DESCRIPTION The manifold
absolute pressure sensor installed to the intake manifold detects the
intake manifold pressure using a built-in sensor. An
atmospheric pressure sensor is built in the ECM. When the engine is
stopped, the value of the manifold absolute pressure sensor and
atmospheric pressure sensor will be approximately the same as the
atmospheric pressure.
DTC No. | Detection Item |
DTC Detection Condition | Trouble Area |
MIL | Memory |
Note | P006900 |
Manifold Absolute Pressure - Barometric Pressure Correlation |
Difference
between atmospheric pressure value of the absolute pressure sensor and
atmospheric pressure sensor is higher than threshold value (2 trip
detection logic). |
- Manifold absolute pressure sensor
- ECM
| Comes on |
DTC stored | SAE Code: P0069 | MONITOR DESCRIPTION
Approximately
50 minutes after the power switch is turned off, the soak timer is
activated and the values of the manifold absolute pressure sensor and
atmospheric pressure sensor are compared. If the difference between the
values of the manifold absolute pressure sensor and atmospheric pressure
sensor is higher than a threshold value in consecutive driving cycles,
the ECM will store this DTC. MONITOR STRATEGY
Related DTCs | P0069: Manifold absolute pressure sensor/Atmospheric pressure sensor correlation |
Required Sensors/Components (Main) | Manifold absolute pressure sensor
ECM | Required Sensors/Components (Related) |
Mass air flow meter sub-assembly Engine coolant temperature sensor |
Frequency of Operation | Once per driving cycle |
Duration | 3 times |
MIL Operation | 2 driving cycles |
Sequence of Operation | None | TYPICAL ENABLING CONDITIONS
All of the following conditions are met |
- | Engine coolant temperature |
-10°C (14°F) or higher |
Intake air temperature |
-10°C (14°F) or higher |
Atmospheric pressure sensor circuit fail (P2228, P2229) |
Not detected |
Manifold absolute pressure sensor circuit fail (P0107, P0108) |
Not detected |
Engine coolant temperature sensor circuit fail (P0117, P0118) |
Not detected |
Intake air temperature sensor circuit fail (P0112, P0113) |
Not detected |
Engine | Stall |
Power switch | Off |
Soak time | 50 minutes |
Time after ECM power on |
60 to 65.625 seconds |
Auxiliary battery voltage |
8 V or higher | TYPICAL MALFUNCTION THRESHOLDS
Atmospheric pressure and manifold absolute pressure deviation |
Higher than 15.297 kPa (2.218 psi) | 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.
Click here
- When clearing the permanent DTCs, refer to the "CLEAR PERMANENT DTC" procedure.
Click here
- Connect the Techstream to the DLC3.
- Turn the power switch on (IG).
- Turn the Techstream on.
- Clear the DTCs (even if no DTCs are stored, perform the clear DTC procedure).
- Turn the power switch off and wait for at least 55 minutes [A].
- Turn the power switch on (IG) [B].
- Turn the Techstream 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: P006900.
- Check the DTC judgment result.
Techstream 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:
CAUTION / NOTICE / HINT
NOTICE:
HINT: Read
Freeze Frame Data using the Techstream. 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
1. |
CHECK ANY OTHER DTCS OUTPUT (IN ADDITION TO DTC P006900) |
(a) Connect the Techstream to the DLC3. (b) Turn the power switch on (IG).
(c) Turn the Techstream on. (d) Enter the following menus: Powertrain / Engine / Trouble Codes.
(e) Read the DTCs. Powertrain > Engine > Trouble Codes
Result | Proceed to |
DTC P006900 is output |
A | DTC P006900 and other DTCs are output |
B | HINT: If any DTCs other than P006900 are output, troubleshoot those DTCs first.
B |
| GO TO DTC CHART |
A |
| |
2. |
READ VALUE USING TECHSTREAM (INTAKE MANIFOLD ABSOLUTE PRESSURE) |
(a) Turn the power switch off and wait for at least 50 minutes. (b) Connect the Techstream to the DLC3.
(c) Turn the power switch on (IG). (d) Turn the Techstream on. (e) Enter the following menus: Powertrain / Engine / Data List / Intake Manifold Absolute Pressure. Powertrain > Engine > Data List
Tester Display | Intake Manifold Absolute Pressure |
(f) Using the following table, determine the normal atmospheric pressure for the current altitude and temperature.
HINT:
- Standard atmospheric pressure is approximately 101 kPa(abs) [15 psi(abs)].
- For every 100 m (328 ft.) increase in altitude, atmospheric pressure
drops by approximately 1 kPa (0.1 psi). This varies depending on the
weather.
(g) Compare the value of the Data List item Intake Manifold Absolute Pressure with the actual atmospheric pressure.
Result | Proceed to |
Approximately the same as the actual atmospheric pressure |
A | Not approximately the same as the actual atmospheric pressure |
B |
B |
| REPLACE MANIFOLD ABSOLUTE PRESSURE SENSOR |
A |
| |
3. |
READ VALUE USING TECHSTREAM (ATMOSPHERIC PRESSURE) |
(a) Connect the Techstream to the DLC3. (b) Turn the power switch on (IG).
(c) Turn the Techstream on. (d) Enter the following menus: Powertrain / Engine / Data List / Atmospheric Pressure. Powertrain > Engine > Data List
Tester Display | Atmospheric Pressure |
(e) Using the following table, determine the normal atmospheric pressure for the current altitude and temperature.
HINT:
- Standard atmospheric pressure is approximately 101 kPa(abs) [15 psi(abs)].
- For every 100 m (328 ft.) increase in altitude, atmospheric pressure
drops by approximately 1 kPa (0.1 psi). This varies depending on the
weather.
(f) Compare the value of the Data List item Atmospheric Pressure with the actual atmospheric pressure.
Result | Proceed to |
Approximately the same as the actual atmospheric pressure |
A | Not approximately the same as the actual atmospheric pressure |
B |
A |
| CHECK FOR INTERMITTENT PROBLEMS |
B |
| REPLACE ECM | |