Eagle ICA-D212-725, Instructions Manual

Page: 243 / 729

ICA-D212-725 (29)
Page 46 of 50
CHAPTER 29 – HYDRAULIC SYSTEM (29-00-00)
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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
CAUTION
DO NOT ATTEMPT ANY ADJUSTMENT OF
SERVO VALVE OR BYPASS VALVE 0F
HYDRAULIC CYLINDER. IF MALFUNCTION
OCCURS, REPLACE CYLINDER ASSEMBLY.
29.3.10.3.7 Check anti-torque controls for free
movement through full range of travel and for
interference or binding of hydraulic hoses. Apply
hydraulic pressure and check for leaks.
29.3.10.3.8 Close access door.
29.4 ROTOR BRAKE HYDRAULIC
SYSTEM
29.4.1 Rotor Brake System
Hydraulic pressure to operate the rotor brake
system is provided by actuation of lever (5,
Figure 29-11) on master cylinder (4) located in
the cabin roof.
29.4.2 Troubleshooting
The following list of probable causes, isolation
procedures and remedies is intended to aid in
rotor brake system troubleshooting.