Sinus 
Virus 
Virus SW 
Taurus Electro 
Taurus 
Apis/Bee 
Panthera 
Spider 
Twister 
LN 
Bam 
Vario 
Technical sheet
|
|
Panthera |
Panthera Hybrid |
Panthera Electro |
|
Category |
Utility (+4.4 g) |
Utility (+4.4 g) |
Utility (+4.4 g) |
|
Powerplant |
Lycoming IO-390 |
Hybrid 145 kW |
Pure electric 145 kW |
|
Rated power |
210 HP |
195 HP (equivalent) |
195 HP (equivalent) |
|
Proportions |
|||
|
MTOM |
1200 kg / 2640 lbs |
1200 kg / 2640 lbs |
1200 kg / 2640 lbs |
|
Useful payload |
520 kg / 1145 lbs |
270 kg / 595 lbs |
200 kg / 440 lbs |
|
Full fuel payload |
345 kg / 760 lbs |
n/a |
n/a |
|
Wing span |
10.86 m / 35 ft 8 in |
10.86 m / 35 ft 8 in |
10.86 m / 35 ft 8 in |
|
Length |
8.07 m / 26 ft 6 in |
8.07 m / 26 ft 6 in |
8.07 m / 26 ft 6 in |
|
Height |
1.90 m / 6 ft 3 in |
1.90 m / 6 ft 3 in |
1.90 m / 6 ft 3 in |
|
Wing area |
10.9 m2/ 117 sqft |
10.9 m2/ 117 sqft |
10.9 m2/ 117 sqft |
|
Performance (MTOM) |
|||
|
Stall speed (flaps extended) |
109 km/h / 59 kts |
109 km/h / 59 kts |
109 km/h / 59 kts |
|
stall speed (flaps retracted) |
118 km/h / 64 kts |
118 km/h / 64 kts |
118 km/h / 64 kts |
|
manoeuvring velocity Va |
248 km/h / 134 kts |
248 km/h / 134 kts |
248 km/h / 134 kts |
|
Turbulence penetration Vb |
324 km/h / 175 kts |
324 km/h / 175 kts |
324 km/h / 175 kts |
|
VNE |
407 km/h / 220 kts |
407 km/h / 220 kts |
407 km/h / 220 kts |
|
Typical cruise speed (TAS) |
374 km/h / 202 kts
|
263 km/h / 142 kts |
218 km/h / 118 kts |
|
Climb rate at MTOW |
6.1 m/s / 1200 fpm |
5.7 m/s / 1140 fpm |
5.7 m/s / 1140 fpm |
|
Takeoff run |
365 m / 1200 ft |
385 m / 1265 ft |
385 m / 1265 ft |
|
Takeoff distance (50 ft obst.) |
670 m / 2200 ft |
700 m / 2300 ft |
700 m / 2300 ft |
|
Landing distance (50 ft obst.) |
570 m / 1900 ft |
570 m / 1900 ft |
570 m / 1900 ft |
|
Range at cruise speed, 4 people aboard (incl. 45 min reserve) - normal category |
>1900 km / >1025 NM |
1220 km / 660 NM |
400 km / 215 NM |
|
Service ceiling |
6,100 m/ FL 200 |
4000 m / FL 130 |
4000 m / FL 130 |
Pipistrel reserves the right to revise the above data whenever occasioned by product improvement, government/authority regulations or other good cause. All speeds are quoted as IAS unless noted otherwise. Take-off and landing data valid for ISA sea level conditions. Typical fuel flow for Lycoming IO-390 in cruise is 37 liters per hour / 10 USgallons per hour.
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