HP d212 Manual do Utilizador Página 79

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FMS-D212-725-1
Page 3-3
• 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
Section 3
Emergency Procedures
3.1 Introduction
Following procedures contain indications of equipment or system failure or
malfunction, use of emergency features of primary and backup systems, and
appropriate warnings, cautions, and explanatory notes. Table 3-1 lists fault
conditions and corrective actions required for illumination of red warning
lights. Table 3-2 addresses malfunction procedures associated with yellow
caution lights.
Corrective action procedures listed herein assume pilot gives first priority to
helicopter control and a safe flight path.
Helicopter should not be operated following any precautionary landing until
cause of malfunction has been determined and corrective maintenance
action taken.
3.2 Definitions
Following terms indicate degree of urgency in landing helicopter.
LAND AS SOON AS POSSIBLE – Land without delay at nearest suitable
area (i.e. open field) at which a safe approach and landing is reasonably
assured.
LAND AS SOON AS PRACTICAL – Duration of flight and landing site are at
discretion of pilot. Extended flight beyond nearest approved landing area is
not recommended.
LAND IMMEDIATELY – The urgency of landing is paramount. The primary
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