ISUZU TROOPER 1995 Workshop Manual

DRIVEABILITV AND EMISSIONS 6E2-45
CHART A-3
.(hfi 2 of 3)
ENGINE CRANKS BUT WILL NOT RUN
FROM CHART A-3 (1 OF 3) I l j_ I
BLINKING LIGHT I STEADY LIGHT I NO LIGHT j
I
I @ • RECONNECT THE BLUE AND @ • IGNITION "OFF". •
BACK PROBE ECM AT TERMINAL BLACK ENGINE HARNESS • DISCONNECT ENGINE CONTROL C11,
C14, D15 AND D16 WITH
CONNECTORS. MODULE (ECM) CONNECTORS. TEST LIGHT TO BATTERY • REFER TO $E.CR01111:2 FOR • PROBE ECM TERMINALS C11, POSITIVE
VOLTAGE.
INTAKE PLENUM REMOVAL. C14, D15 AND D16 WITH TEST •
NOTE LIGHT WHILE CRANKING,
• WITH INTAKE PLENUM REMOVE LIGHT TO BATTERY POSITIVE SHOULD
BLINK.
DISCONNECT AND CHECK AT VOLTAGE. DOES IT? LEAST TWO INJECTORS
WITH LIGHT
SHOULD BE "OFF" ON ALL
THE INJECTOR TEST LIGHT TERMINALS. J34730-B. IS IT? TESTER SHOULD BLINK WHILE I CRANKING ENGINE.
~ ~ ~ $
DOES IT?
SHORT TO GROUND IN I FAULTY I
OPEN IN INJECTOR II FAUL TV
J CIRCUIT THAT LIGHT ECM DRIVER CIRCUIT(S). ECM WAS "ON".
~ $
• CHECK RESISTANCE OF @ • IGNITION "ON". INJECTORS, SHOULD BE 1.2 -3.0 • TEST LIGHT CONNECTED TO GROUND.
OHMS. • PROBE RED/GRN WIRE AT ANY INJECTOR.
• REPLACE ANY INJECTOR THAT LIGHT SHOULD BE "ON". WAS NOT CORRECT. IS IT? IF ALL WERE OK, REFER TO I CHART A-7 TO TEST FUEL
$ ~
PRESSURE.
• TEST LIGHT CONNECTED TO OPEN IN CIRCUIT BATTERY POSITIVE VOLTAGE BETWEEN INJECTORS PROBE BLUIYEL (DOHC} WIRE OR AND ECM MAIN BLU/YEL, ORG/BLU AND BLU/GRN RELAY. (SOHC) OF ANY INJECTOR.
NOTE LIGHT WHILE CRANKING
THE ENGINE.
LIGHT SHOULD "BLINK".
DOES
IT?
I
$
I
I NO (SOHCll NO (DOHC)j
®
I REFER TO CHART A-7 TO
I
• IGNITION "OFF". TEST FUEL PRESSURE. • DISCONNECT INJECTOR
RESISTOR MODULE.
• USING
DVOM MEASURE RESISTANCE OF THE MODULE BETWEEN THE BLU/YEL WIRE AND THE BLU/GRN WIRE.
SHOULD HAVE 2.7 OHMS ±10%. DOES IT?
$ $
REPAIR OPEN REPLACE INJEC-IN THE INJEC- TOR
RESISTOR
TOR DRIVER MODULE
CIRCUIT(S).

6E2-46 DRIVEABILITV AND EMISSIONS
CHART A-3
(Page 3 of 3)
ENGINE CRANKS BUT WILL NOT RUN
Circuit Description:
If the "Scan tool" did not indicate a engine speed and there is no spark present at the plugs, the problem lies in the
electronic ignition system
or the power and ground supplies to the module.
The magnetic crankshaft position is used to determine engine crankshaft position sensor much the same way as
the pick-up coil did in distributor type systems. The sensor is mounted in the block near a seven slot wheel on the
crank shaft. The rotation
of the wheel creates a flux change in the sensor which produces a voltage signal. The
Ignition Control Module (ICM) then processes this signal and creates the reference pulses needed by the engine
control module and the signal triggers the correct coil at the correct time.
Test Description: Numbers below refer to circled ® Checks for continuity of the crankshaft position
numbers on the diagnostic chart. sensor and connections.
good ground is
available at the ICM. cranking speed of engine.
® Tests for battery positive voltage in Ignition Feed
Circuit to the
ICM.
TO ECM RED/GRN #1 BLU/YEL MAIN RELAY
tRED/GRN
RED/GRN #2 BLU/YEL
RED/GRN #3 BLU/YEL
RED/GRN '"#4 BLU/YEL RED/GRN #5 BLU/YEL RED/GRN #6 BLU/YEL
FUEL
INJECTORS INJECTOR
RED/GRN RED/GRN RED/GRN
E"'QINE YELJGRN D11 BLK!ORN ----)>--BLK!YEL _____..,-~ TO IGN BLK!RED
-TO TACHOMETER SWITCH BLK --:::J_ AND TCM (C91-D12)
WHT2cl]= :-·-, 2 CRANKSHAFT BLK ~ : POSITION WHT/RED · __ ,' 1 SENSOR
'-;SHIELD
Fig. 6E2-28
ENGINE CONTROL
MODULEIECM)
1 and 2 fuel injector
•

