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Diamond Katana 100
performance and specifications
Powerplant
Bombardier Rotax 912S, 100 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 |
13.2 lb/sq ft |
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Power loading |
16.5 lb/hp |
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Seats |
2 |
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Empty Weight,
typical |
1,095 lb |
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Maximum gross
weight |
1,653 lb |
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Fuel capacity,
std |
20.1 gal (19.5 gal useable) |
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Oil capacity |
3.2 qt |
Performance |
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Take off
distance, ground roll |
1,025 ft |
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Takeoff
distance over 50-ft obstacle |
1,425 ft |
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Max
demonstrated crosswind component |
15 kt |
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Rate of climb,
sea level |
700 fpm |
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Cruise/fuel
consumption 7,500 feet @ 75% power |
123 ktas/6.1 gph |
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Service ceiling |
17,600 ft |
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Landing
distance, over 50 ft. obstacle |
1,532 ft |
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Landing
distance, ground roll |
790 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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