INSTALLATION MANUAL
AIRCRAFT ENGINES
page 14 - 2
Initial issue, May 01/99
Effectivity: 447 UL SCDI, 503 UL DCDI, 582 UL DCDI /mod. 99
d00324
■ ATTENTION: At trial run, check tightness without fail!
- The propeller flange (5) is furnished with 6 tappings M6 and 6 holes each of 6,5
mm and 8,2 mm dia., but screws are not in the supply scope.
■ ATTENTION: With use of ROTAX gear box type “C” (CL) or “E” (EL) the
moment of inertia of the propeller must not be in excess of 6000
kgcm² (“B” type gearbox: 3000 kgcm²). Enquire for moment
of inertia and have it confirmed by the manufacturer of propeller
in writing.
■ ATTENTION: Gearbox „B“ with reduction ratio i= 3,00 is only allowed to be
used only for engine versions up to 40 HP (= 29,4 kW).
SZ
SS
fig. 27
02812
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