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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.

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