Rotax 447 UL SCDI, Installation Manual

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Effectivity: 447 UL SCDI, 503 UL DCDI, 582 UL DCDI /mod. 99
INSTALLATION MANUAL
AIRCRAFT ENGINES
page 7 - 1
Initial issue, May 01/99
d00317
7) Technical data
For technical data and limits of operation refer to the latest revision of the current Operator’s
Manual 447 UL SCDI- 503 UL DCDI- 582 UL DCDI Model 99.
◆
NOTE: Connecting dimensions, filling capacities, drive and reduction ratios, elec-
tric output etc. can be found in the respective chapter of engine installation.
Joint face
gearbox-engine
D
X2
X2
X2
X2
Z2
Z2
Z3 Z1
Z1
Z3
A
B
C
X1 X1
X3cy X3cy
X3ba
X3ba
G
E
F
C
C
C Engine
Y2
Y2
Y2
Y2
Y3cy
Y3ba
Y3ba
Y1
Y1
Y3cy
C.O.G Reduction gear
with propshaft towards cyl.
Prop shaft
torwards cyl.
Prop shaft
torwards base
C.O.G Engine
C.O.G Powerplant
with propshaft towards cyl.
C.O.G Powerplant
with propshaft towards base
C.O.G Reduction gear
with propshaft towards base
fig. 4
02794
02851
Total dimension
447 UL SCDI 503 UL DCDI 582 UL DCDI / mod. 99
max. dimension x axis 543 556 582
max dimension y axis 523 513 437
max dimension z axis 416 374 387
7.1) Installation dimensions (all dimensions in mm)