Eagle ICA-D212-725, Instructions Manual

Page: 487 / 729

ICA-D212-725 (67)
Page 12 of 55
CHAPTER 67 – FLIGHT CONTROLS (67-00-00)
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COPYRIGHT

2007 BY DART AEROSPACE LTD.

THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO
ANY OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision:
6
Date: 13.08.26
of longitudinal magnetic brake (17) against aft
stop. Adjust force gradient (18) to fit. Extend clevis
on force gradient (18) two turns and install. For
initial installation, install spring (35) in fourth hole
in plate (34).
NOTE
With hydraulic boost on or at ground run-up, adjust
spring tension to position pilot cyclic
stick (25) (longitudinal cyclic only)
perpendicular to deck within 2°.
67.1.7.17
Position pilot cyclic stick (25)
perpendicular to deck within 0.5°. Set output arm
of lateral magnetic brake (20) at center of travel
(view C). Adjust force gradient (21) to fit and install
with bolt and washer. Secure bolt head with
Iockwire (C-405).
NOTE
Check clearances between force gradient
(21) and structure at extreme positions
of magnetic brake arm. If required,
re-index arm relative to shaft by one
serration for clearance. Repeat step 6.1.7.17.
67.1.7.18
Connect spring (2) to bracket on
right forward horn of swashplate.
67.1.7.19
Check complete system for
secure installation and unobstructed full travel.
NOTE
Adjust swashplate lateral pre-tilt, within dimension
of Figure 67-4, for satisfactory flight.