0318956 JOHNSON CARRYING HANDLE


0318956 CARRYING HANDLE JOHNSON 10E74G, 10E75C, 10E76G, 10E77A, 10E78M, 10EL79B, 15E74G, 15E75C, 15E76A, 15E77M, 15E78B, 15E79E, J10ECSE, J10ELCID, J10ELCNS, J10ELCRA, J10ELCTC, J15ECIS, J15ECNC, J15ECRM, J15ECSD, J15ECTR CARRYING
0318956 CARRYING HANDLE JOHNSON
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Number on catalog scheme: 22
 

BRP JOHNSON entire parts catalog list:

10E74G, 10E74S, 10EL74G, 10ELT4S, 10R74G, 10R74S, 10RL74G, 10RL74S 1974
10E75C, 10EL75C, 10R75C, 10RL75C 1975
10E76G, 10E76H, 10E76R, 10EL76G, 10EL76H, 10EL76R, 10R76G, 10R76H, 10R76R, 10RL76G, 10RL76H, 10RL76R 1976
10E77A, 10EL77A, 10R77A, 10RL77A 1977
10E78M, 10EL78M, 10R78M, 10RL78M, 10SEL78M 1978
10EL79B, 10R79B, 10RL79B, 10SEL79B 1979
15E74G, 15E74S, 15EL74G, 15EL74S, 15R74G, 15R74S, 15RL74G, 15RL74S 1974
15E75C, 15EL75C, 15R75C, 15RL75C 1975
15E76A, 15E76R, 15EL76A, 15EL76R, 15R76A, 15R76R, 15RL76A, 15RL76R 1976
15E77M, 15EL77M, 15R77M, 15RL77M 1977
15E78B, 15EL78B, 15R78B, 15RL78B 1978
15E79E, 15EL79E, 15R79E, 15RL79E 1979
J10ECSE, J10ELCSE, J10RCSE, J10RLCSE, J10SELCSE 1980
J10ELCID, J10RCID, J10RLCID, J10SELCID 1981
J10ELCNS, J10RCNS, J10RLCNS, J10SELCNS 1982
J10ELCRA, J10RCRA, J10RLCRA, J10SELCRA 1984
J10ELCTC, J10RCTC, J10RCTR, J10RLCTC, J10RLCTR, J10SELCTC 1983
J15ECIS, J15RCIS, J15RLCIS 1981
J15ECNC, J15RCNC, J15RLCNC 1982
J15ECRM, J15ELCRM, J15RCRM, J15RLCRM 1984
J15ECSD, J15ELCSD, J15RCSD, J15RLCSD 1980
J15ECTR, J15ELCTR, J15RCTA, J15RCTR, J15RLCTA, J15RLCTR 1983

Information:


Illustration 1 g00595836
Schematic For Pressure Sensor (Engine Oil)
The EMCP II monitors the engine oil pressure in order to protect the engine in case of a problem with the oil pressure. The pressure sensor is usually mounted on an oil gallery of the engine. The exact location of the engine oil pressure sensor depends on the engine model.The sensor is powered by an 8 volt sensor supply from the GSC. The oil pressure signal is a pulse width modulated signal. The base frequency of the signal is 500 150 Hz. As pressure changes, the duty cycle of the signal varies from 10% to 95%. A pressure of 0 kPa (0 psi) is approximately 13% of the duty cycle. A pressure of 690 kPa (100 psi) is approximately 85% of the duty cycle.Note: The GSC is usually programmed to treat a diagnostic code with the pressure sensor as an alarm fault (P04 = 0). If the GSC is programmed to treat a fault with the pressure sensor as a shutdown fault (P04 = 1), then diagnostic codes are automatically shown on the upper display.Note: Faults are created when the harness connector (40 contact) is disconnected from the GSC during these troubleshooting procedures. Clear these created faults after the particular fault is corrected. In a properly operating system, when the harness connector is removed from the GSC, the following diagnostic codes are recorded.
CID 100 FMI 3 pressure sensor (engine oil)
CID 110 FMI 3 temperature sensor (engine coolant)
CID 111 FMI 3 fluid level sensor (engine coolant)
CID 190 FMI 3 speed sensor (engine)
CID 331 FMI 2 switch (engine control)
CID 336 FMI 2 switch (engine control)ProcedureThis diagnostic code can be caused by the following conditions:
The base frequency of the sensor is beyond the accepted limits.
The duty cycle of the sensor signal is beyond the accepted limits.Begin performing these procedures only when CID 100 FMI 2 is showing and the "DIAG" indicator is FLASHING on the upper display. The GSC treats a CID 100 FMI 2 as an alarm fault. Active alarm faults are shown on the display when the alarm codes key is pressed and the ECS is in any position except the OFF/RESET position. For an inactive fault, the problem may be intermittent. To troubleshoot an inactive fault, use the preceding system schematic and see Testing And Adjusting, "Electrical Connector - Inspect". Clear the diagnostic code from the fault log after troubleshooting is complete.Note: This procedure can be replaced with Testing and Adjusting, "Pulse Width Modulated (PWM) Sensor - Test" if you are using a meter with the capability of measuring frequency and duty cycle.Note: If CID 269 is active, then correct the diagnostic code prior to proceeding with this procedure.
Check the GSC and the harness.
Ensure that CID 100 FMI 2 is showing on the display.
Turn the ECS to the "OFF/RESET" position.
Disconnect the sensor from the engine harness. The sensor should remain fastened to the engine.
Turn the ECS to the "STOP" position.
Press the alarm codes key. This is not required for shutdown faults.
Verify that CID 100 FMI 02 is no longer showing and verify that CID 100 FMI 03 is now showing. Expected Result: CID 100 FMI 2 is not showing. CID 100 FMI 3 is now showing.Results:
OK - The GSC and the harness function properly. Therefore, the sensor is faulty. Replace the sensor. STOP.
NOT OK - CID 100 FMI 02 is still showing. There is a fault in the GSC or the harness. Proceed to 2.
Check the GSC.
Turn the ECS to the "OFF/RESET" position.
Disconnect the harness connector from the GSC.
Turn the ECS to the "STOP" position.
Press the alarm codes key.
Verify that CID 100 FMI 02 is no longer showing and verify that CID 100 FMI 03 is now showing. Expected Result: CID 100 FMI 2 is not showing. CID 100 FMI 3 is now showing.Results:
OK - The GSC functions properly. Therefore, the signal wire is faulty in the harness. Troubleshoot the signal wire in the harness between the sensor connector and the GSC connector. Also check the electrical connectors and terminals. See Testing and Adjusting, "Electrical Connector - Inspect". STOP.
NOT OK - CID 100 FMI 2 is still showing. The GSC is faulty. Replace the GSC. See Testing and Adjusting, "EMCP Electronic Control (Generator Set) - Replace".


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