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EVAP System Monitor Component Checks

Additional malfunctions that are identified as part of the evaporative system integrity check are as follows:

The Canister Purge Valve (CPV) output circuit is checked for opens and shorts (P0443)

NOTE:

Note that a stuck closed CPV generates a P0455, a leaking or stuck open CPV generates a P1450.

CANISTER PURGE VALVE CHECK OPERATION:

DTCs P0443 - Evaporative Emission System Purge Control Valve "A" Circuit
Monitor execution continuous
Monitor Sequence None
Sensors OK not applicable
Monitoring Duration 5 seconds to obtain smart driver status
TYPICAL CANISTER PURGE VALVE CHECK MALFUNCTION THRESHOLDS:

P0443 (CPV): open/shorted at 0 or 100% duty cycle

The Canister Vent Solenoid  output circuit is checked for opens and shorts (P0446), a stuck closed CVS generates a P1450, a leaking or stuck open CVS generates a P0455.

CANISTER VENT SOLENOID CHECK OPERATION:

DTCs P0446 - Canister Vent Solenoid Circuit
Monitor execution continuous
Monitor Sequence None
Sensors OK not applicable
Monitoring Duration 5 seconds to obtain smart driver status
TYPICAL CANISTER VENT SOLENOID CHECK MALFUNCTION THRESHOLDS:

P0446 (Canister Vent Solenoid Circuit): open/shorted

The Evap Switching Valve (EVAPSV)  output circuit is checked for opens and shorts (P2418).

EVAP SWITCHING VALVE CHECK OPERATION:

DTCs P2418 - Evap Switching Valve Circuit
Monitor execution continuous
Monitor Sequence None
Sensors OK not applicable
Monitoring Duration 5 seconds to obtain smart driver status
EVAP SWITCHING VALVE CHECK MALFUNCTION THRESHOLDS:

P2418 (Evap Switching Valve Circuit): open/shorted

The Fuel Tank Pressure Sensor  input circuit is checked for out of range values (P0452 short, P0453 open), noisy readings (P0454 noisy) and an offset (P0451 offset).

NOTE:

Note that an open power input circuit or stuck check valve generates a P1450.

FUEL TANK PRESSURE SENSOR TRANSFER FUNCTION

FTP volts = [ Vref * (0.14167 * Tank Pressure) + 2.6250 ] / 5.00
Volts  A/D Counts in PCM  Fuel Tank Pressure, Inches H 2  O 
0.100 20 -17.82
0.500 102 -15.0
1.208 247 -10.0
2.625 464 0
3.475. 712 6.0
4.750 973 15.0
4.90 1004 16.06
FUEL TANK PRESSURE SENSOR CHECK OPERATION:

DTCs P0452 - Fuel Tank Pressure Sensor Circuit Low
P0453 - Fuel Tank Pressure Sensor Circuit High
P0454 - Fuel Tank Pressure Sensor Intermittent/Erratic (noisy)
Monitor execution continuous
Monitor Sequence None
Sensors OK not applicable
Monitoring Duration 5 seconds for electrical malfunctions, 10 seconds for noisy sensor test
TYPICAL FUEL TANK PRESSURE SENSOR CHECK MALFUNCTION THRESHOLDS:

P0452 (Fuel Tank Pressure Sensor Circuit Low): < -17.82 in H2 O
P0453 (Fuel Tank Pressure Sensor Circuit High): > 16.06 in H2 O
P0454 (Fuel Tank Pressure Sensor Circuit Noisy): > open circuit, short circuit or > 4 in H2 O change between samples, sampled every 100 msec
FUEL TANK PRESSURES SENSOR OFFSET CHECK OPERATION

DTCs P0451 - Fuel Tank Pressure Sensor Range/Performance (offset)
Monitor execution once per driving cycle
Monitor Sequence No P0443 or P1450 DTCs
Sensors OK not applicable
Monitoring Duration < 1 second
TYPICAL FUEL TANK PRESSURE SENSOR OFFSET CHECK ENTRY CONDITIONS:

Entry Condition  Minimum  Maximum 
Ignition key on, engine off, engine rpm   0 rpm
Purge Duty Cycle   0%
Engine off (soak) time 4 - 6 hours  
Fuel Tank Pressure Sensor Variation during test   0.5 in H2 O
Battery Voltage 11.0 volts  
TYPICAL FUEL TANK PRESSURE SENSOR OFFSET CHECK MALFUNCTION THRESHOLDS:

Fuel tank pressure at key on, engine off is 0.0 in H2 O +/- 2.0 in H2 O

The Fuel Level Input  is checked for out of range values (opens/ shorts). The FLI input is obtained from the serial data link from the instrument cluster. If the FLI signal is open or shorted, the appropriate DTC is set (P0462 circuit low and P0463 circuit high).

