ultralights aircraft, ultralights market, sale planes, ultralight School, ultraligeros, escuela de pilotos, curso de piloto, piloto de ultraligeros
RANS Inc.

http://www.rans.com/

S-17 STINGER

s_17_stinger.jpg (37163 bytes)

 

 

 

SPECIFICATIONS

42 HP

47 HP

Wing Span

29.5 ft

29.5 ft

Area

127sq ft

127 sq ft

Mean Chord

4 ft 4 in

4 ft 4in

Aspect

7:1

7:1

Length

17 ft 4 in

17 ft 4 in

Height

84 in

84 in

Cockpit Width

N/A

N/A

Headroom

40 in

40 in

Legroom

41 in

41 in

Number of Seats

1

1

Landing Gear

F/TD

F/TD

Fuel Capacity

5 gal US

5 gal US

POWER PLANT

447

503

Engine

Rotax 447

Rotax 503

Output

42 hp

47 hp

Propeller Diameter

68 in

68 in

Propeller Type

IVO 3-Blade

IVO 3-Blade

Gear Reduction

1:2.58

1:2.58

Fuel G.P.H

3.75 gal @ 85%

4.0 gal @ 85%

PERFORMANCE

 

 

Take Off Roll

100 ft

80 ft

Rate of Climb

900 fpm

1100 fpm

Service Ceiling

12,500 ft

13,000 ft

Cruise

55 mph

60 mph

VNE

95 mph

95 mph

Stall

28 mph

28 mph

Roll Rate

70o / sec

70o / sec

Glide Ratio

6:1

6:1

Landing Roll

100 ft

100 ft

Endurance

1.3 hrs

1.0 hrs

Range

71 miles

60 miles

WEIGHTS AND LOADINGS

 

 

Gross Weight

527 lbs

536 lbs

Empty Weight*

252 lbs

261 lbs

Useful Load

275 lbs

275 lbs

Wing Loading

4.1 lbs

4.2 lbs

Power Loading

12.5 lbs

11.4 lbs

Limit Load Factors

+4-2

+4-2

* Empty Weight will increase with addition of 5" wheels, brakes, streamline struts, clear coat, and other equipment.