Technical Data And Performance - ELA Aviacion ELA 07 Pilot Operator's Handbook

2.4 TECHNICAL DATA AND PERFORMANCE

The following performance parameters were determined by flight testing
with average piloting skills, aircraft with 450 kg MTOW, 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
Empty weight (minimum equipment)
MTOW*
Useful load (minimum equipment)
Vne
Cruise speed
Min speed (level flight/full power))
Rate of climb
Take-off distance (roll)
Landing distance
Fuel
Fuel capacity
Unusable fuel
Fuel consumption
* See the MTOW limitations for your country.
ELA 07-07S PILOT OPERATOR´S HANDBOOK
Version: V07-05
With Rotax 912 ULS (100 HP)
METRIC
260 kg
450 kg
190 kg
160 kph
100 – 135 kph
40 kph
3.3 m/s
100 m
0 – 30 m
13 – 20 l/h
Last modification: September 2017.
With Rotax 914 TURBO (115
IMPERIAL
575 lb
1000 lb
420 lb
100 mph
(85 kts)
60 – 85 mph
100 – 145 kph
(55 – 73 kts)
25 mph
(22 kts)
650 ft/min
330 ft
0 – 65 ft
Gasoline
75 l
3 l
16
HP)
METRIC IMPERIAL
265 kg 585 lb
500 kg 1100 lb
235 kg 520 lb
100 mph
160 kph
(85 kts)
60 – 90 mph
(55 – 78 kts)
22 mph
35 kph
(19 kts)
5 m/s 1000 ft/min
70 m 230 ft
0 – 30 m 0 – 65 ft
20 gal
0.8 gal
3.5 – 5.5 gal/hr