INSTALLATION MANUAL
AIRCRAFT ENGINES
page 19 - 2
Initial issue, May 01/99
Effectivity: 447 UL SCDI, 503 UL DCDI, 582 UL DCDI /mod. 99
d00329
dia. 8,2
M 8
+0,15
dia. 6,5
+0,15
P.C.D.=100
P.C.D.=75
dia. 114
12
dia. 25,4 -0,1
fig. 48
02841
19.1.2.) “C” (CL) - and “E” (EL) type gearbox
Reduction ratio: 2,62 / 3,0 / 3,47 / 4,0
Attachment holes of propeller flange