XtremeAIR XA41, Руководство по обслуживанию

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Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page date: Page 7
25.09.2018 Chapter 20
20-20-02 Assembly Instructions
Unless specified differently, torque all bolts and nuts as given in chapters 20-10-02 and -03.
Assemble the aircraft in the sequences as follows:
1
Remove the rudder if it is installed to the fuselage; refer to chapter 55-60-00.
2 Prepare the stabilizer assembly: Clean it and lubricate the bolts and bushings with
grease.
3 Install the stabilizer assembly. Follow the installation instructions in chapter 55-10-
00.
4 If the elevator was removed, install the elevator. Refer to chapter 55-20-00.
5 Install the elevator control rod between the elevator bell crank and the elevator.
Refer to chapter 27-30-02 and 27-30-03
6 To install the rudder, refer to chapter 55-60-00.
7 Install the wing. Refer to chapter 57-10-00.
8 If temporary transportation nuts are installed on the wheel axles, remove the nuts.
Install operational wheel nuts on the wheel axles. Safety the nuts with a split pin,
DIN 94 3.2x50mm.
Figure 20-1: Transportation nut (left) operational wheel nut (right)
9 Install the propeller, refer to chapter 61-10-00.
10 Install the landing gear fairings, refer to chapter 32-50-00
11 Install the cowling, refer to chapter 71-10-00.
12 Adjust the ailerons, if necessary. Refer to chapter 27-10-00.
13 Install the spades on the aileron horns, refer to chapter 27-10-01.
14 Connect the battery, RH front footrest (6 mm bolts, 10 mm wrench).
15 Do a functional test of the trim tab.
16 Check that the fuel gage indication is correct.
17 Install the baggage compartment (MS 1032 screws, PH 2 screwdriver). Refer to
chapter 25-50-00.
18 Install the two seats (MS 1032 screws, PH 2 screwdriver). Refer to chapter
25-10-01.
19 Close all access hatches in the cockpit (MS 1032 screws, PH 2 screwdriver).