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Rotax 914 F - 2) Warning Lights

Rotax 914 F
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ReferenceModification no.
- 0 -
Page
211
Date
1997 02 01
Main
914 F
01479
+12V
+12
V
øV
øV
CAUTION LAMP
00211
Pic. 175
13.6.2.2) Warning lights
See Pic. 175.
The TCU is furnished with output terminals for an external red warning lamp
and an orange caution lamp.
Location of the lamps depends on type of aircraft and is limited by the length
of the wiring harness. Standard location is on the instrument panel.
When switching on the voltage supply of the TCU the function of the two
lamps is automatically checked. For approx. 1 to 2 seconds both lamps light
up and then extinguish. If this should not happen check the following:
Inspection for physical damage
Verify connection of cable harness
Check warning lamps for function
NOTE: The two warning lamps are not in the supply volume of
engine.
ATTENTION: Exchange any part with physical damage or if not operating
correctly, without delay.

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