Tecnam P-Mentor - 3. Powerplant

1
st
Edition - Rev. 0
Section 2 – LIMITATIONS
POWERPLANT
P-Mentor – Aircraft Flight Manual Page 2 - 6
EASA Approved
3. Powerplant
3.1. Engine
Manufacturer ……………………………...
Bombardier - Rotax GmbH
Model Number ..………………………......
912 iSc 3 Sport
3.2. Propeller
Manufacturer ……..………………………………..
MT Propeller
Model Number …………………………………….
MTV-21-A/180-51
Number of Propeller ……………………………….
1
Number of Propeller Blades ……………………….
2
Propeller Diameter ………..……………………….
1800 mm (5 ft 10.9 in)
3.3. Powerplant Limitations
Following list reports the operating limitations for installed engines:
Power
 Max. take-off power (max. 5 min) ………..
73.5 kW / 100 hp @ 5800 rpm
 Max. continuous power ……………………
72.0 kW / 98 hp @ 5500 rpm
Oil pressure
 Minimum below 3500 RPM ………………..
 Minimum above 3500 RPM ..…..…………..
 Maximum normal ………………..………….
 Maximum for starting and warm-up ..……..
0.8 bar / 12 psi
2.0 bar / 29 psi
5.0 bar / 73 psi
7.0 bar / 102 psi