DRIVEABILITV AND EMISSIONS 6E2-47
CHART A-3
teage' 3 of 3)
ENGINE CRANKS BUT WILL NOT RUN
FROM
CHART A-3 (1 OF 3)
NO CRANKING REVOLUTION PER MINUTE j INDICATED AND NO SPARK.
• DISCONNECT ELECTRONIC IGNITION
(EI) MODULE 2 PIN CONNECTOR.
• IGNITION "ON" • CONNECT TEST LIGHT BETWEEN HARNESS TERMINALS.
LIGHT "OFF"
I LIGHT "ON" I
• CONNECT TEST LIGHT FROM @ • DISCONNECT CRANKSHAFT POSITION 3-WAY CONNECTOR FROM
HARNESS TERMINAL "B" TO El MODULE.
GROUND. • WITH OHMMETER IN 2K OHMS POSITION, PROBE HARNESS TERMINALS "B1 & B3" (SHOULD READ BETWEEN 900-1200 OHMS).
I
cf
I LIGHT "ON" I LIGHT "OFF" I NOT OK I
I l I I
REPAIR OPEN
I REPAIR OPEN @ • SET VOLTMETER ON 2 VOLT LESS THAN
I
GREATER THAN GROUND CIRCUIT. IGNITION FEED AC POSITION. 900
OHMS 1200 OHMS CIRCUIT.
• CRANK ENGINE AND OBSERVE I l VOLTAGE READING. READING SHOULD BE GREATER SENSOR LEADS OPEN
SENSOR THAN .1 VOLT (100 mV). SHORTED CKT FAULTY IS IT? TOGETHER OR CONNECTION FAUL TV CRANK OR FAULTY SENSOR
SENSOR
YES
I
$
REPLACE El ~ MODULE. FAUL
TV CONNECTION J OR FAUL TV SENSOR.

6E2-48 DRIVEABILITY AND EMISSIONS
CHART A-5
FUEL PUMP RELAY CIRCUIT
Circuit Description:
When the ignition switch is turned "ON", the Engine Control Module (ECM) will activate the ft:Jel pump relay and
operate the in-tank
fuel pump. The fuel pump will operate as long as the engine is cranking or running and the ECM
is receiving ignition reference pulses. If there are no reference pulses, the ECM will shut "OFF" the fuel pump
within 2 seconds after key
"ON".
Test Description:
Numbers below refer to circled numbers on the diagnostic chart.
CD Checks for the presence Battery Position Voltage at switching portion of fuel pump relay.
® Checks circuit between fuel pump relay and ground (including the fuel pump).
® This test will confirm if voltage is available to the relay coil.
Diagnostic Aids:
A visual inspection of wiring and connectors should be made if an intermittent problem exists. For more
information, see
"lntermittents" in "Symptoms," Section "6E2-B".
ECM
FUEL PUMP
RELAY
H02S HEATER _. ___ .,.TO H02S HEATER
10 A BODY HARNESS CONNECTOR (WHITE)
RED/WHT 1---_.__.., '"..._.. __ BLK!RED...J
_[BLK
-= LOCATED PASSENGER SIDE CHASSIS
GROUND
CONNECTOR
TO MAIN RELAY
RED/WHT---+-ECM TERMINALS "81", "C16", 11A6" AND FUEL INJECTORS
FACE VIEW FUEL PUMP RELAY SOCKET
BLK
j__
IN TANK FUEL PUMP
TO BATIERY IN UNDERHOOD ENGINE
CONTRO:-- MODULE(ECM) ·.
FUEL PUMP RELAY DRIVER
8+
VOLTAGE
FUSE/RELAY
i L---------------------------C-EN_T_E_R _______________________ ~
lL---f~. 6E2=29
/
'"·:c·t( (7.::!11t.~ l<(/1) 1/. i-
•

