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

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5.12 Examine the vertical stabilizer outer surface for cracks, deformation and skin distortion.
5.13 Examine the vertical stabilizer fairing 32CT for damage.
5.14 Examine the composite lower rudder fairing 32AB for damage.
5.15 Look at the rudder mechanism below the cockpit floor and examine the rudder stops for damage.
6 Installation
6.1 Install the hinge support fitting Figure 3 [5] to the fuselage structure with a new Bolt Figure 3 [12] new
Washer Figure 3 [11] and new Nut Figure 3 [10].
6.2 Install the hinge bracket Figure 3 [4] to the fuselage structure with the bolts Figure 3 [14] washers
Figure 3 [13] washers Figure 3 [9] and nuts Figure 3 [8].
6.3 Assemble the rudder stop Figure 3 [15] to the rudder stop assembly Figure 3 [1].
6.4 Install the rudder stop fitting/assembly Figure 3 [1] and the bonding leads Figure 3 [3].
6.5 Install a new Bearing Figure 2 [4] in the cable quadrant Figure 2 [3]. Secure with a new Retaining
ring Figure 2 [5].
6.6 Install the cable quadrant Figure 2 [3]. Use a new Bolt Figure 2 [1], new Washer Figure 2 [2] new
Nut Figure 2 [6] and a new Cotter pin Figure 2 [7].
6.7 Attach the rudder cables Figure 2 [9] to the cable quadrant Figure 2 [3] and secure each rudder cable
with a new Cotter pin Figure 2 [8].
6.8 Install the rudder, refer to AMM 12-B-55-40-01-00A-920A-A. After installation of the rudder, do an
adjustment and test of the rudder control system, refer to AMM 12-B-27-20-00-00A-903A-A.
Note
If a new rudder is installed, make sure the painted rudder is balanced before installation. To balance the
rudder, refer to SRM
12-B-51-60-03-00A-276A-A .
Note
Use a new Bolt Figure 4 [2] when you attach the rudder to the top hinge.
6.9 Do the functional test of the rudder control system, refer to AMM 12-B-27-20-00-00A-903A-A.
6.10 Install the rear vertical stabilizer fairing 32CT and the horizontal stabilizer fairing.
6.11 Do the functional test of the elevator control system, refer to AMM 12-B-27-30-00-00A-903A-A.
6.12 Do the operational test of the horizontal stabilizer trim, refer to AMM 12-B-27-40-00-00A-903A-A.
6.13 Close access panels 31AB, 32AL, 32AR, 32CL and 32CR.
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-05-50-11-00A-282A-A
UNCLASSIFIED 2021-12-04 Page 5