Vehicles with a "saddle tank" (a tank that wraps over the axle) have two fuel level senders. The FLI input is obtained from the serial data link from the instrument cluster. If the FLI signal is open or shorted, the appropriate DTC is set (P2067 circuit low and P2068 circuit high). A "jet pump" pumps fuel from the passive side of the saddle tank to the active side of the saddle tank where the main fuel pump supplies the engine with fuel. This means that the active side of the fuel tank typically has a high fuel level reading because it constantly filled by the jet pump. For purposes of computing vehicle fuel level, the two FLI readings are averaged together into one signal that represents the combined fuel level.

Finally, the Fuel Level Input is checked for noisy readings. If the FLI input continues to change > 40% between samples, a P0461 DTC is set.

FUEL LEVEL INPUT CHECK OPERATION:

DTCs P0461 - Fuel Level Sensor A Circuit Noisy
P0462 - Fuel Level Sensor A Circuit Low
P0463 - Fuel Level Sensor A Circuit High
P2067 - Fuel Level Sensor B Circuit Low
P2068 - Fuel Level Sensor B Circuit High
Monitor execution continuous
Monitor Sequence None
Sensors OK not applicable
Monitoring Duration 30 seconds for electrical malfunctions,
TYPICAL FUEL LEVEL INPUT CHECK MALFUNCTION THRESHOLDS:

P0460 or P0462 (Fuel Level Input Circuit Low): < 5 ohms (< 1 A/D count)
P0460 or P0463 (Fuel Level Input Circuit High): > 200 ohms (>253 A/D counts)
P0461 (Fuel Level Input Noisy): > 40% change between samples, > 100 occurrences, sampled every 0.100 seconds

The FLI signal is also checked to determine if it is stuck. "Fuel consumed" is continuously calculated based on PCM fuel pulse width summation as a percent of fuel tank capacity. (Fuel consumed and fuel gauge reading range are both stored in KAM and reset after a refueling event or DTC storage.) If the there is an insufficient corresponding change in fuel tank level, a P0460 DTC is set.

Different malfunction criteria are applied based on the range in which the fuel level sensor is stuck.

In the range between 15% and 85%, a 30% difference between fuel consumed and fuel used is typical. The actual value is based on the fuel economy of the vehicle and fuel tank capacity.

In the range below 15%, a 40% difference between fuel consumed and fuel used is typical. The actual value is based on reserve fuel in the fuel tank and the fuel economy of the vehicle.

In the range above 85%, a 60% difference between fuel consumed and fuel used is typical. The actual value is based on the overfill capacity of the fuel tank and the fuel economy of the vehicle. Note that some vehicles can be overfilled by over 6 gallons.

FUEL LEVEL INPUT STUCK CHECK OPERATION:

DTCs P0460 - Fuel Level Input Circuit Stuck
Monitor execution continuous
Monitor Sequence None
Sensors OK not applicable
Monitoring Duration Between 15 and 85%, monitoring can take from 100 to 120 miles to complete
TYPICAL FUEL LEVEL INPUT STUCK CHECK MALFUNCTION THRESHOLDS:

P0460 (Fuel Level Input Stuck):
Fuel level stuck at greater than 90%: > 60% difference in calculated fuel tank capacity consumed versus change in fuel level input reading
Fuel level stuck at less than 10%: > 30% difference in calculated fuel tank capacity consumed versus change in fuel level input reading
Fuel level stuck between 10% and 90%: > 25% difference in calculated fuel tank capacity consumed versus change in fuel level input reading

The Evap Monitor Microprocessor  is checked for proper microprocessor operation or loss of CAN communication with the main microprocessor (P260F). Applies only if EONV is in separate microprocessor.

