Definition Of Attachment Points - Rotax 914 F Installation Manual

10.1) Definition of attachment points

See Ill. 9/10.
Ill. 9
+z
R4
L4
P
+x
-z
L1
R1
attachment point
1 L 1R
thread size M 1 0
min. length of
25 mm (1")
thread engagement
WARNING: The engine suspension to be designed by the aircraft or fuselage
max. allowable forces (limit
load) in (N) in x, y and z axis
max. allowable bending moment
(limit load) in (Nm) in x, y
and z axis
WARNING: Tighten all engine suspension screws as specified by the aircraft
Modification-No.
- 0 -
40m
L3
L2
R2
4 L 4R
1mm
builder such that it will carry safely the maximum occurring opera-
tional loads without exceeding the max. allowable-forces and mo-
ments on the engine attachment points.
attachment point
1 L 1R
5 0 0 0
7 7
builder.
Reference
R3
-x
+y
1
attachment
point
40mm
max. allowable forces
4 L 4R
(limit load) in (N)
1 9 0 0
max. allowable bending moment
3 9
(limit load) in (Nm)
in x, y and z axis
+z
P
L3 R3
L2 R2
-z
A x e s
x axis y axis
L 1 - 2 0 0 , 8 - 7 1 , 0
R1 - 2 0 0 , 8 7 1 , 0
L 2 - 5 6 2 , 0 1 0 5 , 0
R2 - 5 6 2 , 0 - 1 0 5 , 0
L 3 - 5 6 2 , 0 1 0 5 , 0
R3 - 5 6 2 , 0 - 1 0 5 , 0
L 4 - 1 3 0 , 3 - 7 1 , 0
R4 - 1 3 0 , 3 7 1 , 0
attachment point
2 L
in x axis
in y axis
in z axis
Install Date
1996 05 10
914 F
Ill. 10
- y
z axis
- 2 1 1 , 0
- 2 1 1 , 0
- 2 7 7 , 0
- 2 7 7 , 0
- 7 , 0
- 7 , 0
0 , 0
0 , 0
2R 3 L 3R
5 000
2 000
3 000
1 0 0
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