DRIVEABILITV AND EMISSIONS 6E2-49
CHART A-5
FUEL PUMP RELAY CIRCUIT
• REMOVE FILL CAP. • IGNITION "ON", ENGINE STOPPED.
• LISTEN FOR PUMP TO RUN AT FILLER NECK. • PUMP SHOULD RUN FOR 2 SECONDS, THEN SHUT "OFF". DOES IT?
I
CD
$ $
• REMOVE RELAY FROM UNDERHOOD RELAY CENTER. INTERMITTENT PROBLEM. SEE I • WITH TEST LIGHT TO GROUND, PROBE RED/WHT "DIAGNOSTIC AIDS" ON FACING~. WIRE CAVITY OF FUEL PUMP RELAY CONNECTOR.
• LIGHT SHOULD BE "ON". IS IT?
I
$
$
• JUMPER RED/WHT WIRE AND BLK/RED WIRE WITH A OPEN IN RED/WHT WIRE CIRCUIT. I FUSED JUMPER. • LISTEN FOR FUEL PUMP TO RUN. DOES IT?
I
$ $
• IGNITION "OFF" FOR 10 SECONDS. • JUMPER WIRE STILL IN PLACE. ® • CONNECT TEST LIGHT BETWEEN BLK WIRE AND • PROBE FUEL PUMP CONNECTOR AT FUEL
PNK/WHT WIRE OF FUEL PUMP RELAY CONNECTOR. TANK WITH TEST LIGHT TO GROUND. • IGNITION "ON", LIGHT SHOULD BE "ON" FOR 2 • LIGHT SHOULD BE "ON". SECONDS, THEN SHUT "OFF". IS IT? IS IT?
I
$
$ ~ $
• IGNITION "OFF" FOR 10 SECONDS. I FAULTY RELAY I OPEN IN GROUND TO I OPEN IN BLK/RED WIRE I • BACK PROBE TERMINAL "C3" OF FUEL PUMP ENGINE CONTROL MODULE (ECM) OR WITH TEST LIGHT TO GROUND. FAULTY FUEL PUMP • IGNITION "ON". • LIGHT SHOULD BE "ON" FOR 2 SECONDS.
IS IT?
I
$ $
OPEN IN PNK/WHT WIRE FAULTY ENGINE OR CONTROL MODULE
OPEN IN BLK WIRE (ECM)

6E2-50 DRIVEABILITY AND EMISSIONS
Circuit Description:
CHART A-7
FUEL SYSTEM PRESSURE TEST
(Page 1 of 3)
The fuel pump delivers fuel to the fuel rail and injectors, where the system pressure is controlled from 280 to 320
kPa (41 to 46 psi) by the fuel pressure control valve. Excess fuel is returned to the fuel tank. When the engine is
stopped, the
pump can be energized by jumping the fuel pump relay connector with a fused jumper.
Test Description:
Numbers below refer to circled numbers on the diagnostic chart.
CD Use pressure gauge J-34730-1. Wrap a shop towel around the fuel pressure tap to absorb any small amount
offuelleakage that may occur when installing the gauge. (The pressure will not leak down after the fuel pump
is stopped on a correctly functioning system.)
® While the engine is idling, manifold absolute pressure is low (high vacuum). When this is applied to the fuel
regulator
diaphragm the vacuum will result in a lower fuel pressure at about 190-200 kPa (25-30 psi)
@ The application of high vacuum to the fuel pressure control valve should result in a fuel pressure drop.
@ Fuel pressure leak-down may be caused by one of the following:
• Fuel
pump check valve not holding.
•
Pump coupling hose leaking.
• Fuel
pressure control valve leaking.
• Injector
sticking open/leaking.
Diagnostic Aids:
Improper fuel system pressure may contribute to one or all of the following symptoms:
• Cranks but will not run.
• Diagnostic trouble code 44 or 45.
• Cutting out (May feel like ignition problem).
•
Hesitation, loss of power or poor fuel economy.
Refer
to "Symptoms", Section "6E2-B".
SHRADER FITTING
FUEL PRESSURE
GAUGE
J-34730-1
Fig. 6E2-30
MANIFOLD VACUUM
FUEL PRESSURE CONTROL VALVE
FUEL RETURN LINE
FUEL FILTER
PUMP INLET FILTER

