Diagnostic Instructions
DTC Descriptor
DTC P0106
Manifold Absolute Pressure (MAP) Sensor Performance
Diagnostic Fault Information
Typical Scan Tool Data
MAP Sensor
MAP Sensor, if equipped with Turbocharger
Circuit Description
The manifold absolute pressure (MAP) sensor measures the pressure inside the intake manifold.
Pressure in the intake manifold is affected by engine speed, throttle opening, air temperature, barometric pressure (BARO) and if equipped, turbocharger output. A diaphragm within the MAP sensor is displaced by the pressure changes that occur from the varying load and operating conditions of the engine. The sensor translates this action into electrical resistance.
The MAP sensor wiring includes 3 circuits. The engine control module (ECM) supplies a regulated 5 volts to the sensor on a 5 V reference circuit. The ECM supplies a ground on a low reference circuit. The MAP sensor provides a signal voltage to the ECM, relative to the pressure changes, on the MAP sensor signal circuit. The ECM converts the signal voltage input to a pressure value.
Under normal operation the greatest pressure that can exist in the intake manifold is at ignition ON, engine OFF, which is equal to the BARO. If equipped, a turbocharger can increase the pressure above BARO, when the vehicle is operated at wide-open throttle (WOT). The lowest manifold pressure occurs when the vehicle is idling or decelerating. The ECM monitors the MAP sensor signal for pressure outside of the normal range.
Conditions for Running the DTC
Conditions for Setting the DTC
The ECM determines if the MAP Sensor is not within the normal operating range. It accomplishes this by running 3 different models within the software to determine the values, for greater than 0.5 S.
Action Taken When the DTC Sets
DTC P0106 is a Type B DTC.
Conditions for Clearing the MIL/DTC
DTC P0106 is a Type B DTC.
Reference Information
Schematic Reference
Engine Controls Wiring Schematics (LTG)
Connector End View Reference
Component Connector End View Index
Powertrain Component View
Powertrain Component Views
Electrical Information Reference
DTC Type Reference
Powertrain Diagnostic Trouble Code (DTC) Type Definitions
Scan Tool Reference
Control Module References for scan tool information
Special Tools
GE-23738-A Vacuum Pump
For equivalent regional tools, refer to Special Tools (diagnostic tools) and Special Tools (Mechanical Tools).
Circuit/System Verification
1. Ignition ON.
2. Verify that DTC P0641, P0651, P0697, P06A3, or P06D2 is not set.
Refer to Diagnostic Trouble Code (DTC) List - Vehicle for further diagnosis.
3. If you were sent here from DTC P0068, P0101, P0121, P0236, or P1101 refer to Circuit/System Testing.
4. Verify the scan tool Throttle Body Idle Airflow Compensation parameter is less than 90%.
Refer to Throttle Body Cleaning.
5. Verify the scan tool Throttle Body Sensors 1 and 2 Agree/Disagree parameter displays Agree while performing the Throttle Sweep Test with a scan tool.
Refer to DTC P0121-P0123, P0222, P0223, P16A0-P16A2, or P2135 for further diagnosis.
6. Determine the current vehicle testing altitude.
7. Verify the scan tool MAP Sensor pressure parameter is within the range specified in the Altitude Versus Barometric Pressure table.
Refer to Circuit/System Testing.
8. Verify if the engine is equipped with a turbocharger.
Refer to Step 12.
9. Verify the scan tool Boost Pressure Sensor parameter is within the range specified in the Altitude Versus Barometric Pressure table.
Refer to DTC P0236 for further diagnosis.
10. Verify the scan tool Boost Pressure Sensor parameter decreases after starting the engine.
Refer to DTC P0236 for further diagnosis.
11. Engine idling.
12. Verify the scan tool MAP Sensor pressure parameter is between 26 - 52 kPa (3.8 - 7.5 PSI) and changes with accelerator pedal input.
Refer to Circuit/System Testing.
13. Verify the scan tool MAF Sensor g/s parameter changes smoothly and gradually as the engine speed is increased and decreased while performing the actions listed below.
Refer to DTC P0101 for further diagnosis.
14. Operate the vehicle within the Conditions for Running the DTC. You may also operate the vehicle within the conditions that you observed from the Freeze Frame/Failure Records data.
15. Verify a DTC does not set.
Refer to Circuit/System Testing.
16. All OK.
Circuit/System Testing
1. Verify the integrity of the entire air induction system and verify that none of the following conditions exist:
If a condition is found, repair or replace the component as appropriate.
2. Ignition OFF and all vehicle systems OFF. It may take up to 2 min for all vehicle systems to power down. Disconnect the harness connector at the B74 Manifold Absolute Pressure Sensor.
3. Test for less than 2 Ω between the low reference circuit terminal 2 and ground.
If 2 Ω or greater
Go to next step: If less than 2 Ω
4. Ignition ON.
5. test for 4.8 - 5.2 V between the 5 V reference circuit terminal 1 and ground.
NOTE: If the signal circuit is shorted to a voltage the ECM or the MAP Sensor may be damaged.
6. Verify the scan tool MAP Sensor parameter is less than 0.5 V.
7. Install a 3 A fused jumper wire between the signal circuit terminal 3 and the 5 V reference circuit terminal 1.
8. Ignition ON, verify the scan tool MAP voltage parameter is greater than 4.5 V.
9. Test or replace the B74 Manifold Absolute Pressure Sensor.
Component Testing
NOTE: You must perform the Circuit/System Testing in order to verify the integrity of the MAP Sensor circuits before proceeding with the Component Testing.
Skewed Sensor Test
1. Ignition OFF, remove the B74 Manifold Absolute Pressure Sensor from the engine. Connect the harness to the sensor, if disconnected.
2. Ignition ON.
3. Apply 17 kPa (5.0 in Hg) of vacuum to the B74 Manifold Absolute Pressure Sensor, with the GE- 23738-A.
4. Verify the scan tool MAP pressure parameter decreases between 13 - 21 kPa (1.8 - 3.0 PSI).
Replace the B74 Manifold Absolute Pressure Sensor.
5. Apply 34 kPa (10.0 in Hg) of vacuum to the B74 Manifold Absolute Pressure Sensor, with the GE-23738-A.
6. Verify the scan tool MAP pressure parameter decreases between 30 - 38 kPa (4.4 - 5.5 PSI).
Replace the B74 Manifold Absolute Pressure Sensor.
7. All OK.
Erratic Signal Test
1. Ignition OFF, remove the B74 Manifold Absolute Pressure Sensor and disconnect the harness.
2. Install a 3 A fused jumper wire between the 5 V reference circuit terminal 1 of the sensor and the sensor harness.
3. Install a jumper wire between the low reference circuit terminal 2 of the sensor and ground.
4. Install a jumper wire to the signal circuit terminal 3 of the sensor.
5. Connect a DMM between the jumper wire and ground.
6. Ignition ON, observe the DC voltage on the DMM. Slowly apply between 0 - 15 kPa (0 - 4.4 in Hg) of vacuum to the sensor with the GE-23738-A.
7. Verify the voltage changes, without any spikes or dropouts and is between 0.2 - 4.9 V.
Replace the B74 Manifold Absolute Pressure Sensor.
8. All OK.
Repair Instructions
Perform the Diagnostic Repair Verification after completing the repair.