AML EOBD System Operation Summary
Rory O’Curry Aston Martin Lagonda CONFIDENTIAL 1 May 2009
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Comprehensive Component Monitor - Automatic Transmission
General
The MIL is illuminated for all emissions related electrical component malfunctions. For malfunctions
attributable to a mechanical component (such as a clutch, gear, band, valve, etc.), some transmissions are
capable of not commanding the mechanically faile d component and providing the remaining maximum
functionality (functionality is reassessed on each power up). In such case a non-MIL Diagnostic Trouble
Code (DTC) will be stored and, if so equipped, a Transmission Control Indicator Light (TCIL) will flash.
For example on the CD4E transmission, if a gear ratio is not properly obtained and verified due to a
mechanical malfunction, the unobtainable gear is no longer commanded for that power up, the DTC is
stored and the TCIL flashes.
Transmission Inputs
Transmission Range Sensor Check Operation:
DTCs P0705, P0708 (open/invalid pattern for digital TRS)
P0707, P0708 (opens/shorts for analog TRS)
Monitor execution continuous
Monitor Sequence none
Monitoring Duration 30 seconds
Typical TRS check entry conditions : Minimum Maximum
Gear selector position each position for up to 30 seconds 480 seconds
Typical TRS malfunction thresholds:
For digital sensor : Invalid pattern from 3 (or 5) digital inputs or 1 analog circuit open for 5 seconds
For analog sensor : Voltage > 4.8 volts or < 0.2 voltage for 5 seconds
Output Shaft Speed Sensor Functional Check Operation:
DTCs P0720
Monitor execution continuous
Monitor Sequence none
Monitoring Duration 30 seconds
Typical OSS functional check entry conditions : Minimum Maximum
Gear selector position drive
Engine rpm (above converter stall speed) OR 3000 rpm
Turbine shaft rpm (if available) OR 1500 rpm
Output shaft rpm 650 rpm
Vehicle speed (if available) 15 mph
Typical OSS functional check malfunction thresholds:
Vehicle is inferred to be moving with positive driving torque and OSS < 100 to 200 rpm for 5 seconds
AML EOBD System Operation Summary
Rory O’Curry Aston Martin Lagonda CONFIDENTIAL 1 May 2009
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Transmission Outputs
Shift Solenoid Check Operation:
DTCs SS A - P0750 electrical, P1714 ISIG functional,
SS B - P0755 electrical, P1715 ISIG functional,
SS C - P0760 electrical, P1716 ISIG functional,
SS D - P0765 electrical, P1717 ISIG functional
SS E - P0770 electrical
Monitor execution electrical - continuous, functi onal - during off to on solenoid transitions
Monitor Sequence none
Typical SS malfunction thresholds:
Output driver feedback circuit does not match commanded driver state for 5 seconds.
ISIG functional check: ISIG chip hardware circu it does not detect characteristic current dip and rise
produced by solenoid movement for 10 solenoid events.
Torque Converter Clutch Check Operation:
DTCs P0743 electrical, P1740 ISIG functional
Monitor execution electrical – continuous, functi onal - during off to on solenoid transitions
Monitor Sequence none
Typical TCC malfunction thresholds:
Output driver feedback circuit does not match commanded driver state for 5 seconds
(> 1.0 volt if commanded on, < 2.0 volts if commanded off.)
ISIG functional check: ISIG chip hardware circu it does not detect characteristic current dip and rise
produced by solenoid movement.
Electronic Pressure Control Check Operation:
DTCs P1747 electrical, P1789, P0797 short to ground (low pressure)
P0745, P0775, P0795 mechanical functional
Monitor execution Continuous
Monitor Sequence None
Monitoring Duration Electrical: 5 seconds,
Mechanical functional: up to 30 seconds
Typical EPC malfunction thresholds:
Current feedback circuit is less than commanded current for 5 seconds
Transmission CCM temporary disablement conditions (other than entry requirements) :
None.
