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Diamond Katana DA20-A1 performance and specifications
Powerplant: Bombardier Rotax 912F3, 81
hp, four-cylinder, horizontally opposed
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Recommended TBO |
1,200 hr |
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Length |
23 ft 6 in |
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Height |
6 ft 11 in |
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Wing span |
35 ft 7 in |
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Wing area |
125 sq ft |
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Wing loading |
12.9lb/sq ft |
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Power loading |
19.7lb/hp |
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Seats |
2 |
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Empty Weight, typical |
1,095 lb |
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Maximum gross weight |
1,609 lb |
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Fuel capacity, std |
20.1 gal (19.5 gal useable) |
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Oil capacity |
3.2 qt |
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Performance |
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Take off distance, ground roll |
1,120 ft |
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Takeoff distance over 50-ft obstacle |
1,560 ft |
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Max demonstrated
crosswind component |
15 kt |
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Rate of climb, sea level |
680 fpm |
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Cruise/fuel
consumption 7,500 feet @ 75% power |
117 kt/4.3 gph |
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Service ceiling |
14,000 ft |
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Landing distance, over 50 ft. obstacle |
1,490 ft |
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Landing distance, ground roll |
748 ft |
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Limiting and Recommended Airspeeds |
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Vx (best angle
of climb) |
57 kias |
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Vy (best rate of
climb) |
65 kias |
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Va (design
maneuvering) |
104 kias |
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Vfe (max flap
extended) |
81 kias |
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Vno (max
structural cruising) |
118 kias |
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Vne (never
exceed) |
161 kias |
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Vs (stall,
clean) |
41 kias |
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Vs0 (stall, in
landing configuration) |
37 kias |
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