Pilatus PC-12/47E MSN-1001-UP, Руководство по обслуживанию

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2.3 Equipment Connection at the Wing Top and Rear
2.3.1 Connect the bonding cable Figure 4 [18] to the earth stud GS500 Figure 4 [17] and install the washer
Figure 4 [19] and the nut Figure 4 [20].
2.3.2 Remove the padding from the aileron control rod Figure 4 [12]. Connect the aileron rod Figure 4 [12] to
the bellcrank Figure 4 [13] and install the bolt Figure 4 [11], washer Figure 4 [14] and nut Figure 4 [15].
2.3.3 Connect the left inboard flap drive shaft, refer to AMM 12-B-27-50-02-00A-920A-A.
2.3.4 Remove the caps and connect the pitot pipes Figure 4 [5] and Figure 4 [7] to the tee piece
Figure 4 [6].
2.3.5 Attach the pitot pipe Figure 4 [7] to the support angle Figure 4 [10] with the Cable tie (Pt.No. P09-008)
Figure 4 [8].
2.3.6 Remove the caps and connect the wing electrical connectors Figure 4 [1], Figure 4 [2], Figure 4 [3]
and Figure 4 [4] to the fuselage electrical connectors.
2.4 Equipment Connection at the Wing Bottom Center
2.4.1 Put the ends of the bonding straps Figure 3 [9] in position and install the bolt Figure 3 [10] and nut
Figure 3 [11].
2.4.2 Remove the caps and install the brake pipe Figure 3 [8] between the fuselage and the wing.
2.4.3 Remove the caps and install the grommet Figure 3 [4] and the three fuel pipes Figure 3 [1],
Figure 3 [2] and Figure 3 [3] between the fuselage and the connections in the landing gear
compartment.
2.4.4 Remove the caps and connect the two rear de-ice pipes Figure 3 [12]. Tighten the two clamps
Figure 3 [13].
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-720B-A
UNCLASSIFIED 2021-12-04 Page 11