ALPHA Trainer-POH booklet.pdf - Pipistrel
ALPHA Trainer-POH booklet.pdf - Pipistrel
ALPHA Trainer-POH booklet.pdf - Pipistrel
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<strong>ALPHA</strong> <strong>Trainer</strong><br />
www.pipistrel.eu<br />
www.pipistrel.eu<br />
<strong>ALPHA</strong> <strong>Trainer</strong> i-2<br />
REV. 0<br />
REV. 0<br />
Performance - Specifications<br />
<strong>ALPHA</strong> <strong>Trainer</strong> 80 hp Rotax 912<br />
stall speed (flaps extended)<br />
34 kts (64 km/h)<br />
stall speed (flaps retracted)<br />
cruise speed (5300 RPM)<br />
maximum horizontal speed at sea level<br />
VNE<br />
usable fuel capacity 12.7 USgal, best endurance (with 30 min reserve)<br />
40 kts (74 km/h)<br />
108 kts (201 km/h)<br />
120 kts (222 km/h)<br />
135 kts (250 km/h)<br />
4.1 hours<br />
fuel flow at cruise speed 3.6 gph (13.6 l/h )<br />
range at cruise speed (excl. reserve)<br />
380 NM (702 km)<br />
takeoff - ground roll - at MTOM 555 ft (140 m)<br />
takeoff total distance over 50 ft obst. at MTOM 870 ft (225 m)<br />
landing distance over 50 ft obst. 1510 ft (460 m)<br />
absolute ceiling at MTOM 18,000 ft (5500 m)<br />
NOTE The above performance figures are based on airplane weight at 1040 lbs, standard atmospheric<br />
conditions, level hard-surfaced dry runways and no wind. They are calculated valued<br />
derived from flight test conducted by <strong>Pipistrel</strong> d.o.o. Ajdovščina, under supervision of CAA of<br />
Republic of Slovenia and under carefully documented conditions. Figures may vary based on<br />
numerous factors (surface condition, temperature, water on wing, etc).<br />
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<strong>ALPHA</strong> <strong>Trainer</strong> 80 hp Rotax 912<br />
maximum weight takeoff<br />
1040 lbs (472.5 kg)<br />
maximum weight landing<br />
standard empty weight<br />
1040 lbs (472.5 kg)<br />
605 lbs (275 kg)<br />
baggage allowance, maximum (baggage area floor limit) 55 lbs (25 kg)<br />
baggage allowance, typical with fuel fuel 22 lbs (10 kg)<br />
fuel capacity, total 13.2 USgal (50 l)<br />
fuel capacity, usable 12.7 USgal (48 l)<br />
oil capacity (oil bottle)<br />
engine<br />
propeller<br />
3 liters<br />
Rotax 912 80 hp<br />
fixed pitch* dia. 63’’<br />
1620 mm<br />
Noise levels<br />
According to independent testing performed by German LBA-LTF noise regulations the aeroplanes,<br />
the equivalent exhibited noise measures 55.8 dBa. Noise is measured on the ground when the aeroplane<br />
overflies at 500 ft at full power, at speed of best climb. Measures have been taken to make the<br />
cockpit exceptionally quiet on the inside as well.