AML EOBD System Operation Summary
Rory O’Curry Aston Martin Lagonda CONFIDENTIAL 1 May 2009
[email protected] AML EOBD Monitors 07 ROC.doc Page 34 of 43
6HP26 Automatic Transmission
This transmission is operated by a stand-alone transmission control module (TCM). The MIL related
Diagnostic Trouble Codes will be transmitted via CAN to the Engine Control Module (ECM), and the
MIL illuminated, for all emissions related electrical and mechanical component malfunctions. For
malfunctions attributable to a mechanical component, this transmission may be capable of not
commanding the mechanically failed component a nd providing the remaining maximum functionality
(functionality may be reassessed on each power up). The TCM may be interrogated for transmission
information attributable to setting either code. The TCM Diagnostic Trouble Codes are addressed via a
separate document enclosed.
Auto Shift Manual (ASM) Transmission
The ASM system is based around a standard manual transmission with a clutch and mechanical selection
of a set range of gear ratios (in this case 6 speeds). In this application both clutch and gear selection
operations are controlled via a Transmission Contro l Module (TCM) which commands hydraulic actuators
based on commands from a number of inputs.
The driver actions of depressing and releasing the clutch pedal to control clutch actuation and the shifting
of gears using a gear lever have, in essence, been re placed by a TCM, hydraulic actuators and electronic
switches.
With ASM the demand to shift gears can either be direct from the driver (as in a conventional manual
transmission), or controlled automatically by the system based on parameters such as road speed, current
gear selected and throttle demand.
The MIL is illuminated for all emissions related electrical component malfunctions. For malfunctions
attributable to a mechanical component (such as a cl utch, gear, actuator, etc.), functionality is reassessed
on each power up. In such case a non-MIL or MIL Diagnos tic Trouble Code (DTC) will be stored and, if
so equipped, a Transmission Control Indicator Light will activate and/or a message will be displayed. For
example on the ASM transmission, if a gear selection is not properly obtained and verified due to a
mechanical malfunction, then the amber Transmission Control Indicator Light will activate and the
message center will display 'GEARBOX FAULT'. In addition, the powertrain MIL will activate and a
DTC will be stored. The TCM Diagnostic Trouble Cod es are addressed via a separate document enclosed.
AML EOBD System Operation Summary
Rory O’Curry Aston Martin Lagonda CONFIDENTIAL 1 May 2009
[email protected] AML EOBD Monitors 07 ROC.doc Page 37 of 43
Glossary of Terms
A/D Analogue to Digital
ASM Auto Shift Manul
BTDC Before Top Dead Centre
CALID CALibration IDentification
CD4E Automatic Transmission for Intermediate size Family saloon.
CID Camshaft Identification.
CKP Crankshaft Position
CMP Camshaft Position
COP Coil on Plug
CPC Camshaft Position Control
CVN Calibration Verification Number
DPFE Delta Pressure Feedback
DTC Diagnostic Trouble Code
ECT Engine Coolant Temperature
EDIS Electronic Distributorless Ignition System
EGR Exhaust Gas Re-circulation.
EOBD European On Bard Diagnostics
EPC Electronic Pressure Control
ETC Electronic Throttle Control
ETM Electronic Throttle Monitor
EVR Electronic Vacuum Regulator
EWMA Exponentially Weighted Moving Average
FMEM Failure Mode and Effects Management
FN Automatic Transmission for Medium size Family Saloon
FWD Front Wheel Drive
HDR High Data Rate
HO2S Heated Oxygen Sensor.
IAC Idle Air Control
IDM Ignition Diagnostic Monitor
IMRC Inlet Manifold Runner Control
IPC Independent Plausibility Checker
KAM Keep Alive Memory
LDR Low Data Rate
LTFT Long Term Fuel Trim
MAF Mass Air Flow
MAP Manifold Absolute Pressure
MIL Malfunction Indicator Lamp
OSS Output Shaft Speed
PCM Powertrain Control Module
PIP Profile Ignition Pickup
RWD Rear Wheel Drive
SAE Society of Automotive Engineers
SAIR Secondary AIR
SCV Swirl Control Valve
STFT Short Term Fuel Trim
TCC Torque Converter Clutch
TCIL Transmission Control Indicator Lamp
TP Throttle Position
TPPC Throttle Plate Position Controller
TRS Transmission Range Sensor
TSS Turbine Shaft Speed
VID Vehicle IDentification
VIN Vehicle Identification No.