DRIVEABILITV AND EMISSIONS 6E2-51
CHART A-7
(PJtge 1 of 3}
FUEL SYSTEM PRESSURE TEST
NOTE: FUEL SYSTEM IS UNDER PRESSURE. TO AVOID FUEL SPILLAGE, REFER TO FIELD SERVICE PROCEDURES FOR TESTING OR REPAIRS
REQUIRING DISASSEMBLY OF FUEL LINES OR FITTINGS. REFER TO~ 3 OF 3 OF THIS CHART.
CD • INSTALL FUEL PRESSURE GAUGE, J34730-1 OR EQUIVALENT, SEE CHART A-7 ~3 OF 3) FOR INSTALLATION PROCEDURE.
• DISCONNECT VACUUM HOSE FROM FUEL PRESSURE CONTROL VALVE.
• IGNITION MUST BE "OFF" FOR 10 SECONDS.
• TURN IGNITION "ON". FUEL PUMP SHOULD RUN FOR ABOUT 2 SECONDS.
• NOTE FUEL PRESSURE AFTER PUMP STOPS.
• FUEL PRESSURE SHOULD BE 280-320 kPa (41-46 PSI) AND HOLDING STEADY. IS IT?
I
• START AND IDLE ENGINE AT NORMAL OPERATING TEMPERATURE. • RECONNECT VACUUM LINE.
• FUEL PRESSURE SHOULD HAVE
DROPPED SLIGHTLY.
DID IT?
I
@ FUEL PRESSURE
WITHIN SPECIFICATION,
BUT NOT HOLDING.
• IGNITION "OFF".
.---'---$YES
-$r---'--NO -
@ • DISCONNECT VACUUM NO TROUBLE •
CONNECT FUSED
JUMPER FROM BATTERY POSITIVE
VOLTAGE TO FUEL PUMP
RELAY CONNECTOR BETWEEN THE BLK/RED WIRE AND RED/WHT WIRE IN ENGINE
COMPARTMENT.
HOSE FROM
FUEL FOUND. REFER PRESSURE CONTROL TO "DIAGNOSTIC
VALVE. AIDS" ON
• WITH ENGINE IDLING. FACING P.A@f. APPLY 12-14"
HYDRAGYRUM OF VACUUM TO FUEL PRESSURE CONTROL
VALVE
•
FUEL PRESSURE SHOULD DROP SLIGHTLY.
DID IT?
I
• GRADUALLY BLOCK FUEL PRESSURE LINE BY PINCHING FLEX HOSE.
• REMOVE JUMPER FROM
TEST CONNECTOR WHILE
CONTINUING TO BLOCK
PRESSURE LINE.
• PRESSURE SHOULD HOLD.
DID
IT?
I PRESSURE
OUT OF SPECIFICATION.
I USE,.eAef 2 OF THIS CHART.
I
INO I PRESSURE
I
I USE CHART I A-5
~~NLO------------------~ $~YELS---------------------, LOCATE AND CORRECT
CAUSE OF INTERRUPTED
MANIFOLD ABSOLUTE
PRESSURE SUPPLY TO
REGULATOR. FUEL PRESSURE
CONTROL VALVE ASSEMBLY
IS FAULTY.
• REPEAT ABOVE PROCEDURE CHECK FOR WHILE BLOCKING FUEL -LEAKING PUMP COUPLING HOSE. RETURN LINE INSTEAD OF -FAUL TV IN-TANK PUMP PRESSURE LINE BY PINCHING FLEX HOSE.
• PRESSURE SHOULD HOLD.
DID
IT?
LOCATE AND REPLACE LEAKING INJECTOR AND DRY SPARK PLUGS
FROM FLOODED
CYLINDERS.
FUEL PRESSURE
CONTROL VALVE
ASSEMBLY
IS FAULTY.

