|
|
|

Diamond DA20-C1
Evolution/Eclipse performance and specifications

Powerplant: Teledyne Continental IO240B3B,
four-cylinder, horizontally opposed, fuel injected
125 hp
|
Length |
23 ft 6 in |
|
Height |
7 ft 2 in |
|
Wingspan |
35 ft 8 in |
|
Wing Area |
125 sq ft |
|
Seats |
2 |
|
Empty weight,
typical |
1,166 lb |
|
Maximum gross
weight |
1,720 lb |
|
Useable fuel |
24 US gal |
| |
|
|
Performance |
|
|
Takeoff
distance, ground roll |
1,106 ft |
|
Takeoff distance
over 50-ft obstacle |
1,470 ft |
|
Max demonstrated
crosswind component |
20 kt |
|
Rate of climb,
sea level |
1,000 fpm |
|
Cruise speed @
75% power |
135 ktas |
|
Landing distance
over 50-ft obstacle |
1,280 ft |
|
Landing
distance, ground roll |
581 ft |
| |
|
|
Limiting and
Recommended Airspeeds |
|
|
Vx (best angle
of climb) |
60 kias |
|
Vy (best rate of
climb) |
75 kias |
|
Vso (stall, in
landing configuration) |
44 kcas |
|
Vne (never
exceed) |
164
kias |
|
|