VQZ VQuizzer
VMV Vapour Management Valve
Aston Martin V8 Vantage 2009 MY EOBD DocumentationAston Martin/Ford Confidential
Component/ System Fault Code Monitor Strategy
Description Malfunction Criteria Threshold Parameter Secondary Parameters Entry Parameters Time Required DTC
StorageMIL Illumin-
ation
P0300
to
P0308 Deviations in crankshaft
acceleration processed by
Neural Network Misfire
Monitor software and Catalyst
Temperature model Percentage misfire
required to exceed
Catalyst Damage
Temperature 1000 deg c
(1832 deg F) catalyst
damage threshold, per
engine bank Type A: See RPM/Load
Table FNMISPCT_97 %
Type A:
200 revs
(Continuous)Type A:
Footnote b)
Type A:
Footnote d)
Percentage misfire
required to exceed
emission thresholds Type B> 0.0323*100% Type B:
1000 revs
(Continuous)Type B/C:
Footnote a)
Type B:
Footnote c)
Percentage misfire
required to clear emission
pending code < 0.001 * 100 % Time since engine start,
value based on time and
IAT 0 + FNMISACT sec
(See Transfer Functions)
Time since PCM power up 0 sec
Time for NNMM
computation queue to fill 4 revs from initial crank
(Meets 2 rev start delay
requirement)
Engine coolant temp -7 - 115 deg C ( 20 - 240 degF )
Engine rpm 600 - 7250 rpm
Net engine torque > -81 Nm ( -60 ft lbs)
Engine torque rate of
change > -33.9Nm (-25 ft lbs/sec)
or
< 33.9Nm (25 ft lbs/sec)
Throttle position rate of
change > -30 volts/background
loop or
< 30 * 5/1024
volts/background loop
Engine rpm/load range See RPM/Load Table FNMISOK_97: Monitor
disabled when less than
0.5
Crankshaft position circuit
(PIP) OK (P0320)
Fuel shutoff for rpm or
vehicle speed limiting No fuel cutoff occurring
Fuel level > 0.15 * 100 %
Misfire Detected At
Startup P0316 Misfire detected during first
1000 engine revs since start P0316 is set in addition to
P0300 - P0308 DTC 1000 revs
(Continuous)Footnote a) Footnote c)
AICE chip failure in
PCM P0606 NNMM chip to CPU
communication fault Number of attempts 10
Continuous Footnote a) Footnote c)
Camshaft/crankshaft
synchronization
failure P1336 AICE chip reports inability to
synchronize camshaft and
crankshaft signals
(Replaces P1309) Number of attempts > 255
Continuous Footnote a) Footnote c)
Engine speed >1550rpm
<2275rpm
Engine load >0.075
<0.225
Engine coolant
temperature >68.3degC (155degF)
Transmission in 6th gear
Vehicle speed >30mph
<70mph
Maximum rate of engine
speed change <500rpm/second
In decel fuel cut
ROM checksum error P260F NNP ROM checksum error Checksum from NNP does not equal mainline
strategyNone
Continuous Footnote a) Footnote c)
Cylinder Misfire
DetectedMisfire Monitor
Footnote c)
Unable to learn
crankshaft profile P0315 Unable to learn stable
crankshaft profile Number of attempts > 6 attempts Continuous within
profile learning
entry conditionsFootnote a)
2
2009 MY OBD-II Documentation4.7L, Aston Martin V8 VantageAston Martin / Ford Confidential
1) "Continuous" under the "Time Required" column indicates that the specified test cycles at a frequency greater than once every 0.5 seconds whenever the
test entry conditions are met.
2) "Once per driving cycle" under the "Time Required" column indicates that the specified test will complete during the first 2 bags of an FTP as well as under
the test entr
y conditions specified, on the road.
3)All test entry condition parameters are measured instantaneously unless otherwise indicated.
p) If a 6 hour soak is met, some strategies will not require another continuous 6 hour soak if the customer performs a brief key-off. This has been put into
effect to improve evap monitor completion frequency.
q) Some strategies will have the ability to base evap monitor soak length on the CARB cold soak criteria which consists of an ECT range and ACT/ECT
differential.
r) A minimum soak time has been added to CARB's cold soak criteria (footnote q) to allow calibrators to set a minimum soak time if longer soak times are
n
eeded than given by the ACT/ECT-based CARB soak criteria.
