Tecnam P2010 - Page 510

AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGURATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 1-6
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 (180
hp) @ 2700 rpm
1
29.2 kW (173.3 hp) @ 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
Ed. 1, Rev. 0