2.3
Equipment Connection at the Wing Top and Rear
2.3.1
Remove the padding from the aileron control rod Figure 3 [12]. Connect the aileron control rod
Figure 3 [12] to the bell crank Figure 3 [15] and install the bolt Figure 3 [11], washer Figure 3 [14] and
nut Figure 3 [13].
2.3.2
2.3.3
Connect the bonding cable Figure 3 [18] to the earth stud Figure 3 [17] (GS600) and install the washer
Figure 3 [19] and the nut Figure 3 [20].
2.3.4
Remove the caps and connect the wing electrical connectors Figure 3 [1], Figure 3 [2], Figure 3 [3]
and Figure 3 [4] to the fuselage electrical connectors.
2.3.5
Connect the right inboard flap drive shaft, refer to AMM 12-B-27-50-02-00A-920A-A.
2.3.6
Attach the pitot pipe Figure 3 [10] to the support angle Figure 3 [5] with the Cable tie (Pt.No. P09-008)
Figure 3 [6].
2.3.7
Connect the emergency landing gear release cable to the right main gear actuator, refer to AMM 12-B-
32-30-01-00A-920B-A.
PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719,
1721-1999
12-B-AM-00-00-00-I
UNCLASSIFIED
Effectivity: All
12-B-57-00-00-00B-720B-A
UNCLASSIFIED
2021-12-04 Page 11