Part 3
2AZ-FXE ENGINE CONTROL SYSTEM: SFI SYSTEM: P043E,P043F,P2401,P2402,P2419: Evaporative Emission System Reference Orifice Clog Up - Continued
DTC P043E - Evaporative Emission System Reference Orifice Clog Up
DTC P043F - Evaporative Emission System Reference Orifice High Flow
DTC P2401 - Evaporative Emission Leak Detection Pump Stuck OFF
DTC P2402 - Evaporative Emission Leak Detection Pump Stuck ON
DTC P2419 - Evaporative Emission System Switching Valve Control Circuit Low
31. REPAIR OR REPLACE HARNESS OR CONNECTOR
NEXT -- PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK AGAIN (AUTOMATIC OPERATION))
32. REPAIR OR REPLACE VACUUM HOSE
NEXT -- PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK AGAIN (AUTOMATIC OPERATION))
33. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION))
HINT: In the manual operation check, the EVAP system can be checked in signal steps. Valve operation and pressure in each step can also be checked.
(a) Clear the DTCs DTC Check / Clear.
(b) Remove the fuel tank cap and reinstall the fuel cap.
(c) Enter the following menus: Powertrain / Engine / Utility / Evaporative System Check / Manual Mode.
NOTICE:
- In Evaporative System Check (Manual Mode), the series of 9 Evaporative System Check steps is performed automatically. It takes a maximum of approximately 18 minutes.
- Do not perform Evaporative System Check when the fuel tank is more than 90% full because the cut-off valve may be closed, making the leak check of the fuel tank unavailable.
- Do not run the engine in this step.
- When the temperature of the fuel is 35°C (95°F) or more, a large amount of vapor forms and any check results become inaccurate. When performing Evaporative System Check, keep the temperature below 35°C (95°F).
Tester Display
Manual Operation Step
- Timing Chart
NEXT -- Continue to next step.
34. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 1))
(a) Select step 1 and wait 10 seconds.
NEXT -- Continue to next step.
35. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 2))
(a) Perform step 2.
(b) Check the EVAP pressure 2 seconds after the leak detection pump is activated*.
*: The leak detection pump begins to operate at the start of step 2.
(c) Check the EVAP pressure again when it has stabilized. This pressure is the first reference pressure standard.
Result:
C -- REPLACE CANISTER ASSEMBLY
B -- PERFORM ACTIVE TEST USING TECHSTREAM (VACUUM PUMP)
A -- Continue to next step.
36. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 3))
(a) Perform step 3.
(b) Check the EVAP pressure change in step 3.
Result:
(c) Check the fuel tank pressure change in step 3.
Result:
(d) Check the EVAP pressure again when it has stabilized. This pressure is the canister leak pressure standard.
(e) Compare the first reference pressure with the canister leak pressure.
Result:
D -- LOCATE EVAP LEAK PART (PURGE VSV - CANISTER)
C -- CHECK FUEL VAPOR-CONTAINMENT VALVE ASSEMBLY (POWER SOURCE CIRCUIT)
B -- INSPECT CANISTER PUMP MODULE (VENT VALVE OPERATION)
A -- Continue to next step.
37. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 4))
(a) Perform step 4.
(b) Check the EVAP pressure change in step 4.
Result:
B -- CHECK VACUUM HOSE (PURGE VSV - INTAKE MANIFOLD)
A -- Continue to next step.
38. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 5))
(a) Perform step 5 and wait 60 seconds.
(b) Check the EVAP pressure. This pressure is the second reference pressure standard.
NEXT -- Continue to next step.
39. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 6))
(a) Perform step 6 and wait 5 seconds.
NEXT -- Continue to next step.
40. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 7))
(a) Perform step 7.
(b) Check that the tank pressure and EVAP pressure change.
(c) Check the tank pressure again when it has stabilized. This pressure is the fuel tank leak pressure standard.
Result:
B -- CHECK FUEL VAPOR-CONTAINMENT VALVE ASSEMBLY (POWER SOURCE CIRCUIT)
A -- Continue to next step.
41. PERFORM SYSTEM CHECK (EVAPORATIVE SYSTEM CHECK (MANUAL OPERATION STEP 8))
(a) Perform step 8 and wait 60 seconds.
(b) Check the EVAP pressure. This pressure is the third reference pressure standard.
(c) Compare the tank pressure checked in step 8 with the third reference pressure.
Result:
B -- CHECK FUEL TANK CAP ASSEMBLY
A -- Continue to next step.
42. PERFORM CONFIRMATION DRIVING PATTERN
(a) KEY-OFF MONITOR DRIVE PATTERN
(1) Connect the Techstream to the DLC3.
(2) Confirm the following conditions are satisfied:
- The fuel level is less than 90%.
- The altitude is less than 8,000 ft. (2,400 m).
- The vehicle is stopped (the vehicle speed is less than 2 mph).
- The ECT is 4.4 to 35°C (40 to 95°F.)
- The IAT is 4.4 to 35°C (40 to 95°F).
- Drive the vehicle in a city area or on free-way for 10 minutes or more.
(3) Perform the drive pattern:
1. Allow the engine to idle for 5 minutes or more.
2. Turn the power switch off and wait 6 hours.
(4) Check the monitor status with the Techstream.
(b) PURGE FLOW MONITOR DRIVE PATTERN (P0441)
(1) Connect the Techstream to the DLC3.
(2) Confirm that the following conditions are satisfied:
- The Engine Coolant Temperature (ECT) is more than 4.4°C (40°F).
- The Intake Air Temperature (IAT) is more than 4.4°C (40°F).
(3) Perform the drive pattern:
1. Remove and reinstall the fuel cap to release the fuel tank pressure.
2. Warm up the engine until the ECT reaches 75°C (167°F) or more.
3. Drive vehicle in a city area or on free-way for 10 minutes or more.
(4) Check the monitor status with the Techstream.
NEXT -- PERFORM EVAP SYSTEM (EVAPORATIVE SYSTEM CHECK AGAIN (AUTOMATIC OPERATION))
MONITOR DESCRIPTION
In sequence B and E, the leak detection pump creates negative pressure (vacuum) through the reference orifice. The EVAP system pressure is then measured by the ECM (included in the hybrid vehicle control ECU), using the canister pressure sensor, to determine the reference pressure. If the pressure is one of the following conditions, the ECM illuminates the MIL and sets the DTC (2-trip detection logic).
- Canister pressure is lower than the malfunction criterion (ex. 724 mmHg).
- Canister pressure is higher than the malfunction criterion (ex. 752 mmHg).
- Canister pressure is not saturated within 60 seconds.
- Canister pressure difference of sequence B and sequence E is large.
MONITOR STRATEGY
TYPICAL ENABLING CONDITIONS
Example of restart time
Key-off monitor sequence 1 to 15
1. Atmospheric pressure measurement
2. First reference pressure measurement
3. Vent valve stuck closed check
4. Vacuum introduction for canister
5. Purge VSV stuck closed check
6. Second reference pressure measurement
7. Canister leak
8. Fuel vapor-containment valve (FVCV stuck closed check)
9. Vacuum introduction for fuel tank
10. FVCV stuck closed check
11. FTP sensor stuck check
12 Third reference pressure measurement
13. Fuel tank leak check
14. FTP sensor stuck check
15. Atmospheric pressure measurement
TYPICAL MALFUNCTION THRESHOLDS
"Saturated" indicates that the EVAP pressure change is less than 0.1 kPa (0.75 mmHg) in 30 seconds.
MONITOR RESULT
Refer to CHECKING MONITOR STATUS Mode 6 Data.