Maintenance and Inspection Procedures Manual
Type:
CT
Series:
CTLS
LSA
Page: 4-41
AF 04800001
Revision No. 3
Date: 14 Sep 2008
Install the wings (1 and 2) onto the fuselage. Fix them by the main bolts (3)
КА
2000010. Fig. 8.
While installing the wings make sure that the pin in the flap root bracket (1) (
КА
2040010L for the left wing,
KA2040010R for the right wing) gets into slot in the tip of the flap rod (2)
КА
6030200 (Transverse rod).
Fig. 9.
Fig. 8
Fig. 9