Tecnam P-Mentor - Page 22

1
st
Edition - Rev. 0
Section 1 – GENERAL
GENERAL FEATURES
P-Mentor – Aircraft Flight Manual Page 1 - 6
4. Engine
Manufacturer .…………………….……….... Bombardier- Rotax GmbH
Model ……….………………………....……. 912 iSc 3 Sport
Type Certificate .…………………....…….... EASA.E.121
Engine type .…...………….…………………
4 cylinder horizontally-opposed twins
with overall displacement of 1352
c.c., mixed cooling, (water-cooled
heads and air-
cooled cylinders),
electronic injection, integrated
reduction gear with torque damper.
Max. take-off power (max. 5 min) ……….. 73.5 kW / 100 hp @ 5800 rpm
Max. continuous power …………………… 72.0 kW / 98 hp @ 5500 rpm
5. Propeller
Manufacturer.…………………….… MT Propeller
Model……….………………………. MTV-21-A/180-51
Type Certificate.………………….... EASA.P.101
Blades.…...………………………….
2 laminated wood composite
Diameter……….……………...……. 1800mm / 5 ft 10.9 in
Type…………………………...…….
Variable pitch propeller at constant
speed
6. Governor
Manufacturer.…………………….… MT Propeller
Model……….………………………. MTV P-850-12
Type…………………………...……. Standard hydraulic constant speed