Maintenance and Inspection Procedures Manual
Type:
CT
Series:
CTLS
LSA
Page: 4-25
AF 04800001
Revision No. 3
Date: 14 Sep 2008
Make installation of the new main gear leg in the reverse sequence. If necessary, refer to sections 4.2.2.7
and 4.2.2.6.
Notes:
1. If necessary replace the C9993111B Perbunan gasoline-proof rubber NBR 80 Gas, 2mm (Fig. 6,
item 5) using C9993947N TESAFIX 50m x 0.006m.
2. For mounting bolts KF32100043 (Fig. 7, item 1) and KF32100042 (Fig. 6, item 1) use "Bonding
liquid, middle strength Art.No.3247".
3. Torque moment for M6 self-locking nuts - 9Nm.
4. Mark all bolt-nut connections with "Enamel Red NC-132
К
Art.No.09110".
Important: Use only new M6 self-locking nuts (C9996334).
4.2.2.9 Wheel Inspection and Maintenance
4.2.2.9.1 Type of Maintenance
Line
4.2.2.9.2 Minimum Level of Certification
Repairman, Light Sport Aircraft-Maintenance (RLSA-M) or higher.
4.2.2.9.3 Procedure
Fig. 8
For main wheel inspection (Fig. 8) do the following:
1. Unscrew the bolt KA4020503 (Bolt) by a 19x24 wrench.
2. Unscrew C9997205I (Pins for brake disk) by a 4 hex-nut wrench.
3. Remove the wheel from the axle.
4. Deflate tire before dismantling the rim
5. Unscrew the C9996058 Bolt DIN 912 M6x25-8.8 by a 10x13 wrench and 5 hex-nut wrench.
6. Inspect the rims for dents and cracks. Replace, if necessary.
7. Inspect mounting holes in the rims for bearing, cracks, circularity. Replace if necessary.
8. Inspect bearing for condition and replace if necessary.
