DOCUMENT No.:
REVISION: 1.2
DATE: 2014/11/10
DC-MAM-001-X-C-2
Page 121
D
B
C
A
E
C
PROCEDURE (INSTALLATION)
1.
Reverse the above procedure (removal), paying close attention to the following:
Inspect all bolts, nuts and screws for damage. Replace if necessary.
Do not reuse lock-nuts. Fit new.
The signal cable connector must be secured to the servo motor before
installing the motor, otherwise there may not be enough space to insert and
manipulate a tool to tighten the connector securing screws.
If applicable secure the servo cable to the aircraft frame with tie wraps, in the
manner it was before removal, using spacers as applicable.
Apply thread locking sealant to the servo mounting screws before fitment. Do
not over tighten.
Observe the correct placement of washers (refer to Figure 28).
Figure 28: Autopilot elevator servo installation.
Paint orange creep marks on the bolts / lock-nuts.
2.
Inspect for security of attachment. Ensure servo signal cable will not chafe against the
aircraft frame.
A
AN3-10A bolt
B
AN4 washer (thick)(1.6 mm)
C
AN3 washer (thick)(1.6 mm)
D
AN3 washer (thin)(0.8 mm)
E
AN3 lock-nut (Nyloc)
Refer to paragraph 16 for hardware
designations
Summary of Contents for Sling 4
Page 1: ......