EVAP MONITOR MICROPROCESSOR PERFORMANCE:

DTCs P260F - Evap System Monitoring Processor Performance
Monitor Execution continuous
Monitor Sequence None
Sensor OK not applicable
Monitoring Duration 5 seconds

Evap Switching Valve (EVAPSV) Diagnostics 

The Evap Switching Valve (EVAPSV) is included on HEV applications for 2009 Model Year. It is very similar to the Fuel Tank Isolation Valve (FTIV) used in previous model years. The Evap Switching Valve is also known as a Vapor Blocking Valve (VBV). The purpose of the EVAPSV is to isolate the fuel tank from the rest of the evaporative system so that the Canister Purge Valve (CPV) can purge more aggressively with minimal risk of purge vapor slugs being ingested into the intake.

The EVAPSV is normally closed during engine operation, but may vent during a drive to relieve positive pressure. The exact pressure points at which the valve opens and closes are vehicle dependent. When the vehicle is in a key-off state, the EVAPSV is not powered and the valve is open.

The VBV circuit and functional diagnostics will set the following DTCs:

P2418 - EVAPSV circuit fault

P2450 - EVAPSV stuck open fault

The EVAPSV circuit diagnostics are very similar to that of the Canister Purge Valve (CPV) and Canister Vent Solenoid (CVS). See Evap System Monitor Component Checks below.

A diagram of an evaporative system with an EVAPSV (shown as a VBV) is shown below:

Fig 1: Mode $06 Evaporative System Diagram
G00574725Courtesy of FORD MOTOR CO.

The Evaporative System monitor performs a functional check of the EVAPSV in Phase 3 of the evap monitor cruise tests if the 0.040" leak test passes. At the end of Phase 2, tank pressure will be in the range of -8 to -5 "H2 0 and the EVAPSV will be open. At the beginning of Phase 3, the EVAPSV is commanded closed and the CVS is commanded open. If the EVAPSV fails to close, there will be a rapid pressure loss in the fuel tank. If this pressure loss exceeds a calibrated threshold, a P2450 DTC is set. (Requires 2 or 3 failures in a row during a driving cycle (calibratable)). If the fault is present on a second driving cycle, the MIL will be illuminated.

EVAP SWITCHING VALVE (EVAPSV) MONITOR OPERATION:

DTCs P2450
Monitor Execution once per driving cycle
Monitor Sequence Run after evap 0.040" cruise test
Sensors/Components OK MAF, IAT, VSS, ECT, TP, FTP, CPV, CVS
Monitoring Duration 30 seconds (see disablement condition below)
TYPICAL EVAP SWITCHING VALVE (EVAPSV) MONITOR ENTRY CONDITIONS:

Entry Condition  Minimum  Maximum 
0.040" Cruise Test completes    
TYPICAL EVAP SWITCHING VALVE (EVAPSV) ABORT CONDITIONS:

Change in fuel fill level: > 15%
TYPICAL EVAP SWITCHING VALVE (EVAPSV) MALFUNCTION THRESHOLDS:

P2418: Presence of short, open, or intermittent fault for more than 5 seconds
P2450: Pressure loss > 3" H2 0 during phase 3.
J1979 EVAPORATIVE SYSTEM MODE $06 DATA

Test ID  Comp ID  Description  Units 
$3D $82 Vapor blocking valve performance (P2450) Pa
NOTE: Default values (0.0 Pa) will be displayed for all the above TIDs if the evap monitor has never completed. Each TID is associated with a particular DTC. The TID for the appropriate DTC will be updated based on the current or last driving cycle, default values will be displayed for any phases that have not completed.

Blocked Purge Line Diagnostics 

If an in-line Fuel Tank Pressure Transducer is used, it is possible for a blockage to occur between the Fuel Tank Pressure Transducer (FTPT) and fuel tank. If this occurs, the evap monitor would run and pass all leak check diagnostics even if there is a leak at the fuel cap. (The blockage will make the system look sealed despite the leak.). The blocked line diagnostic looks for a rapid drop in pressure during Phase 0 of the cruise test. This rapid pressure drop occurs because the Canister Purge Valve (CPV) applies a vacuum to just the canister and evap lines. Upon seeing an excessively fast pressure drop in Phase 0, the evap monitor will invoke a special execution of Phase 3 & 4 where a CPV pressure pulse is applied to the evap system. This pressure pulse is at a very low flow and short duration (0.5 -1.0 seconds) to avoid driveability issues. If this intrusive test fails, the Phase 0 test and the intrusive test are repeated 2 or 3 times prior to setting a P144A DTC.

