ELA Aviacion ELA 07, Pilot Operator'S Handbook

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