Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (76)
Page 15 of 21
CHAPTER 76 – ENGINE CONTROLS (76-00-00)

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:
0
Date: 07.05.31
around tube assembly (32) and in opening of
retainer (30) and secure with retainer ring (29).
76.3.1.7.5.4
Place loosened clamp (28) on
boot assembly (27) and install tube assembly
(32) down into boot assembly (27)
76.3.1.7.5.5
Position boot assembly (27)
approximately 0.20 inches (5.08 mm) above
clamp. Adjust boot assembly so that there will
be no blinding during tube extension or
retractions. Install retainer (29) and secure with
clamp (28)
76.3.1.7.5.6
Position tube assembly (32) to
mate with bellcrank (34) and secure with bolt,
washers, nut, and cotter pin.
76.3.1.7.6
Position bellcrank (23) on
mounting and secure with washers, nut and
cotter pin.
76.3.1.7.7
Connect previously installed
tube assembly (32) to bellcrank (23) using bolt,
washers, nut, and cotter pin.
76.3.1.7.8 Install
bellcranks (11, 13, and
15) respective mounts and secure with washers,
nuts, and cotter pins.
76.3.1.7.9. Install
tube assemblies (10, 12,
14, 16, and 18) to their respective bellcranks
and secure with bolts, washers, nuts, and cotter
pins.
NOTE
Check adjustable tube assembly
(14) for 31.19 inches between
centers of rod end bearings.
76.3.1.7.10
Install control rods (7 and 8,
Figure 76-3) on sector gears on pilot and copilot
collectives and bellcrank (8) at center and
secure with screws and blot, washers, nuts, and
cotter pins.
76.3.1.7.11
Final adjustment of adjustable
tube assemblies will be accomplished during
rigging.