Flap Deflection Adjustment - FLIGHT DESIGN CTLS Series Maintenance And Inspection Procedures Manual

(Transverse rod tube, left) by 3 hex-nut wrench up to bolts С9996042 (Bolt DIN 912 M5x45-
8.8). Fig. 7.
6) Tighten the nut C9996333 (Self-locking nut DIN 985-M5, regular) on the bolt С9996042 (Bolt
DIN 912 M5x45-8.8) by an 8 wrench and 4 hex-nut wrench. Use only new nuts. Put the washer
С9996503 under the nut C9996333 (Self-locking nut DIN 985-M5). Repeat for all bolts. Fig. 5.
7) Set the flap position indicator to zero.
8) Inspect connection of the tip KA6030201 and the flap rod (КА6030210 and КА6030220,
Transverse rod tube) for play. In case of play replace the rivets (3) (С9996653 Stainl. steel rivet
A2 4x11.5) to next bigger ones (Fig. 8). Eventually diameter of the rivets should not exceed
" / 0.5 mm. If it would, replace the tubes (КА6030210 and КА6030220, Transverse rod
5
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tube) and the tip КА6030201.

4.3.2.6.4 Flap Deflection Adjustment

AF 04800001
Maintenance and Inspection Procedures Manual
CT
Type:
Revision No. 3
CTLS
Series:
Fig. 7
Fig. 8
Page: 4-54
LSA
Date: 14 Sep 2008