Diagram of an evaporative system with a blockage is shown below:

Fig 2: Mode $06 Data Evaporative System With Blockage Diagram
G00547726Courtesy of FORD MOTOR CO.
EVAP BLOCKED LINE MONITOR OPERATION:

DTC P144A
Monitor execution once per drive cycle
Monitor Sequence Runs during Phase 0 of evap 0.040" cruise test. Performs an intrusive test in Phase 3 & 4 to confirm a fault.
Sensor/Components OK MAF, IAT, VSS, ECT, CKP, TP, FTP, CPV, CVS
Monitoring Duration 30 seconds (see disablement conditions below)
TYPICAL BLOCKED LINE MONITOR ENTRY CONDITIONS:

Entry condition  Minimum  Maximum 
General 0.040" Cruise Test conditions apply    
Air mass high enough for intrusive portion of test 1.5 (lb/min)  
Manifold vacuum high enough for intrusive portion of test 5 "Hg  
Not in open loop fueling    
CPV purging    
TYPICAL EVAP BLOCKED LINE ABORT CONDITIONS:

All items cited under entry conditions apply.
TYPICAL EVAP BLOCKED LINE MALFUNCTION THRESHOLDS:

P144A: Phase 0 portion of test delta pressure < -5 "H2 0/sec
P144A: Phase 3 & 4 (intrusive test) pressure response < -2 "H2 0
J1979 EVAPORATIVE SYSTEM MODE $06 DATA

Test ID  Comp ID  Description  Units 
$3D $80 Blocked Evap System Line - Screening test (P144A) Pa/sec
$3D $81 Blocked Evap System Line - Fault confirmation test (P144A) Pa
NOTE: Default values (0.0) will be displayed for all the above TIDs if the evap monitor has never completed. Each TID is associated with a particular DTC. The TID for the appropriate DTC will be updated based on the current or last driving cycle, default values will be displayed for any phases that have not completed.

Single Path Purge Check Valve Diagnostics 

Boosted applications use a mechanical check valve between the intake manifold and the Canister Purge Valve (CPV). The purpose of this check valve is to prevent reverse flow through the evaporative emissions system under boosted conditions. The check valve is a simple diaphragm type valve were the rubber diaphragm slides inside a cylinder and is pushed against a stop under boost closing off flow through the valve. While at atmosphere or under vacuum the valve is pulled off the stop allowing flow from the evaporative system to the intake manifold. The check valve diagnostic looks for a failed open, improperly installed, or missing valve that could result in intake manifold vapors being pushed back into the evaporative emissions system (see figure below). A failed check valve is detected if the rate of rise in Fuel Tank Pressure Sensor is greater than a calibratable threshold while the Canister Vent Valve is closed, Canister Purge Valve open, and the engine is boosted above a minimum level (under boost the system should be sealed if the check valve is operating properly). This condition will set DTC P144C.

Figure: System schematic showing the potential for reverse flow if the check valve is failed.

Fig 3: Mode $06 Data System Failed Check Valve Schematic
G00574727Courtesy of FORD MOTOR CO.
EVAPORATIVE SYSTEM PURGE CHECK VALVE PERFORMANCE DIAGNOSTIC OPERATION:

DTC P144C Evaporative Emission System Purge Check Valve Performance
Monitor execution Once per drive cycle, during boosted operation
Monitor Sequence None
Sensor/Component OK ECT/CHT, IAT, MAP, CPV, FTPT, FLI, BARO, TIP
Monitoring Duration 5 to 10 seconds depending on level of boost
TYPICAL EVAPORATIVE SYSTEM PURGE CHECK VALVE PERFORMANCE ENTRY CONDITIONS

