I do not have a 915is to reference so I will make an educated guess.
With the Lanes powered up ...
Guess #1
If the EGT Sensors Do NOT share the #1 Pin on the connector.
EGT #4 is connected to pins 1 and 2 and EGT #2 is connected to Pins 3 and 4.
With your meter set to Ohms (Not Continuity);
On the Connector to the sensors:
Pins 1 to 2 should Measure ~210 Ohms at Room Temperature.
Pins 3 to 4 should Measure ~210 Ohms at Room Temperature.
On the Connector going to the ECU:
Pin 1 should measure +5V referenced to the Airframe Ground.
Pin 4 should measure +5V referenced to the Airframe Ground.
The connections might also be EGT 2 on 1 and 3, and EGT 4 on 2 and 4.
Use your powers of observation.
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Guess #2
If the EGT Sensors DO share the #1 Pin on the connector.
EGT #4 is connected to pins 1 and 2 and EGT #2 is connected to Pins 1 and 3. Pin 4 is the Shield.
With your meter set to Ohms (Not Continuity);
On the Connector to the sensors:
Pins 1 to 2 should Measure ~210 Ohms at Room Temperature.
Pins 1 to 3 should Measure ~210 Ohms at Room Temperature.
On the Connector going to the ECU:
Pin 1 should measure +5V referenced to the Airframe Ground.
Pin 4 should measure +0V referenced to the Airframe Ground.
Compare the readings on the 1/3 EGT connector to the 2/4 EGT Connector.
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You are mixing what you are saying.
Are you reading EGT values off the ECU CAN-Bus using the BUDS Interface?
Or are you using a panel-mounted EMU?
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The EGTs are high-tempThermistors.
The Thermistor Drive is the 5-volt power supply for the EGTs.
If the 5 Volt Thermistor Drive Power Supply Faults out, ALL the EGTs will fail as a group.
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There is also the option of swapping the 1/3 EGTs with the 2/4 EGTs to see if the fault moves to a different cylinder.