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Tecnam P2002 JF - Page 650

Tecnam P2002 JF
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Page 5 2
nd
Edition Rev 0
51-00
STRUCTURE - GENERAL
ENGINE AND PROPELLER
Aircraft is powered by Rotax 912S2 engine featuring 4 cylinders horizontally opposed
with 1352 c.c. of overall displacement, liquid cooled cylinder heads, ram-air cooled
cylinders, carburetor, integrated reduction gear box with torsional shock absorber and
overload clutch.
Propellers are made by Hoffmann propeller. They are fitted with two wood/composite
blades and aluminum hub.
Figure 5. Engine mount and propeller

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