a) A pending code will be stored after a malfunction has been detected on one driving cycle; a DTC will be stored after the same malfunction has been detected on the second consecutive driving cycle. The DTC will be erased after 40 warm-up cycles with no malfunction present, after the MIL has been
extinguished for the DTC.b) A DTC will be stored immediately upon detection of a malfunction. The DTC will be erased after 40 warm-up cycles with no malfunction present, after the MIL has been extinguished for the DTC.k) A DTC will be stored after a malfunction has been detected on one drive cycle.The DTC will be erased after 40 warm-up cycles with no malfunction present, after the MIL has been extinguished for that DTC.l) A DTC will be stored after a malfunction has been detected on six consecutive drive cycles. The DTC will be erased after 40 warm-up cycles with no malfunction present, after the MIL has been extinguished for that DTC.o)For intake air temperatures below 20 deg F, no DTC will set for indicated AIR malfunction.
s) A DTC will be stored after an evaporative system leak has been detected and the refueling debounce check has been completed on the subsequent
driving cycle
c)The MIL will be illuminated after a malfunction has been detected on two consecutive driving cycles.
The MIL will be extinguished after three consecutive driving cycles where the monitor was run without a malfunction.d)The MIL will blink immediately upon detection of a misfire rate that exceeds the catalyst damage threshold, regardless of whether fuel is shut off or not.
If the misfire rate drops below the catalyst damage threshold, the MIL will stay on solidly.
The MIL will be extinguished after three consecutive drive cycles where similar conditions have been seen without the malfunction.e)The MIL will be illuminated after a malfunction has been detected on two consecutive driving cycles.
The MIL will be extinguished after three consecutive drive cycles where similar conditions have been seen without the malfunction.f)For intake air temperatures below 32 deg F, the MIL will not illuminate for the indicated EGR DTCs.
For barometric pressures below 22.5"Hg, the MIL will not illuminate for the indicated EGR DTCs.
For intake air temperatures below 20 deg F, the MIL will not illuminate for the indicated AIR DTCs.
This prevents false MIL illumination due to ice in the EGR hoses or AIR switching valve(s).g)This monitor employs EWMA.
The MIL will be illuminated after a malfunction has been detected on two consecutive driving cycles after DTCs have been erased or Keep Alive Memory
h
as been erased (battery disconnect).
The MIL will be illuminated after a malfunction has been detected on up to six consecutive driving cycles during subsequent, "normal" customer driving.
The MIL will be extinguished after up to six consecutive driving cycles without a malfunction.
h) Some automatic transmission monitors are demonstrated following the USCAR Abbreviated On-Board Diagnostic Test Procedure for Vehicles Equipped
wi
th Automatic Transmissions.
This prevents false MIL illumination on this non-turbine speed sensor transmission application.
i)The MIL will be illuminated after a malfunction has been detected on the first driving cycle.
The MIL will be extinguished after three consecutive driving cycles where the monitor was run without a malfunction.j)A DTC will be set after a malfunction has been detected on two consecutive driving cycles.
m) MIL will be illuminated after a malfunction has been detected on two consecutive driving cycles. MIL will be extinguished after the monitor has run
wi
thout a malfunction (same or subsequent drive cycle).
n) A check cap light will be illuminated after a malfunction has been detected on one driving cycle. The check cap light will be extinguished after the monitor
h
as run without a malfunction (same or subsequent drive cycle).
MIL Illumination:
Notes:
Footnotes
Secondary Parameters
DTC Stora
ge:
EOBD 2009MY_V8 Vantage.xls
Notes 08/02/2005
15
Aston Martin V12 Family
2009 MY V12 Family EOBDincl. V12 Vantage
Aston Martin/Ford Confidential
The MIL will be extin
guished after three consecutive drive c
ycles where similar conditions have been seen without the malfunction.
f
)For intake air tem
peratures below 32 de
g F, the MIL will not illuminate for the indicated EGR DTCs.
For intake air tem
peratures below 20 de
g F, the MIL will not illuminate for the indicated AIR DTCs.
This
prevents false MIL illumination due to ice in the EGR hoses or AIR switchin
g valve
(s).
g)
This monitor em
ploys EWMA.
The MIL will be illuminated after a malfunction has been detected on two consecutive driving cycles after DTCs have been erased or
Kee
p Alive Memor
y has been erased
(batter
y disconnect
).
