Pilatus PC-12/47E MSN-1001-UP, Maintenance Manual

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2 Installation
2.1 Make sure that the damping gasket is installed and is not damaged. If required, use the
manufacturer's instructions to replace the damping gasket.
2.2 Put the roll actuator Figure 1 [5] in position on the mount Figure 1 [3] and install the two washers
Figure 1 [2] and bolts Figure 1 [1].
Note
If a new actuator is to be installed, remove the two anchor nuts from the removed actuator and install
them on the new actuator.
2.3 Torque the bolts Figure 1 [1] to 4,5 to 5,6 Nm (40 to 50 lbf in).
2.4 Use the Lockwire (Pt.No. P02-007) Figure 1 [6] to safety the bolts Figure 1 [1].
2.5 Apply Glyptal (Pt.No. P08-076) to the bolts Figure 1 [1].
2.6 Connect the electrical connector Figure 1 [4] to the actuator.
2.7 Remove the safety clip and close the circuit breakers:
− A/P SERVO (AVIONIC 1 BUS)
− A/P SERVO ENABLE (AVIONIC 1 BUS).
3 Close Up
3.1 Do the operational test of the autopilot system, refer to AMM 12-B-22-10-00-00A-903A-A.
3.2 Remove all the equipment, tools and materials from the work area. Make sure that the work area is
clean.
3.3 Close the access panel 12EZ.
3.4 Install the center carpet:
− For Executive interior, refer to AMM 12-B-25-21-04-00A-920A-A
− For Standard interior, refer to AMM 12-B-25-22-04-00A-920A-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-22-10-03-00A-920A-A
UNCLASSIFIED 2021-12-04 Page 3