6E2-52 DRIVEABILITV AND EMISSIONS
CHART A-7
(Page 2 of 3)
FUEL SYSTEM PRESSURE TEST
Circuit Description:
The fuel pump delivers fuel to the fuel rail and injectors, where the system pressure is controlled from 280 to 320
kPa (41 to 46 psi) by the fuel pressure control valve. Excess fuel is returned to the fuel tank. When the engine is
stopped, the
pump can be energized by jumping the fuel pump relay connector with a fused jumper.
Test Description:
Numbers below refer to circled numbers on the diagnostic chart.
® Pressure less than 280 kPa (41 psi) may be caused by one of two problems.
• The regulated fuel pressure is too low. The system will be running lean and may set diagnostic trouble code
44. Also, hard cold starting and overall poor performance is possible.
• Restricted flow is causing a pressure drop. Normally, a vehicle with a fuel pressure loss at idle will not be
driveable. However,
if the pressure drop occurs only while driving, the engine will surge and then stop as
pressure begins to drop rapidly.
® Restricting the fuel return line allows the fuel pump to build above regulated pressure. When battery positive
voltage is applied to the fuel pump relay, pressure should
be above 450 kPa (65 psi).
® This test determines if the high fuel pressure is due to a restricted fuel return line or a fuel pressure control
valve problem.
SHRADER FITIING
FUEL PRESSURE GAUGE J-34730-1
Fig. 6E2-31
MANIFOLD VACUUM
FUEL PRESSURE CONTROL VALVE
FUEL RETURN
LINE
FUEL FILTER
PUMP INLET FILTER
•

DRIVEABILITV AND EMISSIONS 6E2-53
CHART A-7
(P«ge 2 of 3)
FUEL SYSTEM PRESSURE TEST
NOTE: FUEL SYSTEM IS UNDER PRESSURE. TO AVOID FUEL SPILLAGE, REFER TO FIELD SERVICE PROCEDURES FOR TESTING OR REPAIRS
REQUIRING DISASSEMBLY OF FUEL LINES OR FITIINGS. REFER TO PAGE 3 OF 3 OF THIS CHART.
FROM CHART A-7 E!A:8E 1 PRESSURE OUT OF SPEC.
LOW PRESSURE I
(j) • CHECK FOR RESTRICTED IN-LINE FILTER. I IS FILTER OK?
® ~ $
• IGNITION "OFF"
REPLACE FILTER I • APPLY BATIERY POSITIVE AND RE-TEST.
VOLTAGE TO FUEL PUMP RELAY CONNECTOR USING A FUSED JUMPER
WIRE WITH FUEL PUMP RELAY
REMOVED.
• GRADUALLY BLOCK FUEL
RETURN LINE BY PINCHING
FLEXIBLE HOSE AND NOTE FUEL PRESSURE.
• FUEL PRESSURE SHOULD BE ABOVE 450 kPa (psi) IS IT?
~ $
FUEL PRESSURE CHECK IN-TANK PUMP
CONTROL VALVE ASSEMBLY FOR ASSEMBLY IS FAULTY.
-FAULTY FUEL PUMP -LEAKING COUPLING HOSE -INCORRECT PUMP. HIGH
PRESSURE
I
• DISCONNECT VACUUM LINE TO PRESSURE REGULATOR. • DISCONNECT FUEL RETURN LINE FLEXIBLE HOSE.
• ATIACH AS/16. I.D. FLEX HOSE TO PRESSURE REGULATOR SIDE OF RETURN LINE AND INSERT THE OTHER END INTO AN APPROVED GASOLINE
CONTAINER.
• NOTE FUEL PRESSURE WITHIN 2 SECONDS AFTER IGNITION IS TURNED "ON" • FUEL PRESSURE SHOULD BE 280-320 (41-46 PSI).
IS IT?
CfJ ~ FUEL PRESSURE LOCATE AND REPAIR
CONTROL VALVE RESTRICTED FUEL ASSEMBLY IS FAULTY. RETURN LINE.

6E2-54 DRIVEABILITY AND EMISSIONS
Circuit
description
CHART A-7
(Page 3 of 3)
FUEL SYSTEM PRESSURE TEST
The fuel rail is equipped with a schrader fitting. Install fuel pressure gauge J-34730-1.
NOTE: On vehicles with DOHC Engine, it is necessary to remove the common chamber from the Intake Manifold
to gain access to the Shrader Fitting on the fuel rail. Refer to Section "6E2-C2" "Fuel Metering System", for
common chamber removal procedure.
SHRADER FITIING
FUEL PRESSURE
GAUGE
J-34730-1
Fig. 6E2-32
MANIFOLD VACUUM
FUELPRESSURECONTROLVALVE
FUEL RETURN LINE
FUEL FILTER
PUMP INLET FIL TEA
•