DOCUMENT No.:
REVISION: 1.2
DATE: 2014/11/10
DC-MAM-001-X-C-2
Page 81
Tighten the lock-nut on the bolt through the aileron pushrod rod-end bearing sufficiently,
observe the correct placement of washers (refer to Figure 11) and note that the bolt is
installed with its head facing the wing upper surface.
Figure 11: Aileron pushrod -to-bellcranck connection.
2.
Ensure that with the control column vertical the aileron trailing edge is aligned with wing trailing
edge and that the aileron bellcrank is in the neutral position, i.e. the inside arm (the arm closest
to the cabin) is perpendicular with the spar axis.
3.
Verify for alignment and correct travel (refer to paragraph 1.13).
4.
Apply creep marks to the bolts / nuts with orange paint.
5.
Apply thread locking sealant and replace the inspection panel.
A
AN4 washer (1.6 mm / 0.0
63”)
B
AN4-11A bolt.
C
AN4 lock-nut (Nyloc)
Refer to paragraph 16 for hardware
designations
A
B
A
A
C
Summary of Contents for Sling 4
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