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FWD GEN II Northstar 2000-current? by AJxtcman
Started on: 02-23-2007 07:01 AM
Replies: 18
Last post by: AJxtcman on 02-26-2007 07:39 AM
AJxtcman
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Report this Post02-23-2007 07:01 AM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post
This will be Information only on the Engine Mechanical and Engine Controls.
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AJxtcman
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Report this Post02-23-2007 07:12 AM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post
Engine Mechanical Specifications (LD8 (VIN Y)) 2000 - 2003
Application Specification
Metric English
General
• Engine Type V-8
• Piston Displacement 4.6 Liter 279 cu in
• RPO LD8
• VIN Y
• Compression Ratio 10.0:1
• Compression Pressure at Cranking Speed, Throttle Open 965-1172 KPa 140-170 psi
• Power 205 kW @ 5,600 RPM 275 hp @ 5,600 RPM
• Torque 407 N•m @ 4,000 RPM 300 lb ft @ 4,000 RPM
• Firing Order 1-2-7-3-4-5-6-8
Bearings
• Crankshaft, Main, Bearing Material Aluminum
• Production Clearance 0.015-0.055 mm 0.0006-0.0022 in
• Service - Maximum 0.0635 mm 0.0025 in
• Connecting Rod Bearing Material Aluminum
• Production Clearance 0.025-0.076 mm 0.0010-0.0030 in
• Service - Maximum 0.076 mm 0.0030 in
Camshaft
• Camshaft Material Hardened Cast Gray Iron
• Bearing Number 5
• Bearing Number on Left Cylinder Head Intake 6
• Bearing Journal Diameter 26.948-26.972 mm 1.0610-1.0619 in
• Bearing Bore Diameter, In Cylinder Head 27.013-27.033 mm 1.0635-1.0642 in
• Bearing Clearance 0.051-0.076 mm 0.0020-0.0030 in
• Production Limits 0.040-0.090 mm 0.0016-0.0035 in
• Service Limits - Maximum 0.090 mm 0.0035 in
• Runout 0.050 mm 0.0020 in
• Out-of-Round 0.006 mm 0.0002 in
• Straightness 0.007 mm 0.0003 in
• Thrust Width 22.990-23.090 mm 0.9051-0.9091 in
• Timing, @ 0.150 mm [0.006 in] Lift, Intake Opens 5.6 degrees BTDC
• Intake Centerline 113 degrees ABDC
• Intake Closes 236.8 degrees ABDC
• Exhaust Opens 222.5 degrees BTDC
• Exhaust Centerline 107 degrees BTDC
• Exhaust Closes 13.8 degrees ABDC
• Camshaft Lift, Intake 6.15 mm 0.2421 in
• Exhaust 5.94 mm 0.2339 in
• Valve Intake 10.500 mm 0.4134 in
• Exhaust 10.000 mm 0.3937 in
• Duration, @ 0.150 mm [0.006 in] Lift, Intake 242 degrees
• Exhaust 236 degrees
• Valve Overlap, @ 0.150 mm [0.006 in] Lift 1.98 degrees
• Left Intake Water Pump Drive End, Diameter 15.852-15.902 mm 0.6241-0.6261 in
• Diameter Within Last 19.5 mm (0.7677 in) 15.872-15.882 mm 0.6249-0.6253 in
• Runout 0.150 mm 0.0059 in
Camshaft Drive
• Primary Drive Type Endless Chain
• Adjustment Hydraulic, Automatic
• Pitch 8 mm 0.315 in
• Width Single Row
• Secondary Drive Type Endless Chain
• Adjustment Hydraulic, Automatic
• Pitch 8 mm 0.315 in
• Width Single Row
Connecting Rods
• Diameter, Crankshaft End, Without Bearings 57.136-57.152 mm 2.2495-2.2501 in
• Taper, Maximum 0.005 mm 0.0002 in
• Piston Pin End, With Bushing 21.002-21.016 mm 0.8268-0.8274 in
• Taper, Maximum 0.007 mm 0.0003 in
• Without Bushing 23.453-23.493 mm 0.9234-0.9421 in
