Tecnam P2010 2015 - 9. Recovery from Unintentional Spin; 10. Other Emergencies

AFMS N·Do7 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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5.ENGINE
Manufacturer ..... .. ....... .. .... ....... .... Lycoming Engines
Model ............ .... .. .. .... ... .... . ... .... .. .10-360-MIA
Type Certificate ...................... ... .... EASA TCDS no. IM.E.032
Engine type
Fuel injected (10), 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 (I 73 . 3hp)@2600 rpm
6. PROPELLER
Manufacturer ...... ...... .. ... ... .... ... .. .. MT Propeller
Model ............ .. .. .. ............ .. .... .... MTV-15-8/193-52
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
Section 1 - General
Ed. 2, R ev. O
GENERAL FEATURES