Tecnam P2010 - Page 404

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV1-6
Section 1 – General-
GENERAL FEATURES
Ed. 1, Rev.0
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 134.0 kW (180hp) @ 2700 rpm
Maximum continuous power …………...129.2 kW (173.3hp) @ 2600 rpm
6. PROPELLER
Manufacturer ………………………….MT Propeller
Model ………………………………….MTV-15-B/193-52
Type Certificate ……………………….EASA TCDS no. P.098
Blades/hub …………………………….wood/composite 2-blades – aluminum hub
Diameter ………………………………1930 mm (76 in) (no reduction is permitted)
Type ………………………………… Variable pitch
GOVERNOR
Manufacturer ……………………… MT Propeller
Model ……………………………… P-860-23:
Type ……………………….. Hydraulic