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RANS S-10 SAKOTA
Wir bieten Ihnen RANS S-10 UL´s als Bausatz oder Ready To Fly.
Preise auf Anfrage
RANS S-10 SAKOTA
Specifications,
Performance, Standard Features
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SPECIFICATIONS |
65 HP |
80
HP/100 HP |
| Wing
Span |
24.0 ft |
24.0 ft |
| Area |
95.0 sq
ft. |
95.0 sq
ft |
| Mean
Chord |
4 ft 2
in |
4 ft 2
in |
| Aspect. |
4.23:1 |
4.23:1 |
| Length. |
17 ft 10
in |
17 ft 10
in |
| Height |
4 ft 10
in |
4 ft 10
in |
| Cockpit
Width |
35 in. |
35 in.
|
| Headroom |
38 in |
38 in |
| Legroom |
42 in |
42 in |
| Number
of Seats. |
2 |
2 |
| Doors |
2 |
2 |
| Landing
Gear* |
F/TD |
F/TD |
| Baggage
Volume |
8 cu ft |
8 cu ft |
| Baggage
Capacity. |
30 lbs |
30 lbs |
|
Auxiliary Baggage Volume |
n/a. |
n/a |
|
Auxiliary Baggage Capacity |
n/a. |
n/a |
| Fuel
Capacity |
18 gal
US |
18 gal
US |
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| POWER
PLANT |
582 |
912/912S |
| Engine. |
Rotax
582. |
Rotax
912/Rotax 912S |
| Output. |
65 hp. |
80
hp/100 hp |
| Oil
Capacity. |
2.5 qts. |
3.0 qts |
| Coolant
Capacity. |
4.4 qts. |
4.4 qts |
|
Propeller Diameter |
68 in to
70 in. |
68 in to
70 in |
|
Propeller Type. |
Wood |
Wood |
| Gear
Reduction. |
1:2.58 |
1:2.27/1:2.43 |
| Fuel
G.P.H. |
5.75 gal
@ 85% |
4.1/4.5
gal @ 80% |
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PERFORMANCE |
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| Take Off
Roll. |
300 ft. |
325
ft/310 ft |
| Rate of
Climb |
800 fpm. |
900
fpm/1200 fpm |
| Service
Ceiling |
12,500
ft |
14,000
ft/14,500 ft |
| Cruise |
110 mph |
120
mph/125 mph |
| VNE. |
130 mph |
130 mph |
| Stall
Clean. |
45 mph |
48 mph |
| Stall
Flaps. |
41 mph |
44 mph |
| Roll
Rate. |
100°
/sec |
100°
/sec |
| Glide
Ratio |
7:1 |
7:1 |
| Landing
Roll |
400 ft. |
400 ft |
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Endurance. |
3.1 hrs. |
4.4 hrs/4
hrs |
| Range. |
341
miles |
528/520
miles |
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WEIGHTS AND LOADINGS |
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| Gross
Weight |
960 lbs |
1010 lbs |
| Empty
Weight |
460 lbs |
510 lbs |
| Useful
Load. |
500 lbs |
500 lbs |
| Wing
Loading |
10.1
lbs. |
10.6 lbs |
| Power
Loading |
14.7
lbs. |
12.6 lbs |
| Limit
Load Factors** |
+4 -2 |
+4 -2 |
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* F/TD = Fixed Taildragger
**+6-3 at or below 800 gross weight |
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RANS S-10 SAKOTA
Standard Equipment and Features
ROTAX 582 65 HP liquid cooled with dual
CDI ignition; RPM gauge; 2-Blade wood prop; 4130 Welded steel fuselage,
tail group and tapered steel landing gear; Aluminum wheels with aircraft
tires; Wheel pants; Pre-formed trussed wing ribs; .020 Aluminum leading
edge wrap; 3" Tubular Aluminum Main spars; 2" Tubular Aluminum Aft spars;
(2) 9 Gallon wing tanks; Seat adjustable in tilt and fore and aft; 2.7
ounce aircraft covering fabric, all tapes, glue, and inspection plates;
Aluminum framed canopy; Airfoil struts; In-flight pitch trim; In-flight
start; "Deep Set" panel; Roll over protection; Shoulder harnesses and
lap belts; Dual elevator horns; 1 1/4" Push-pull elevator tube; Cable
operated rudder; 2-Position flaps; Differential ailerons are cable and
push-pull tube operated; Center control sticks and throttles; Pilot side
flap lever; Pre-molded cowling; 12" Composite spinner; 4130 welded steel
heavy duty engine mount with 4 point isolation; Under the wing lever;
Dual fuselage foot pegs and wing steps; Dual wire braced folding tail;
Steerable tail wheel; Dual rudder pedals; Hydraulic brakes; Firewall
sound proofing; Baggage compartment.
The S-10 Sakota is an FAA Approved 51%
Kit - No welding required.
Build Time: 350 to 600 hours
Kits delivered as of 11/05:
198
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