2.3
Equipment Connection at the Wing Top and Rear
2.3.1
Remove the padding from the aileron rod Figure 3 [12]. Connect the aileron rod Figure 3 [12] to the
bellcrank Figure 3 [13] and install the bolt Figure 3 [11], washer Figure 3 [14] and nut Figure 3 [15].
2.3.2
Connect the left inboard flap drive shaft Figure 3 [9] (AMM 12-B-27-50-02-00A-920A-A).
2.3.3
Remove the caps and connect the pitot pipes Figure 3 [5] and Figure 3 [7] to the tee piece
Figure 3 [6].
2.3.4
Attach the pitot pipe Figure 3 [7] to the support angle Figure 3 [10] with the Cable tie (Pt.No. P09-008)
Figure 3 [8].
2.3.5
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.
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-57-00-00-00A-720A-A
UNCLASSIFIED
2021-12-04 Page 10
