Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (67)
Page 40 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
67.3.7.1.11 Disassemble and remove burrs
and metal particles.
67.3.7.1.12
Install tapered bushing and secure
with bolt, washer and nut (7).
NOTE
After torquing bolt (7), the washer must
be held off the surface of jackshaft tube
within limits given in Figure 67-16, detail A.
67.3.7.1.13
Repeat steps 67.3.7.1.7 through
67.3.7.1.11 for remaining holes.
67.3.7.1.14
Apply primer (C-204) to all raw
metal.
67.3.7.1.15 Insert right and left tube
assemblies, with bearings and supports in place,
through access openings at sides of cabin lower
skin. Slip ends of tubes on stub shafts of control
arm. Align bolt holes with center arm pointing
up and end arms down, and install bolts and
tapered bushings. Secure right and left housing
assemblies (5 and 6) to each beam with four
bolts, washers and nuts. Check for free
operation.
67.3.7.1.16
Connect control tubes (1, 2 and
3) to jackshaft
67.3.7.1.17
Connect force gradient (4) to
jackshaft. Check rigging (paragraph 67.1.6 or
67.1.7).