ALPHA Electro
www.pipistrel-aircraft.com
REV.0
POH-167-00-40-150
REV
Performance - Specifications
ALPHA Electro 60 kW Electric
Stall speed (flaps extended +25
o
) 39 KIAS (72 km/h)
Stall speed (flaps retracted 0
o
) 44 KIAS (82 km/h)
Best endurance speed 85 KIAS (157 km/h)
VNE 135 KIAS (250 km/h)
Best endurance - not considering reserves * 60 min
Standard range at cruise 75 NM (139 km)
Takeoff - ground roll - at MTOM 595 ft (181 m)
Takeoff total distance over 50 ft obst. at MTOM 930 ft (285 m)
Landing distance over 50 ft obst. 1615 ft (492 m)
Absolute ceiling at MTOM 12,800 ft (3900 m)
* NOTE Legal flight time must be applied according to applicable local regulations!
NOTE The above performance figures are based on an airplane weight of 1256 lbs (570 kg),
standard atmospheric conditions, level hard-surfaced dry runways and no wind. They are cal-
culated values derived from flight tests conducted by Pipistrel, under the supervision of the
Slovenian CAA and under carefully documented conditions. Figures may vary based on numer-
ous factors (surface condition, temperature, water on wing, etc).
ALPHA Electro 60 kW Electric
Maximum weight takeoff 1256 lbs (570 kg)
Maximum weight landing 1256 lbs (570 kg)
Empty weight (incl. BPRS, no batteries, typical) 553 lbs (251 kg)
Battery capacity, total 21.0 kWh
Battery capacity, useful 20.0 kWh
Motor 60 kW E-Motor
Propeller
three blade, fixed pitch composite propeller,
diameter 64 9/16’’ (1640 mm)
This aircraft is compliant with ASTM F2245 (design and construction) and ASTM F3198 for continued airworthiness.
For a detailed compliance declaration please refer to the applicable LSA Compliance Statement as issued by the
manufacturer for this aircraft’s serial number.”
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