ALPHA Electro
www.pipistrel-aircraft.com
REV. 0
POH-167-00-40-150
5-4
Performance
Takeoff performance
All data published in this section was obtained under the following conditions:
Aircraft at MTOM
Elevation: sea level
Wind: calm
Runway: grass runway
Data extrapolated for ICAO standard atmosphere
ALPHA Electro ALPHA Electro
Takeoff ground roll at MTOM 595 ft (181 m)
Takeoff runway length (over 50 ft/15 m obstacle) 930 ft (285 m)
NOTE In order to meet the data for takeoff runway length over 50 ft obstacle maintain V
x
(55
kts, 102 km/h) after take off.
The runway length required for takeoff may vary depending on the wind, temperature, ele-
vation and wing & propeller surface condition.
Effect of elevation
The table below provides data about the effect of elevation on takeoff runway length.
Elevation (m) 0 500 1000 1500
Elevation (ft) 0 1640 3280 4921
Atmosph. pressure (inHg) 29.92 28.17 26.52 24.95
Atmosph. pressure (hPa) 1013 954 898 845
Outside temperature (°C) 15,0 11,7 8,5 5,2
Outside temperature (°F) 59 53 47 41
Takeoff ground roll [ft] ([m])
ALPHA Electro 595 (181) 750 (228) 930 (285) 1165 (355)
Takeoff distance over 50 ft / 15 m obstacle [ft] ([m])
ALPHA Electro 930 (285) 1100 (338) 1385 (422) 1520 (465)
WARNING! The runway length required for takeoff is affected by several factors like eleva-
tion, OAT, runway conditions.
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