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Pipistrel ALPHA Trainer User Manual

Pipistrel ALPHA Trainer
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ALPHA Trainer www.pipistrel-aircraft.com
REV. 0
POH-162-00-40-050
Powerplant, fuel, oil
Engine manufacturer: ROTAX
Engine type: Rotax 912 (80 HP)
The engine
TEMPERATURE °C / ROTAX ENGINE 912 80 HP
Maximum coolant temp. (CT) 120
Maximum exhaust gas temperature (EGT) 880
Oil temperature (OIL TEMP); minimum, normal, highest 50; 90-110; 140
RPM, PRESSURE
912 80 HP
Oil pressure (OIL PRESS); lowest, highest bar (psi) 0.8; 2.0-5.0; 7.0
Maximum continuous speed (RPM) 5500
Take-o speed; maximum allowable 5 min (RPM) 5800
Magneto check at (RPM) 4000
Maximum single magneto drop (RPM)
< 300
Fuel and oil
ROTAX ENGINE 912 80 HP
Recommended fuel **
minimum 90 RON
grade,
up to 10% alcohol
content permitted,
0% is preferable*
Also approved fuels **
leaded* or AVGAS
100 LL
Recommended oil **
SAE 10 W-40
AeroShell Oil Sport
Plus 4
Oil system capacity typical 3.5 L (check dipstick)
* Engine life is reduced. If using this type of fuel is unavoidable, changing the engine oil
every 50 flight hours is crucial. Please consult the manufacturer on which type of oil to use.
** See latest edition of Rotax Service Instruction SI-912-016R10 Selection of suitable operating
uids for Rotax Engine.
IMPORTANT!
Four-stroke engines should only be powered by unleaded fuel, for lead sedimentation inside the en-
gine shortens its life. Provided you are unable to use unleaded fuel, make sure engine oil and the oil
filter are replaced every 50 flight hours.
WARNING! Use of fuels with alcohol content exceeding 10% is not permitted. See Rotax
specification - please refer to SI-912-016 “Selection of suitable operating fluids“ latest issue.
NOTE Please refer to the applicable Rotax operators manual for additional engine operating limi-
rations.
1-4
General

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Pipistrel ALPHA Trainer Specifications

General IconGeneral
ManufacturerPipistrel
ModelALPHA Trainer
Aircraft TypeLight Sport Aircraft
Horsepower80 hp
Seating Capacity2
EngineRotax 912
Length6.5 m
Maximum Takeoff Weight550 kg
Cruise Speed108 knots
Range1000 km
PropellerFixed Pitch

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