2.3
Equipment Connection at the Wing Top and Rear
2.3.1
Remove the padding from the aileron control rod Figure 3 [11]. Connect the aileron control rod
Figure 3 [11] to the bellcrank Figure 3 [14] and install the bolt Figure 3 [10], washer Figure 3 [13] and
nut Figure 3 [12].
2.3.2
Remove the caps and connect the pitot pipes Figure 3 [7] and Figure 3 [8] to the tee piece
Figure 3 [9].
2.3.3
Remove the caps and connect the three wing electrical connectors Figure 3 [1], Figure 3 [2] and
Figure 3 [3] (and four if installed) to the fuselage electrical connectors.
2.3.4
Connect the right inboard flap drive shaft Figure 3 [6], refer to AMM 12-B-27-50-02-00A-920A-A.
2.3.5
Attach the pitot pipe Figure 3 [8] to the support angle Figure 3 [4] with the Cable tie (Pt.No. P09-008)
Figure 3 [5].
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-720A-A
UNCLASSIFIED
2021-12-04 Page 10