The MIL will be illuminated after a malfunction has been detected on up to six consecutive driving cycles during subsequent, "normal"
customer drivin
g.
The MIL will be extin
guished after u
p to six consecutive drivin
g cycles without a malfunction.
h) Some automatic transmission monitors are demonstrated following the USCAR Abbreviated On-Board Diagnostic Test Procedure for
Vehicles E
quipp
ed with Automatic Transmissions.
This
prevents false MIL illumination on this non-turbine s
peed sensor transmission a
pp
lication.
i
)The MIL will be illuminated after a malfunction has been detected on the first drivin
g cycle.
The MIL will be extin
guished after three consecutive drivin
g cycles where the monitor was run without a malfunction.
j)A DTC will be set after a malfunction has been detected on two consecutive drivin
g cycles.
m) MIL will be illuminated after a malfunction has been detected on two consecutive driving cycles. MIL will be extinguished after the
monitor has run without a malfunction
(same or subse
quent drive c
ycle
).
n) A check cap light will be illuminated after a malfunction has been detected on one driving cycle. The check cap light will be
extinguished after the monitor has run without a malfunction (same or subsequent drive cycle).
t) The MIL will be illuminated after a pending code has been confirmed. The MIL will be extinguished after three consecutive driving c
ycles where the monitor was run without a malfunction. This monitor em
ploye EVMA.
20
System
Component
P Codes (AML)
Malfunction Strategy Description
Malfunction Criteria
(Fault)
Fault condition
(Internal labels)
Threshold Value
(Fault condition)
Entry conditions
Entry conditions values
Filter Time to log DTC (AML)
EMS controlled MIL Illumination
(AML)
CAN LinkEngine P0725Engine speed signal
Engine Speed signal QF ≠ 3 No CAN BUS error.
No CAN level error and
No EMS timeout.600mS
1 DTC
CAN Link CAN level P0614Incorrect configuration ID received CANid does not match that stored in the TCM Engine not in crank.
No CAN BUS error
Ignition on & Timer after ignition passed.
Battery Voltage > threshold7v250mS
1 DTC
CAN Link CAN bus off P1796Monitors the CAN for Bus or RAM faults.
TCM CAN driver detects CAN bus fault. Bit, stuff, CRC or form error,
(CAN-wiring or CAN-module defective, EMC
radiation.) Battery voltage > Threshold
7v100mS1 DTC
Sensor Temperature Sensor P0711 ATF temperature sensor short circuit ATF sensor faulty - Sensor input signals (Vcgt_plus
and Vcgt_minus) out of acceptable range utmsm2_Gt
utmsm2_Gt
and
utmsm2_Gt =2.3v
utmsm1_Gt =2.7v 1.5s
2 DTC
Sensor Temperature Sensor P0711ATF Sensor - stuck value Stuck Temperature value - ATF temperature is out
of an acceptable range of tolerance when
compared to the TCM chip temperature sensor
value.
Range of tolerance is depending on the heating up
velocity of transmission . [
Fast heating = wide range of tolerance :
Chip sensor temp +/- cgt_tolwt <> ATF
temperature
OR
Slow heating = narrow range of tolerance :
Chip sensor temp +/- cgt_toleng <> ATF
temperature.]