• Width 21.774 mm 0.8572 in
• Center to Center 151.000 mm 5.9449 in
• Side Clearance, Pair of Connecting Rods on Crankpin 0.200-0.500 mm 0.0079-0.0197 in
Crankshaft
• Journals Crankshaft, Main, Diameter 64.350-64.366 mm 2.5335-2.5341 in
• Runout #1, #5 0.022 mm 0.0009 in
• Runout #2, #3, #4 0.025 mm 0.0010 in
• Round 0.005 mm 0.0002 in
• Taper 0.005 mm 0.0002 in
• Width, #1, #2, #4, #5 24.540-24.660 mm 0.9661-0.9709 in
• Thrust #3, Wall Width 25.150-25.250 mm 0.9902-0.9941 in
• Runout 0.040 mm 0.0016 in
• Square 0.010 mm 0.0004 in
• Crankpin, Connecting Rod, Diameter 53.947-53.963 mm 2.1239-2.1245 in
• Round 0.005 mm 0.0002 in
• Taper 0.005 mm 0.0002 in
• Width 43.840-43.960 mm 1.7260-1.7307 in
• End Play, Production 0.050-0.500 mm 0.0020-0.0197 in
• Service - Maximum 0.500 mm 0.0197 in
• Flange, Engine Flywheel, Face Runout 0.025 mm 0.0010 in
• Rear Seal, Diameter 95.880-95.980 mm 3.7748-3.7787 in
• Runout 0.025 mm 0.0010 in
• Nose Diameter, 0.0-21.0 mm (0.000-0.827 in), From Front Face 34.500-34.750 mm 1.3583-1.3681 in
• Runout 0.100 mm 0.0039 in
• 21.0-53.00 mm (0.827-2.087 in), From Front Face 34.892-34.912 mm 1.3737-1.3745 in
• Runout 0.030 mm 0.0012 in
• 53.00 mm (2.087 in), From Front Face, to Rolled Fillet 33.450-33.550 mm 1.3169-1.3209 in
• Runout 0.100 mm 0.0039 in
• 89.94-110.54 mm (3.541-4.352 in), From Front Face 44.950-45.000 mm 1.7697-1.7717 in
• Runout 0.025 mm 0.0010 in
Crankshaft Balancer
• Hub Inside Diameter 34.847-34.864 mm 1.3719-1.3726 in
• Outside Diameter, Without Wear Sleeve 50.730-50.870 mm 1.9972-2.0028 in
• Runout 0.100 mm 0.0039 in
Cylinder Block
• Material Aluminum with Cast-in Grey Iron Sleeves
• Length 528.45 mm 20.8100 in
• Cylinder Bore Diameter @ 41 mm (1.6100 in) Below Deck Face 92.992-93.008 mm 3.6611-3.6617 in
• Out-of-Round, Production 0.010 mm 0.0004 in
• Service - Maximum Allowed 0.100 mm 0.0039 in
• Taper, Production 0.010 mm 0.0004 in
• Service - Maximum Allowed 0.100 mm 0.0039 in
• Piston Clearance @ 41 mm (1.6100 in) Below Deck Face 0.020-0.051 mm 0.0008-0.0020 in
• Stroke 84 mm 3.3071 in
• Deck Height 224.55 mm 8.8406 in
• Clearance - Above Deck Surface 0.45 mm 0.0177 in
• Face Flatness - Maximum Allowed 0.100 mm 0.0039 in
• Crankshaft Bearing Bore, Mains, Diameter 72.430-72.442 mm 2.8516-2.8521 in
• Crankshaft Rear Seal Bore, Diameter 115.962-116.038 mm 4.5654-4.5684 in
• Runout - Maximum Allowed 0.250 mm 0.0098 in
Cylinder Head
• Type DOHC -- 4 Valves Per Cylinder
• Material Aluminum
• Combustion Chamber Volume 48.6 cc 2.965 cu in
• Chamber Depth to Surface 10.470-10.710 mm 0.4122-0.4217 in
• Flatness, Without Resurfacing - Maximum 0.050 mm 0.0020 in
• Resurfacing Amount - Maximum 0.200 mm 0.0079 in
• Distance to Camshaft Bore Centerline 136.000 mm 5.3543 in
• Inside Diameter 5.969-5.989 mm 0.2350-0.2358 in
• Valve Guide-to-Valve Stem Clearance Production, Exhaust 0.050-0.100 mm 0.0020-0.0039 in
• Intake 0.028-0.068 mm 0.0011-0.0027 in
• Service, Exhaust 0.120 mm 0.0047 in
• Intake 0.110 mm 0.0043 in
• Valve Seating Surface, Angle 45.75 degrees
• Width, Exhaust 1.300-1.700 mm 0.0512-0.0669 in
