HP d212 Manual do Utilizador Página 65

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FMS-D212-725-1
Page 2-21
• 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
Loadmeter – Within Limits
START FUEL switch – ON
Caution Panel – All segments extinguished
AVIONICS MASTER switches – ON
2.5.2 Engine Fails to Start
When the engine fails to start within 15 seconds after the throttle has been
opened to idle, the following action is recommended:
Throttle – Fully close.
Starter – Disengage.
After N
1
has decreased to zero, allow 30 seconds for fuel to drain from
engine.
2.6 Systems Check
2.6.1 Force Trim Check
FORCE TRIM switch – ON.
Flight controls – Friction off, collective lock removed.
Cyclic and pedals – Move slightly each direction to check force gradients.
Cyclic FORCE TRIM release button – Press. Check trim releases with button
pressed, reengages with button released.
FORCE TRIM switch – OFF. Check trim disengages.
FORCE TRIM switch – ON.
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