LOADINGS |
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|
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Gross Weight |
1000 lbs |
1030 lbs |
1100
lbs |
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Empty Weight |
500
lbs |
530
lbs |
600
lbs |
|
Useful Load |
500
lbs |
500
lbs |
500
lbs |
|
Wing Loading |
6.44 lbs |
6.44 lbs |
6.5
lbs |
|
Power Loading |
19.2 lbs |
15.3 lbs |
12.6
lbs |
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Limit Load Factors |
+4
-2 |
+4
-2 |
+4
-2 |
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* Larger Chord Aileron/Flaps
are available as option Area-2 (166.25 sq ft). |
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** Trike height is shown,
Taildraggers are 6 ft. |
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***F/TD/TR = Fixed Taildragger/Trike |
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**** Baggage Compartment
optional. |
† Includes 2-cycle injection or
4-cycle crankcase oil.
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