Tecnam P2010 - Page 146

Page 7 - 16
Section 7 – Airframe and Systems description
POWERPLANT
2
nd
Edition, Rev. 0
7. POWERPLANT
7.1. ENGINE
Manufacturer ……………………………
Lycoming Textron
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
134.0 kW (180hp) @ 2700 rpm
Oil Consumption
Operation
RPM
HP
Max.
Oil Cons.
Qts./Hr.
*Max.
Cyl. Head
Temp.
Normal Rated
2700
180
.80
500°F (260°C)
Performance Cruise (75%)
2450
135
.45
500°F (260°C)
Economy Cruise (60R Rated)
2350
117
.39
500°F (260°C)
7.2. 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 (6,17 ft) no reduction allowed
Type ……………………………………
Fixed pitch