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) - 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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