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

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Support equipment
Table 3 Support equipment
Name Identifications/References Qty Reference Remark
Safety clip (circuit breaker hold
open) Part T12-030 AR
Supplies
Table 4 Supplies
Name Identifications/References Qty Reference Remark
Lockwire Part P02-007 AR
Corrosion preventative Part P10-013 AR
Spares
Table 5 Spares
Name Identifications/References Qty Reference Remark
None
Safety Conditions
Note
To identify the consumable items used in this procedure refer to the Consumable Materials List, AMM 12-B-20-31-
00-00A-070A-A .
Note
To identify the AGE and tools used in this procedure, refer to the List of AGE and Tools, TEM
12-B-00-00-00-00A-
060A-A .
Procedure
1 Removal
1.1 Open and install a Safety clip (circuit breaker hold open) (Pt.No. T12-030) on these circuit breakers:
− A/P SERVO (AVIONICS 1 BUS)
− A/P SERVO ENABLE (AVIONICS 1 BUS).
1.2 Open the access panel 31AB.
1.3 Disconnect the electrical connector Figure 1 [1] from the pitch actuator Figure 1 [4].
1.4 Cut and remove the lockwire from the bolts Figure 1 [2].
1.5 Hold the pitch actuator Figure 1 [4]. Remove the two bolts Figure 1 [2] and washers Figure 1 [3] then
remove the pitch actuator from the mount Figure 1 [5].
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.
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-22-10-02-00A-920A-A
UNCLASSIFIED 2021-12-04 Page 2