HP d212 Manual do Utilizador Página 104

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FMS-D212-725-1
Page 3-28
• 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:
E
TC Approved Date: 09.08.10
Table 3-2 Caution Segments (Amber)
Segment
Indication
Fault Condition Corrective Action
DC GENERATOR Generator has failed
or circuit open.
1. GEN FIELD and RESET
circuit breaker – Check
in.
2. GENERATOR switch –
RESET position, then
ON.
If generator fails to reset
3. GEN switch – OFF.
4. BAT – Check ON.
5. All unnecessary
electrical equipment –
OFF.
6. If possible – descend
below 4600 feet
pressure altitude.
7. Land as soon as
practical.
ENGINE DE-ICE
ON
ENG DE-ICE switch
ON
1. ENG DE-ICE switch –
Position as desired.
ENG FUEL PUMP Failure of either
element of dual
element pump
1. Land as soon as
possible.
ENG ICE DET Engine ice detector
system malfunctioned
1. Icing conditions – Avoid
ENGINE ICING Icing conditions
present
1. ENG DE-ICE switch –
ON
2. Land as soon as
practical
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