2.1.24.1
If the gap is less than 0,5 mm (0.02 in) go to Step 2.1.25.
2.1.24.2
If the gap is 0,5 mm (0.02 in) or more, install a shim Figure 1 [26] between the fuselage frame 24 and
the wing rear spar.
2.1.25
Install the shim Figure 1 [26] if previously installed, and the washers Figure 1 [23] with the chamfer
towards the fitting. Use Grease (Pt.No. P04-029) to lubricate the nut. Install the new nut Figure 1 [22]
and torque to between 112 and 120 Nm (992 and 1062 lbf in) plus the nut friction torque. Make sure
the washer Figure 1 [23] does not turn when the nut Figure 1 [22] is torque tightened.
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 6
