
FMS-D212-725-1
Page 2-16
• 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
ANTI-COLL light switch – BOTH
POSITION light switch – As Desired
UTILITY LIGHT switch – OFF.
INV1 and INV2 switches – ON.
NON ESS BUS switch – MANUAL
GENERATOR switch – OFF.
BATTERY switch – ON.
Note
If EXTERNAL POWER is being used, BATTERY switch
must be placed in the ON position to energize electrical
systems.
Note
If external power (1000 amps maximum) is used adjust
power source voltage to 27 ± 1 VDC.
DC Voltmeter – Greater than 24 VDC.
AC voltmeter – (S/Ns 30687, 30576, 30817 and 30599 only) 104 to 122 VAC.
AC voltage – (All EXCEPT S/Ns 30687, 30576, 30817 and 30599) – Verify
both #1 and #2 inverter caution lights out.
Engine Instruments – Check gauges for proper indications.
ENGINE RPM and ROTOR RPM warning light (LH and RH side) –
Illuminated.
CARGO FIRE TEST switch – Test, verify lights flash
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