Tecnam P2010 - Page 16

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Section 1 – General
GENERAL FEATURES
2
nd
Edition, Rev.0
TERMINOLOGYFLI
GHT CONTROL
SURFACES
TRAVEL
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
134.0 kW (180 hp) @ 2700 rpm
6. PROPELLER
Manufacturer …………………………..
MT Propeller
Model ………………………………….
MT 188 R 145 – 4G
Type Certificate ………………………..
EASA TCDS no. P.006
Blades/hub ……………………………..
2 wood/composite blades – aluminium hub
Diameter ……………………………….
1880 mm (74 in) (no reduction allowed)
Type ……………………………………
Fixed pitch