
FMS-D212-725-1
Page 2-24
• 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
INV 1 – OFF
AC Voltmeter 104 to 122 VAC (if installed).
#1 INVERTER caution light illuminates
INV 1 – ON
AC Voltmeter 104 to 122 VAC (if installed).
#1 INVERTER caution light extinguishes
DC Voltmeter – Indicates 28 ± 1 VDC.
For all S/Ns EXCEPT 30817, 30576, 30687 and 30599
GCU Check.
GCU TEST switch - OVERVOLTAGE, DC GENERATOR light on and DC
generator offline
GCU TEST switch - center
GEN switch - RESET and then ON, DC GENERATOR light OFF
GCU TEST switch - OVERLOAD, DC GENERATOR light ON
GCU TEST switch - center
GEN switch - RESET and then ON, DC GENERATOR light OFF.
PITOT HTR – Check. Place PITOT HTR switch in ON position. Note
Loadmeter increase. Return to OFF position.
2.6.7 Hydraulic System Checks
Note
This check is to determine proper operation of hydraulic
actuators for each flight control system. If abnormal
forces, unequal forces, control binding or motoring is
encountered, it may be an indication of a malfunction of
a flight control actuator.
FORCE TRIM switch – OFF.
Collective – Down, friction removed.
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