Rotax 914 F - 8.5 Engine; Components

Reference
Modification-No.
- 0 -
Page
27
Date
1996 05 10
Install
914 F
Propeller axis:
➪ The centres of attachment points L1 und R1 must be on an axis y2 parallel to y-
axis.
Tolerated roll deviation of parallelism:..........................± 5°. (see ill. 12)
Vertical axis:
➪ y-axis must be square to the longitudinal axis of the aircraft.
Yaw tolerance: ± 10° (see ill. 13)
+z
-y
+y
P
-z
L1R1
y2
5°
5°
-x
+x
-y
+y
P
10°
10°
Ill. 12
Ill. 13