Tecnam P2010 - General Features

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V1-6
5. ENGINE
Manufacturer ……………………………
Lycoming
Engines
Model …………………………………...
IO
-360-M1A
Type Certificate ………………………...
EASA TCDS no. IM.E.032
Engine type ……………………………..
Fuel injected (IO), direct drive, four cylinder
horizontally opposed, air cooled with down
exhaust outlets.
Maximum power …….
Maximum continuous power …………...
134.0 kW (180hp) @ 2700 rpm
1
29.2 kW (173.3hp) @ 2600 rpm
6. PROPELLER
Manufacturer …………………………..
MT Propeller
Model ………………………………….
MT
V-15-B/193-52
Type Certificate ………………………..
EASA
TCDS no. P.098
Blades/hub ……………………………..
w
ood/composite 2-blades – aluminum hub
Diameter ……………………………….
1
930 mm (76 in) (no reduction is permitted)
Type ……………………………………
Variable
pitch
Governor
Manufacturer …………………………..
MT Propeller
Model ………………………………….
P
-860-23:
Type ………………………..
Hydraulic
Section 1 – General
GENERAL FEATURES
2
nd
Edition, Rev. 0