Section 7 – Airframe and Systems description
POWERPLANT
3.1. ENGINE FEATURES
EASA TCDS no. E.121 dated 1st April 2008
4 cylinders horizontally opposed with 1352 c.c. of overall
displacement, liquid cooled cylinder heads, ram-air
cooled cylinders, two carburetors, integrated reduction
gear box with shock absorber.
Maximum power
(at declared rpm)
73.5 kW (98.6hp) @ 5800 rpm –5 min. maximum
69.0 kW (92.5hp) @ 5500 rpm (continuous)
3.2. PROPELLER FEATURES
LBA 32.130/086 (MTV-21 series)
2 wood/composite blades, aluminium hub
1780 mm (no reduction allowed)
Variable pitch hydraulically controlled
3.3. PROPELLER GOVERNOR FEATURES
To Next Page
Loading...
