RANS S-6ES COYOTE II Specifications and Performance
SPECIFICATIONS
80 HP/100 HP
Wing Span
30.4 ft
Area
137.6 sq ft
Mean Chord
4 ft 6 in
Aspect
6.73
Length
20 ft 9 in
Height *
7 ft 8 in
Cockpit Width
45 in
Headroom
39 in
Legroom
41 in
Number of Seats
2
Doors
2
Landing Gear**
F/TD/TR
Baggage Volume ***
6 cu ft
Baggage Capacity
50 lbs
Auxiliary Baggage Volume
7 cu ft
Auxiliary Baggage Capacity
30 lbs
Fuel Capacity
18 gal US
POWER PLANT
912 UL /912ULS
Engine
Rotax 912 UL/912 ULS
Output
80 hp/100 HP
Oil Capacity
†
3.0 qts
Coolant Capacity
4.4 qts
Propeller Diameter
66 in to 72 in
Propeller Type
Wood
Gear Reduction
1:2.27/1:2.43
Fuel G.P.H.
4.5 /.5 gal @ 75%
PERFORMANCE
Take Off Roll
220 ft/210 ft
Rate of Climb
950 fpm/1250 fpm
Service Ceiling
14,000 ft/16,000 ft
Cruise
105 mph/110 mph
VNE
130 mph
Stall Clean
41 mph
Stall Flaps
36 mph
Roll Rate
80° /sec
Glide Ratio
9:1
Landing Roll
260 ft
Endurance
3.5 hrs/3 hrs
Range
385 miles/345 miles
WEIGHTS AND LOADINGS
Gross Weight
1200 lbs
Empty Weight
650 lbs
Useful Load
550 lbs
Wing Loading
8.7 lbs
Power Loading
15 lbs / 12 lbs
Limit Load Factors
+4 -2
* Trike height is shown, Taildraggers are 6 ft.
**F/TD/TR = Fixed Taildragger/Trike
*** Baggage Compartment optional.
Optional props available .
Performance at sea level and maximum gross weight.
