Lycoming TEO-540-C1A Maintenance Manual page 479

TEO-540-C1A Engine Maintenance Manual
Fault ID 194
Fault Primary: FRP Circuit Fault
Description Secondary: FPP Circuit Fault
This fault occurs if the Raw voltage observed on the input is outside the expected window
defined by the calibratable Highest and Lowest Valid Raw voltage values.
This does not distinguish between Open and Short Circuit Faults as any of the following
Root Cause
failures would result in the Raw voltage outside the expected voltage window:
-
-
1. Run the engine in accordance with the engine and aircraft maintenance manuals. Is the fault active?
If yes, go to step 3. If no, go to step 2.
2. Using the FST, download active and service fault logs, then clear fault logs and monitor engine
operation for the fault to repeat.
3. Inspect sensor, and lines for any damage (eg...burned, broken or frayed wires, cracked or broken
connectors or hoses, burned or broken sensors). If damage is found, replace the damaged part per the
"Sensor Replacement Procedure" in Chapter 72-70. If no damage is found, go to step 4.
4. Inspect harness connection for any damage (eg...burned, broken or frayed wires, cracked or broken
connectors). Contact Lycoming if harness damage is found. If no damage found, go to step 5.
5. Swap fuel rail pressure sensor with fuel pump pressure sensor and run the engine. Does the fault move
with the sensor? If yes, replace the sensor. If no, go to step 6.
6. Complete a continuity test of the harness from the harness sensor connector to the ECU connector using
the engine system schematic. If the continuity check fails, isolate to affected harness by disconnecting
the firewall connection, then contact Lycoming Engines. If the continuity checks good, replace the
sensor. If fault persists, replace the ECU.
Fault ID 195
Primary: -reserved-
Fault
Secondary: Op Mode Selector Circuit
Description
This fault occurs if the Raw voltage observed on the input is outside the expected window
defined by the calibratable Highest and Lowest Valid Raw voltage values.
This does not distinguish between Open and Short Circuit Faults as any of the following
Root Cause
failures would result in the Raw voltage outside the expected voltage window:
-
-
1. Inspect wires and resistors connected to switch for breaks or damage. Are wires or resistors broken or
damaged? If yes, repair in accordance with the aircraft maintenance manual. If no, go to step 2.
2. Disconnect wires from switch and disconnect ECU connector A001-P2. Measure resistance from A001-
P2 pin 48 to each wire and check for resistance as shown in the table below. Are the resistances
measured within the table limits? If yes, go to step 4. If no, but resistance is present and not within
table limits, replace the defective resistor in accordance with the aircraft maintenance manual. If no, and
circuit is open, go to step 3.
Switch Position
C
NORM
S
© 2018 Avco Corporation. All Rights Reserved
November 2018
Fault Group
-
Open Circuit
-
Short to 5V
Troubleshooting Steps
Fault Group
Fault
-
Open Circuit
-
Short to 5V
Troubleshooting Steps
Resistance
330kΩ
1.01MΩ
3.21MΩ
25 Fault Name
Fault Lamp
Short to VPwr
Short to GND
25 Fault Name
Fault Lamp
Short to VPwr
Short to GND
Tolerance
±10%
±10%
±10%
[FAULT: AN25 circuit]
TLO
[FAULT: AN30 circuit]
TLO
Appendix D
Page 449