Maintenance and Inspection Procedures Manual
Type:
CT
Series:
CTLS
LSA
Page: 4-53
AF 04800001
Revision No. 3
Date: 14 Sep 2008
Fig. 5
Fig. 6
4.3.2.6 Flap
Adjustment
4.3.2.6.1 Type of Maintenance
Line
4.3.2.6.2 Minimum Level of Certification
Repairman, Light Sport Aircraft-Maintenance (RLSA-M) or higher.
Flight Design task specific training required.
4.3.2.6.3 Rigging “Zero” Position of the Flaps
“Zero” position is the position of the flaps when the top skin of the flaps is aligned with the top of the
fuselage.
If the flaps are not synchronous (at the “zero” position one is higher than another), adjust the flap rod
КА
6030200 (Transverse rod) as follows.
1) Unscrew the lock-nut C9996332 (Self-locking nut DIN 985-M4, regular) by a 7 wrench towards
the head of the bolt and release the bolts C9996026 (Bolt DIN 912 M4x 20-8.8), Fig. 7.
2) Unscrew the bolts C9996026 (Bolt DIN 912 M4x20-8.8) 5 turns from the flange of the flap rod
KA6030220 (Transverse rod tube, left) by a 3 hex-nut wrench. Fig. 7.
3) Unscrew the nuts C9996333 (Self-locking nut DIN 985-M5, regular) from the bolts
С
9996042
(Bolt DIN 912 M5x45-8.8) by an 8 wrench and 4 hex-nut wrench. Fig. 7.
4) Turn KA6030210 (Transverse rod tube, right) and KA6030220 (Transverse rod tube, left) with
respect to each other so that both flaps are aligned to the top of the fuselage.
5) Fix position of the bolts
С
9996042 Bolt DIN 912 M5x45-8.8 with respect to the KA6030220
(Transverse rod tube, left) by the bolts C9996026 (Bolt DIN 912 M4x20-8.8). The bolts
C9996026 (Bolt DIN 912 M4x20-8.8) are to be screwed into the flange of KA6030220