DOCUMENT No.:
REVISION: 1.2
DATE: 2014/11/10
DC-MAM-001-X-C-2
Page 79
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.
Tighten the lock-nut on the bolt through the inboard aileron hinge sufficiently, observe
the correct placement of washers (refer to Figure 9) and note that the bolt is installed
with its head facing the wingtip.
Figure 9: Aileron hinge (inboard).
A
AN4-6A bolt
B
AN4 washer
(0.8 mm / 0.032”)
C
AN4 lock-nut (low profile) (Nyloc)
Refer to paragraph 16 for hardware
designations
B
B
AIRCRAFT SIDE
AILERON SIDE
WINGTIP
A
B
B
C
WINGTIP
Summary of Contents for Sling 4
Page 1: ......
