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Landing Gear Configuration: |
Taildragger |
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Landing Gear Type: |
Oleo Strut or Spring Aluminum Gear |
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Engine Type: |
Lycoming |
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Engine Model: |
IO-540-W1A5 |
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Propeller: |
81 McCauley Constant Speed Prop - 2 blade |
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No. of Seats: |
Five |
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Useful Load: (avg.) |
895 lbs. (235B) 847 lbs. (235C) |
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Cruising Speed: (75% power at optimum altitude): |
160 mph |
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Wing Span: |
32.9 feet |
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Wing Area: |
165.6 sq. feet. |
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Length: |
23.5 feet |
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Height: |
8.3 feet |
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Cabin Width: |
42 inches |
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Gross Weight: |
2500 lbs. |
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Empty Weight: |
1605 lbs. (235B) 1653 lbs. (235C) |
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Fuel Capacity: |
73 gal. |
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Stall speed (with full flaps, 1 pilot, 1/2 tank of fuel) |
40 mph |
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Takeoff distance: (1 pilot, 1/2 tank of fuel) |
250 feet |
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Takeoff distance at gross over 50 high obstacle: |
600 feet |
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Rate of Climb: (1 pilot, 1/2 tank of fuel) |
1500 fpm |
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Land at gross over 50 obstacle: |
500 feet |
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Best Climb Speed: |
90 mph |
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Service Ceiling: |
20,000 feet |
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Fuel Consumption (65% power): |
12 gph (B4B5) 11 gph (W1A5) |
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Flap Settings: |
-7, 0, 24, 40, 48 (degrees) |