NR Series ENGINE CONTROL SFI SYSTEM P010511 Manifold Absolute Pressure / Barometric Pressure Sensor Circuit Short to Ground
DESCRIPTION
The internal sensor in the No. 2 turbo pressure sensor detects the intake manifold pressure as a voltage. The No. 2 turbo pressure sensor consists of a semiconductor which utilizes the characteristics of a silicon chip that changes its electrical resistance when pressure is applied to it. The sensor converts the intake air pressure into an electrical signal, and sends it to the ECM in an amplified form.
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory | Note |
|---|---|---|---|---|---|---|
| P010511 | Manifold Absolute Pressure / Barometric Pressure Sensor Circuit Short to Ground | The No. 2 turbo pressure sensor output voltage is less than 0.9 V for 3 seconds or more (1 trip detection logic). | ·
Open or short in No. 2 turbo pressure sensor circuit ·
No. 2 turbo pressure sensor ·
ECM |
Comes on | DTC stored | SAE Code: P0107 |
- HINT:
-
When this DTC is output, check the Intake Manifold Absolute Pressure in the Data List. Enter the following menus: Powertrain / Engine / Data List / Intake Manifold Absolute Pressure.
DTC No. Intake Manifold Absolute Pressure Malfunction P010511 Approximately 0 kPa (0 psi) ·Short to ground in PIM circuit
·Short in PIM to EPIM circuit
·Open in VCPM circuit
-
If the Data List values is normal it may be due to a temporary recovery from the malfunction condition. Check for intermittent problems.
MONITOR DESCRIPTION
The ECM monitors the No. 2 turbo pressure sensor voltage and uses this value to calculate the intake manifold pressure. When the No. 2 turbo pressure sensor output voltage deviates from the normal operating range, the ECM interprets this as a malfunction in the No. 2 turbo pressure sensor circuit, illuminates the MIL and stores a DTC.
Example:
If the No. 2 turbo pressure sensor output voltage is less than 0.9 V for 3 seconds or more, the ECM stores this DTC.
MONITOR STRATEGY
| Frequency of Operation | Continuous |
CONFIRMATION DRIVING PATTERN
- HINT:
- ·
After repair has been completed, clear the DTC and then check that the vehicle has returned to normal by performing the following All Readiness check procedure.
·When clearing the permanent DTCs, refer to the "CLEAR PERMANENT DTC" procedure.
Connect the GTS to the DLC3.
Turn the ignition switch to ON.
Turn the GTS on.
Clear the DTCs (even if no DTCs are stored, perform the clear DTC procedure).
Turn the ignition switch off and wait for at least 30 seconds.
Start the engine [A].
Wait 5 seconds or more [B].
Turn the GTS on.
Enter the following menus: Powertrain / Engine / Trouble Codes [C].
Read the pending DTCs.
- HINT:
- ·
If a pending DTC is output, the system is malfunctioning.
·If a pending DTC is not output, perform the following procedure.
Enter the following menus: Powertrain / Engine / Utility / All Readiness.
Input the DTC: P010511.
Check the DTC judgment result.
| GTS Display | Description |
|---|---|
| NORMAL | ·
DTC judgment completed ·
System normal |
| ABNORMAL | ·
DTC judgment completed ·
System abnormal |
| INCOMPLETE | ·
DTC judgment not completed ·
Perform driving pattern after confirming DTC enabling conditions |
- HINT:
- ·
If the judgment result is NORMAL, the system is normal.
·If the judgment result is ABNORMAL, the system is malfunctioning.
·[A] to [C]: Normal judgment procedure.
The normal judgment procedure is used to complete DTC judgment and also used when clearing permanent DTCs.
·When clearing the permanent DTCs, do not disconnect the cable from the battery terminal or attempt to clear the DTCs during this procedure, as doing so will clear the universal trip and normal judgment histories.
WIRING DIAGRAM
CAUTION / NOTICE / HINT
- HINT:
-
Read Freeze Frame Data using the GTS. The ECM records vehicle and driving condition information as Freeze Frame Data the moment a DTC is stored. When troubleshooting, Freeze Frame Data can help determine if the vehicle was moving or stationary, if the engine was warmed up or not, if the air fuel ratio was lean or rich, and other data from the time the malfunction occurred.
PROCEDURE
| *a | Front view of wire harness connector
(to No. 2 Turbo Pressure Sensor) |
- HINT:
-
Make sure that the connector is properly connected. If it is not, securely connect it and check for DTCs again.
Disconnect the No. 2 turbo pressure sensor connector.
Turn the ignition switch to ON.
Measure the voltage according to the value(s) in the table below.
- Standard Voltage:
Tester Connection Condition Specified Condition C99-3 (VC) - C99-2 (E2) Ignition switch ON 4.75 to 5.25 V C99-1 (PIM) - C99-2 (E2) Ignition switch ON 1.2 to 5.25 V
Turn the ignition switch off and wait for at least 30 seconds.
Measure the resistance according to the value(s) in the table below.
- Standard Resistance:
Tester Connection Condition Specified Condition C99-3 (VC) - C99-1 (PIM) Ignition switch off 171 to 189 kΩ
- Result:
Proceed to OK NG
OK
NG
Disconnect the No. 2 turbo pressure sensor connector.
Disconnect the ECM connector.
Measure the resistance according to the value(s) in the table below.
- Standard Resistance:
Tester Connection Condition Specified Condition C99-3 (VC) - C78-138 (VCPM) Always Below 1 Ω C99-1 (PIM) or C78-106 (PIM) - Body ground and other terminals Always 10 kΩ or higher
- Result:
Proceed to OK NG
OK
NG