Tecnam P2010 - Page 496

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV 7-16
Ed. 1Rev 0
Section 7 – Airframe and Systems description -
POWERPLANT
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 cyl-
inder horizontally opposed, air cooled
with down exhaust outlets.
Maximum power………………… 134.0 kW (180hp) @ 2700 rpm
Maximum continuous power …………... 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 …………………………………. MTV-15-B/193-52
Type Certificate ……………………….. EASA TCDS no. P.098
Blades/hub …………………………….. wood/composite 2-blades – aluminium hub
Diameter ………………………………. 1930 mm (6,33 ft) no reduction allowed
Type …………………………………… Variable pitch
Governor
Manufacturer ………………………….. MT Propeller
Model …………………………………. P-860-23:
Type……………………………………. Hydraulic