Maintenance and Inspection Procedures Manual
Type:
CT
Series:
CTLS
LSA
Page: 4-22
AF 04800001
Revision No. 3
Date: 14 Sep 2008
Fig. 4
4.2.2.6.5 Before Installation
Inspect the bolts for burrs, dents and thread integrity. Replace, if there is any doubt about bolt condition.
Inspect the wheel attachment for dents and cracks, mounting holes for integrity and circularity. Replace, if
necessary.
4.2.2.6.6 Main Wheel Installation
Make installation in the reverse sequence (Fig. 4). Use new self-locking nuts only.
Note:
Torque moment for nuts: Self-locking nut DIN 985-M6, regular, C9996334 - 9Nm; Nut M20x1.5,
C9997207T - 70Nm. Torque moment for bolts: Bolt DIN 912 M8x90 A4-70, C9996088 - 9Nm; Pin for
brake disk, C9997205I - 9Nm.
For mounting KF32100043, KF32100037, C9996088, C9997205I use "Bonding liquid, middle strength
Art.No.3247".
Mark all bolt-nut connections with "Enamel Red NC-132
К
Art.No.09110".
Install spacer for camber and toe-in adjusting. Angles of camber and toe-in assure at empty plane with
engine installed and wings attached. Spacers: KF32100054, KF3210056 - use for camber adjusting,
KF32100055, KF32100057- for toe-in adjusting. Maximum quantity of spacers on each wheel 2 pcs.