Technical Data And Performances - ELA Aviacion ELA 07 Operator's Handbook Manual

2.4 TECHNICAL DATA AND PERFORMANCES

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
Empty weight (standard equipment)
MTOW
Useful load
Vne
Cruise speed
Min speed (level flight/full power))
Rate of climb
Take-off distance
Landing distance
Fuel
Fuel capacity
Unusable fuel
Fuel consumption
2.5 ENGINE
- Manufacturer .......................................................................................... Rotax
- Take-off power:
912 ULS..................................................................................... 100 hp
o
914 UL...................................................................................... 115 hp
o
- Max. engine speed....................................................................... 5800 rpm
ELA 07-07S PILOT OPERATOR´S HANDBOOK
Version: V07-04
With Rotax 912 ULS (100 HP)
60 – 85 mph
258 kg
450 kg
192 kg
100 mph
25 mph
650 ft/min
100 m
0 – 30 m
Gasoline
75 l
3 l
15 – 20 l/h
16
With Rotax 914 TURBO (115
HP)
264 kg
450 kg
186 kg
100 mph
60 – 90 mph
20 mph
1000 ft/min
70 m
0 – 30 m