Rotax 447 UL SCDI - 7.3 Engine Type Designation

Effectivity: 447 UL SCDI, 503 UL DCDI, 582 UL DCDI /mod. 99
INSTALLATION MANUAL
AIRCRAFT ENGINES
page 9 - 1
Initial issue, May 01/99
d00319
9) Engine suspension and position
■ ATTENTION: At installation of engine be aware of engine weight and assure careful
handling.
The engine suspension is determined essentially by the aircraft design. Four attachment
points are provided on the engine.
▲ WARNING: All four attachments points must be utilized.
9.1) Definition of attachment points
9.1.1) 503 UL DCDI, 582 UL DCDI and 582 UL DCDI mod. 99
153 mm
94 mm
9.1.2) 447 UL SCDI
145 mm
94 mm
fig. 5
02865
fig. 6
02862
02863
02864