2.6
Forward De-ice Pipeline Connection
2.6.1
Remove the caps. Put the forward cross connector Figure 6 [19] in position and connect the de-ice
pipe Figure 6 [7] to the ejector flow control valve Figure 6 [8].
2.6.2
Remove the caps and connect the de-ice pipe Figure 6 [15] to the pressure switch Figure 6 [12].
2.6.3
Remove the caps. Put the rear cross connector Figure 6 [6] in position and connect the de-ice pipe
Figure 6 [11] to the ejector flow control valve Figure 6 [10].
2.6.4
Remove the caps and connect the de-ice pipe Figure 6 [14] to the pressure switch Figure 6 [13].
2.6.5
Remove the caps. Put the tee connector Figure 6 [4] in position and connect the de-ice pipes
Figure 6 [3], Figure 6 [9] and Figure 6 [5].
2.6.6
Remove the caps and connect the de-ice pipe Figure 6 [9] to the tee connector Figure 6 [16].
2.6.7
Remove the caps and install the de-ice pipe Figure 6 [18] between the rear cross connector
Figure 6 [6] and the fuselage.
2.6.8
Remove the caps and install the de-ice pipe Figure 6 [1] between the forward cross connector
Figure 6 [19] and the fuselage.
2.6.9
2.6.10
Remove the electrical cable temporary attachment to the wing. Position the cable along the de-ice
pipe Figure 6 [18] and attach the cable to the pipe with the Cable tie (Pt.No. P09-008).
2.6.11
Install the right wing tip, refer to AMM 12-B-57-33-00-00A-920B-A.
2.6.12
Remove the rigging pin Figure 3 [16] from the right aileron bell crank Figure 3 [15].
2.6.13
Remove the rigging pin Figure 3 [21] from the aileron control cable segment.
2.6.14
Remove the jack and trestle from the left wing.
2.6.15
Do the close up procedure.
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 17
