ALPHA Trainer
www.pipistrel-aircraft.com
REV. 0
POH-162-00-40-050
Performance - specifications
ALPHA Trainer
80 hp Rotax 912
Stall speed (flaps extended)
37 kts (68 km/h)
Stall speed (flaps retracted)
43 kts (80 km/h)
Cruise speed (5300 RPM)
108 kts (201 km/h)
Maximum horizontal speed at sea level
120 kts (222 km/h)
VNE
135 kts (250 km/h)
Standard endurance 108 knots cruise
3.0 hours + 30 min reserve
Standard range at 108 knots cruise
324 NM (600 km)
Fuel flow at 108 knots cruise speed (typical)
3.6 gph (13.6 L/h )
Best speed for maximum endurance
90 knots 4900-5000 rpm
Maximum endurance at 90 knots
3.6 hours + 30 min reserve
Takeoff - ground roll - at MTOM
555 ft (170 m)
Takeoff total distance over 50 ft obst. at MTOM
870 ft (265 m)
Landing distance over 50 ft obst.
1510 ft (460 m)
Absolute ceiling at MTOM
18,000 ft (5500 m)
NOTE
The above performance figures are based on an airplane weight at 1212 lbs (550 kg), stan-
dard atmospheric conditions, level hard-surfaced dry runways and no wind. They are calculated val-
ues derived from flight tests conducted by Pipistrel, under the supervision of the Slovenian CAA and
under carefully documented conditions. Figures may vary based on numerous factors (surface condi-
tion, temperature, water on wing, etc).
ALPHA Trainer
80 hp Rotax 912
Maximum weight takeoff
1212 lbs (550 kg)
Maximum weight landing
1212 lbs (550 kg)
Standard empty weight
615 lbs (279 kg)
Payload without fuel
597 lbs (271 kg)
Payload with full fuel
518 lbs (235 kg)
Baggage allowance aft of the cabin*
22 lbs (10 kg)
Fuel capacity, total
13.2 US gal (50 L)
Fuel capacity, usable
12.7 US gal (48 L)
Fuel weight full
79.4 lbs (36 kg)
Oil system capacity
3.5 Liters
Engine
Rotax 912 80 hp
Propeller
Pipistrel FP02-80, dia. 65’’
1660 mm
*
WARNING!
only when baggage net or solid baggage compartment is installed ( p/n 6023077).
CG limits must be always respected!
Noise levels
According to independent testing performed by German LBA-LTF noise regulations the airplanes, the
equivalent exhibited noise measures 55.8 dBa. Noise is measured on the ground when the airplane
overflies at 500 ft at full power, at speed of best climb. Measures have been taken to make the cockpit
exceptionally quiet on the inside as well.
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Summary of Contents for 890 AT 912 LSA
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