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25 Apr 2012 Ladies and gentlemen, we proudly present.... the PANTHERA! The revolutionary 4-seat all composite design, featuring retractable undercarriage, 200 kts cruising speed, 1000 NM range, comfortable cabin and a choice of three powerplants – conventional/hybrid/electric - is presented to the World for the very first time. Read more...
24 Apr 2012 The ALPHA Trainer is flying! We have successfully concluded the test flights program and we are proud to announce the release of our new aircraft - the ALPHA Trainer! Read more...
20 Apr 2012 Panthera is the Aircraft of the year 2012, Virus SW also nominated! The 4-seat Pipistrel Panthera won the Fliegermagazin award for the best aircraft of the year! Read more...
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Panthera

 

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)

>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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