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±³À°
±âÁ¾ : STOL CH 701
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SPECIFICATIONS
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WING SPAN
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27 feet |
8.2 m.
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WING AREA |
122 sq.ft.
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11.4 m.sq
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LENGTH
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50 ft.11 in.
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6.38 m.
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HEIGHT(rudder
tip)
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8ft.7 in.
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2.6 m.
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EMPTY WEIGHT*
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580 lbs.
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263 kg
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GROSS WEIGHT
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1,100 lbs.
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500kg
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USEFUL LOAD
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520 lbs.
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236kg
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WING LOADING
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9.0 lbs/ft
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43.8 m.
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POWER LOADING
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13.75 lbs
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6.25 kg/bhp
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DESIGN LOAD FACTOR
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+6G/-3G
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CABIN
WIDTH |
41
inches |
104 cm
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FUEL CAPACITY(std)
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20
us gallons
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76
liters
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 | ±³À° ±âÁ¾ : AVID MARK IV | ||
| - | STOL | SPEEDWING | |
| WING SPAN | 29 ft. 10.5 in. | 23 ft. 11.5 in. | |
| WING AREA | 122.46 sq. ft. | 97.31 sq. ft | |
| WING CHORD | 42 in. | 42 in. | |
| ASPECT RATIO | 7.1 | 5.65 | |
| LENGTH | 17 ft. 11 in. | 17 ft. 11 in. | |
| HEIGHT | 71 in. | 71 in. | |
| GROSS WEIGHT | 1,150 lbs. | 1,050 lbs | |
| USEFUL LOAD | 540+ lbs. | 540+ lbs | |
| FUEL CAPACITY | 14 gal. | opt. 18 gal. | |
| CRUISE SPEED | 90 mph. | 115 mph. | |
| STALL SPEED | 32 mph./ solo | 42 mph./ solo | |
| LANDING DISTANCE | 150ft. / solo | 500 ft. / solo | |