ELA 10-Eclipse PILOT OPERATOR´S
HANDBOOK
Version: V10-05
Issue date: 26
th
July 2016.
Last modification: 04
th
February 2019.
16
2.4 TECHNICAL DATA AND PERFORMANCE
The following performance parameters were determined by flight testing
with average piloting skills, aircraft in good conditions and clean rotor
blades and propeller. The parameters apply to standard conditions ISA
(15ºC temperature, sea level and standard pressure).
Gyroplane data
With Rotax 912 ULS (100 HP)
With Rotax 914 TURBO (115
HP)
METRIC
IMPERIAL
METRIC
IMPERIAL
Empty weight (minimum equipment)
283 kg
625 lb
293 kg
650 lb
MTOW*
500 kg
1100 lb
530 kg
1170 lb
Useful load (minimum equipment)*
217 kg
475 lb
237 kg
520 lb
Vne
190 kph
120 mph
(103 kts)
190 kph
120 mph
(103 kts)
Cruise speed
120 – 160 kph
75 – 100 mph
(65 – 85 kts)
120 – 160 kph
75 – 100 mph
(65 – 85 kts)
Min speed (level flight/full power))
45 kph
30 mph
(24 kts)
40 kph
25 mph
(22 kts)
Rate of climb
3 m/s
600 ft/m
5 m/s
1000 ft/m
Take-off distance (roll)
120 m
400 ft
100 m
330 ft
Landing distance (roll)
0 – 30 m
0 – 65 ft
0 – 30 m
0 – 65 ft
Fuel
Gasoline
Fuel capacity
87 l
23 gal
Unusable fuel
2 l
0.5 gal
Fuel consumption
12 – 20 l/h
3 – 5.5 gal/hr
* See the MTOW limitations for your country.
