
FMS-D212-725-1
Page 2-18
• 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
IN DETENT POSITION (OFF) AT ALL TIMES WHEN
ENGINE RUNNING.
ROTOR BRAKE LIGHTS (if installed) – Test. Pull brake lever and check that
both lights illuminate; return to off and check lights extinguish.
HEATER switch – ON; Verify HEATER ON light illuminates.
Raise Collective until Bleed Air Priority switch actuates (HEATER OFF light
illuminates, HEATER ON light extinguishes).
Lower Collective to the full down position, verify HEATER OFF light
extinguishes and HEATER ON light illuminates.
HEATER switch – OFF.
Non-essential buss – Normal
Light rheostats (6) – As Required.
GOV RPM switch – Decrease for 10 seconds.
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