G1000 NXi System Maintenance Manual
Page 293
King Air 300 Series
Revision 1
190-00716-N1
5.
If the test input shows an incorrect gauge reading outside the Indication tolerance in
Table 7-7 perform the following:
a. Check gauge circuit wiring for faults.
b. Replace GEA 1.
6.
Turn off the G1000 system and remove external power from the aircraft.
7.
If no other EIS gauge tests are needed, reconnect and safety the J104 connector and
reinstall the engine cowling(s).
If the right engine gauge needs to be tested, perform the following:
1.
Disconnect the J105 firewall connector.
2.
Apply external power to aircraft and start the G1000 system in normal mode.
3.
Inject a resistance into GEA 2 by connecting the Decade box to the left engine firewall
connector-pins J105-W and J105-X.
4.
If the test input shows a correct gauge reading within the Indication tolerance in Table
7-7, troubleshoot the oil temperature sensor per the Beechcraft King Air 300 Series
Maintenance Manual.
5.
If the test input shows an incorrect gauge reading outside the Indication tolerance in
Table 7-7 perform the following:
a. Check gauge circuit wiring for faults.
b. Replace GEA 2.
6.
Turn off the G1000 system and remove external power from the aircraft.
7.
If no other EIS gauge tests are needed, reconnect and safety the J105 connector and
reinstall the engine cowling(s).
Test Point (Ohms)
Indication (C)
75
-46 ± 3
90
0 ± 3
108
50 ± 3
Table 7-7, Oil Temperature Test Points