Entry Condition  Minimum  Maximum 
Ambient temperature 40 °F 95 °F
Battery Voltage 11.0 Volts  
Fuel Level 15% 85%
Engine Coolant Temperature (CHT/ECT) 160 °F  
Atmospheric Pressure (BARO) 23" Hg  
Boost Pressure (MAP - BARO) 4 to 8" Hg  
Engine Delta Load 0.2  
Vehicle Acceleration 0.5 mph/sec  
TYPICAL EVAPORATIVE SYSTEM PURGE CHECK VALVE DIAGNOSTIC MALFUNCTION THRESHOLDS:

Pressure Rise Rate (delta pressure / delta time) > 0.50 " H2 O/sec
Threshold is a function of fuel level with a range of 0.5 to 1.0

Dual Path Purge Check Valve Diagnostics 

Boosted applications that have a lower power-to-weight ratio use two purge flow paths to allow purge under boost conditions in addition to normal vacuum conditions.

Dual path purge applications use a mechanical check valve 1 (CV1) between the intake manifold and the Canister Purge Valve (CPV). During non-boosted conditions, purge vapors go through check valve 1 before entering the intake. The purpose of this check valve is to prevent reverse flow through the evaporative emissions system under boosted conditions. The check valve is a simple diaphragm type valve were the rubber diaphragm slides inside a cylinder and is pushed against a stop under boost closing off flow through the valve.

A second identical check valve 2 (CV2) is used to facilitate purging during boost. During boosted conditions, a venturi device, called an ejector, is used to generate the needed vacuum for purging. The purge vapors flow through CV2, the turbo charger, and the charge air cooler before entering the intake manifold.

The check valve diagnostic looks for a failed open CV1, a failed closed CV2, a failed ejector, an improperly installed CV1 or CV2, or missing CV1 that could result in intake manifold vapors being pushed back into the evaporative emissions system or lack of purge under boost.

Fig 4: Mode $06 Data Dual-Path Purge For Turbo DI Engines
G00574728Courtesy of FORD MOTOR CO.

A failed CV1 is detected if the rate of rise in Fuel Tank Pressure Sensor is greater than a calibratable threshold while the Canister Vent Valve is closed, Canister Purge Valve open, and the engine is boosted above a minimum level. Under boost, the system should be sealed if the check valve is operating properly. This condition will set DTC P144C.

A failed CV2 is detected if the rate of change of ejector generated vacuum is relatively flat within a threshold window during boosted conditions. This will set DTC P144C. Steep vacuum slopes for CV2 are indicative of good functioning valves. See the figure below for CV1/CV2 pass and fail ranges.

Fig 5: Mode $06 Data CV1, CV2 Pass and Fail Ranges
G00574729Courtesy of FORD MOTOR CO.
EVAPORATIVE SYSTEM PURGE CHECK VALVE PERFORMANCE DIAGNOSTIC OPERATION:

DTC P144C - Evaporative Emission System Purge Check Valve Performance
Monitor execution Once per driving cycle, during boosted operation
Monitor Sequence None
Sensors/Components OK ECT/CHT, IAT, MAP, CPV, CVV, FTPT, FLI, BARO, TIP, WASTEGATE
Monitoring Duration 5 to 10 seconds depending on level of boost
TYPICAL EVAPORATIVE SYSTEM PURGE CHECK VALVE PERFORMANCE ENTRY CONDITIONS

Entry Condition  Minimum  Maximum 
Ambient air temperature 40 °F 105 °F
Battery Voltage 11.0 Volts  
Fuel level 15% 90%
Engine Coolant Temperature 160 °F  
Atmospheric Pressure (BARO) 23" Hg  
Boost Pressure (MAP - BARO) 8" Hg  
TYPICAL EVAPORATIVE SYSTEM PURGE CHECK VALVE DIAGNOSTIC MALFUNCTION THRESHOLDS:

CV1- Pressure Rise Rate (delta pressure / delta time) > 1 " H2 O/sec
CV1- Threshold is a function of fuel level with a range of 1.5 to 2.6
CV2- Vacuum Rate (delta vacuum / delta time) >-0.4 and < 0.5 H2 O/sec
CV2- Threshold is a function of fuel level with a range of 0.5 to 0.7 for the upper band and -0.4 to -0.3 for the lower band