AND
Temperature cgtf_Neu out of allowed range of
tolerance for > zgts_CgtPlausiErr * 100ms cgt_tolwt = 40degC
cgt_toleng = 25degC
AML: zgts_CgtPlausiErr= 6000 ( =
10min)
Jag+LR: zgts_CgtPlausiErr= 9000 ( =
15min)Chip sensor OK
Engine speed > threshold
Turbine speed > threshold
450rpm
450rpm1.5s
2 DTC
Sensor Temperature Sensor P0713ATF Sensor short to battery ATF sensor faulty - Sensor input signals (Vcgt_plus
and Vcgt_minus) out of acceptable range vcgt_plus > utmso_Gt
and
vcgt_minus > utmsu_Gtutmso_Gt = 4.5v
utmsu_Gt =0.5v
1.5s
2 DTC
Sensor Temperature Sensor P0712ATF Sensor short to GND ATF sensor faulty - Sensor input signals (Vcgt_plus
and Vcgt_minus) out of acceptable range vcgt_plus < utmso_Gt
and
vcgt_minus < utmsu_Gtutmso_Gt = 4.5v
utmsu_Gt =0.5v
1.5s
2 DTC
Sensor Temperature Sensor P0714ATF sensor open cct (circuit break) ATF sensor faulty - Sensor input signals (Vcgt_plus
and Vcgt_minus) out of acceptable range vcgt_plus > utmso_Gt
and
vcgt_minus < utmsu_Gtutmso_Gt = 4.5v
utmsu_Gt =0.5v
1.5s
2 DTC
Sensor Temperature Sensor P0713 ATF temperature sensor value jump
or
ATF value not warming up quickly
enough Unacceptable temperature jump (lOld value - new
value <> threshold) within a period of 100ms
or
ATF temperature (cgt_neu) not warming up quickly
enough within a specified time period
|cgt_Neu - cgta1_CUew| > cgtd1_Cuew
or
(cgt_Neu(t=tgtd_CUew) - cgt_Neu(t=0) ) <
cgtd2_Cuewcgtd1_Cuew = 20DegC
cgtd2_Cuew = 4DegC
tgtd_CUEW = 240s
Output speed > Threshold
Engine speed > Threshold
No Output speed & Engine speed error
Temperature cgt_Neu < Threshold at t=0Jag +
AML / LR
800 / 11000rpm
400 / 11000rpm
20DegC1.5s
2 DTC
TCM Internal Impossible substitute functions (monitoring contradictory
substitute functions) P0701
Two Priority 2 faults present at the same
time (Currently not possible) 20ms
2 DTC
TCM Internal Impossible substitute functions (monitoring contradictory
substitute functions) P0701
OSS fault and wheel speed faults present
concurrently (Priority 3) Wheel speed and output speed sensor faults
present concurrently. 20ms
2 DTC
TCM Internal Impossible substitute functions (monitoring contradictory
substitute functions) P0701
Bosch solenoid current monitorin
g fault 20ms 2 DTC
TCM Internal EEPROM Flash emulation P062FEEPROM emulation lifetime exceeded Communication disturbed, lifetime exceeded EEError !=0 =1
400000 Write/Erase-cycles possible. At
temperatures over 135°C no EEProm
update is made.always active
no0mS1 DTC
TCM Internal FLASH checksum P1603Checksum incorrect Calculated checksum does not match stored
checksum 0mS
2 DTC
CAN Link Engine P1719Engine Torque signal inaccurate
Engine torque signal QF 0 = 3 fcn_MmmErr
=1No CAN BUS error.
No CAN level error
and No EMS timeout. 600ms
2 DTC
CAN Link Engine Speed P1920Engine speed too high Engine Speed > Engine speed threshold> for a time
threshold n_mot > NS_MOTUEB
&
Timer_nmotueb > T_FNMOTUEBNS_MOTUEB = 7100rpm
T_FNMOTUEB=2550mS T_FNMOTUEB=2550mS 2 DTC
Speed Sensors Turbine speed sensor P0715Turbine speed sensor s/c to battery
supply Turbine speed sensor s/c to battery supply sgt_DiNtu = 2 (short circuit to plus)
2 (Status of turbine speed sensor signal. Sensor supply voltage OK0600mS2 DTC
Speed Sensors Turbine speed sensor P0717Turbine speed sensor s/c to gnd or O/C Turbine speed sensor s/c to gnd or O/C sgt_DiNtu = 0 (short to gnd or OC)0 (Status of turbine speed sensor signal. Sensor supply voltage OK 0600mS2 DTC
Speed Sensors Turbine speed sensor P0716Turbine Speed Value too high Value too high NTU >= NTUmaxntumax = 8000rpmSensor supply voltage OK
No electrical error 0
600mS2 DTC
Speed Sensors Turbine speed sensor P0716Turbine Speed Value too low Value too low NTU < ntu_Minntu_min = 20 rpmSensor supply voltage OK
No electrical error
engine speed NMO is higher than a
threshold:
status of NMO-signal is alright
output speed NAB is higher than a
threshold:
status of NAB-signal is alright or substitute
fltfl fb Ei t t
nmos_TuUew = 600rpm
nabs_TuUew = 250rpm 600mS
2 DTC
8ASXV05.9VH1 Aston Martin
Auto Gearbox Summary Jan 2008