
FMS-D212-725-1
Page 2-25
• 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:
G
TC Approved Date: 13.08.09
ROTOR RPM (N
R
) – Set to 100%
Cyclic – Centered, friction removed.
Hydraulic System – Check as follows:
HYDR SYS NO. 1 switch – OFF. Check MASTER CAUTION light illuminates
and #1 HYDR SYST caution light illuminates. Hydraulic system no. 1
pressure decreases.
Cyclic – Check normal operation by moving cyclic in an “X” pattern, right
forward to left aft, then left forward to right aft (approximately 1 inch). Center
cyclic.
Collective – Check normal operation by increasing collective slightly (1 to 2
inches). Return to down position.
Note
Boost for tail rotor controls is furnished by hydraulic
system no. 1 only. When hydraulic system no. 1 is being
checked, tail rotor controls will be unboosted.
Pedals – Displace slightly left and right. Note an increase in force required to
move pedals.
Warning
DO NOT TURN BOTH HYDRAULIC SYSTEMS OFF AT
SAME TIME DUE TO EXCESSIVE FORCE REQUIRED
TO MOVE FLIGHT CONTROLS.
HYDR SYS NO. 1 switch – ON. Check MASTER CAUTION light
extinguishes and hydraulic system no. 1 pressure returns to normal. #1
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