Tecnam P2010 - Power Plant

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V7-16
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
129.2 kW (173.3hp) @ 2600 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
V-15-B/193-52
Type Certificate ………………………..
EASA
TCDS no. P.098
Blades/hub ……………………………..
w
ood/composite 2-blades – aluminium hub
Diameter ……………………………….
1
930 mm (6,33 ft) no reduction allowed
Type ……………………………………
Variable
pitch
Governor
Manufacturer …………………………..
MT Propeller
Model ………………………………….
P
-860-23:
Type
Hydraulic
Section 9 – Supplements
POWERPLANT
2
nd
Edition, Rev. 0