
FMS-D212-725-1
Page 3-30
• 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
HEATER O/HEAT High temperature
detected in heater
ducting.
1. HEATER switch – OFF
immediately.
2. CABIN HTR circuit
breaker – Check; if out,
do not reset. If not out –
Pull breaker.
3. Continue flight. Correct
before next flight.
#1 HYDR SYST
or
#2 HYDR SYST
Hydraulic pressure
below limit or
temperature above
limit.
1. Verify fault by reading
affected gauge.
2. Turn off affected system.
3. Land as soon as
practical.
#1 INVERTER
or
#2 INVERTER
(S/Ns 30817,
30687, 30931,
30576 and 30599
Only)
Applicable inverter
has failed
1. Verify other Inverter is
powering AC busses by
reading Voltmeters.
2. Turn off inoperative
Inverter.
3. Continue flight. Correct
before next flight.
#1 INVERTER
or
#2 INVERTER
(All S/Ns EXCEPT
30817, 30687,
30931, 30576 and
30599)
Applicable inverter
has failed
1. Turn off inoperative
Inverter.
2. Continue flight. Correct
before next flight.
Kommentare zu diesen Handbüchern