HP d212 Manuel d'utilisateur Page 41

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FMS-D212-725-1
Page 1-32
• 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
Dual Tachometer (for aircraft with AC powered instrument system)
Engine Tachometer
97.0%
97.0 to 100%
100%
Rotor Tachometer
91.0%
91.0 to 104.5%
104.5%
Dual Tachometer (for aircraft with DC powered instrument system)
Engine Tachometer
97.0%
97.0 to 100%
100%
Rotor Tachometer
91.0%
91.0 to 104.5%
104.5%
Figure 1-13 – Instrument Markings
(Sheet 6 of 9)
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