• Intake 0.420-0.820 mm 0.0165-0.0323 in
• Runout - Maximum 0.050 mm 0.0020 in
• Relief, Angle 20 degrees
• Width, Exhaust 0.160-0.360 mm 0.0063-0.0142 in
• Intake 0.110-0.310 mm 0.0043-0.0118 in
• Runout - Maximum 0.050 mm 0.0020 in
• Undercut Angle, Exhaust 65 degrees
• Intake 60 degrees
Oil System
• Oil Pump Type Gerotor
• Minimum Pressure at Normal Operating Temperature @ Idle 35 kPa 5 psi
• Minimum Pressure at Normal Operating Temperature @ 2,000 RPM 250 kPa 35 psi
• Oil Pressure Recirculation Internal Piston Valve
• Oil Filter Type PF 58
• Oil Capacity with Filter 7.098 Liter 7.5 Quarts
• Without Filter 6.625 Liter 7 Quarts
Pistons
• Material Aluminum
• Diameter 92.957-92.972 mm 3.6597-3.6603 in
• Taper No Taper Measurement
• Pin Bore Diameter 21.003-21.008 mm 0.8269-0.8271 in
• Ring Groove Width, 1st Compression, Top 1.230-1.255 mm 0.0484-0.0494 in
• 2nd Compression 1.530-1.555 mm 0.0602-0.0612 in
• Oil Control 2.530-2.555 mm 0.0996-0.1006 in
• Inside Diameter, 1st Compression, Top 84.720-84.970 mm 3.3354-3.3453 in
• 2nd Compression 83.260-83.510 mm 3.2779-3.2878 in
• Oil Control 85.570-85.820 mm 3.3689-3.3787 in
Piston Pins
• Material Steel
• Diameter 20.995-21.000 mm 0.8266-0.8268 in
• Length 62.000-61.500 mm 2.4409-2.4212 in
• Retention Snap Rings (2)
Piston Rings
• Compression 2
• Oil Ring 1
• Side Clearance, 1st Compression, Top 0.040-0.095 mm 0.0016-0.0037 in
• 2nd Compression 0.040-0.095 mm 0.0016-0.0037 in
• Oil Control None - Side Sealing
• Ring End Gap, 1st Compression, Top 0.250-0.400 mm 0.0098-0.0157 in
• 2nd Compression 0.350-0.050 mm 0.0138-0.0020 in
• Oil Control 0.250-0.760 mm 0.0098-0.0299 in
Rocker Arms, Followers
• Type Roller
• Ratio 1.68 to 1
• Roller Diameter 17.740-17.800 mm 0.6984-0.7008 in
Valves
• Exhaust, Length from Tip to Face OD 91.730-91.990 mm 3.6114-3.6217 in
• Head, Diameter 27.880-28.140 mm 1.0976-1.1079 in
• Runout - Maximum 0.380 mm 0.0150 in
• Chamfer, Angle 30 degrees
• Width - Minimum 0.380 mm 0.0150 in
• Margin Width 1.070 mm 0.0421 in
• Face, Angle 45 degrees
• Width - Minimum 1.500 mm 0.0591 in
• Runout - Maximum 0.038 mm 0.0015 in
• Valve Stem Diameter 5.920-5.940 mm 0.2331-0.2339 in
• Out-of-Round - Maximum Deviation 0.008 mm 0.0003 in
• Straightness - Maximum Deviation 0.013 mm 0.0005 in
• Intake, Length from Tip to Face OD 110.600-110.860 mm 4.3543-4.3646 in
• Head Diameter 36.090-36.350 mm 1.4209-1.4311 in
• Runout - Maximum 0.380 mm 0.0150 in
• Chamfer, Angle 30 degrees
• Width - Minimum 0.380 mm 0.0150 in
• Margin Width 0.890 mm 0.0350 in
• Face, Angle 45 degrees
• Width - Minimum 1.000 mm 0.0394 in
• Runout - Maximum 0.038 mm 0.0015 in
• Valve Stem Diameter 5.920-5.940 mm 0.2331-0.2339 in
• Out-of-Round - Maximum Deviation 0.008 mm 0.0003 in
• Straightness - Maximum Deviation 0.013 mm 0.0005 in
Valve Lifters, Stationary Hydraulic Lifter Adjuster - SHLA
• Type Stationary Hydraulic
• Diameter 11.986-12.000 mm 0.4719-0.4724 in
• Lifter Bore Diameter, In Cylinder Head 12.013-12.037 mm 0.4730-0.4739 in
• Clearance 0.037-0.041 mm 0.0015-0.0016 in
Valve Springs
• Length Installed 35 mm 1.3780 in
• Free 40.790-43.690 mm 1.6059-1.7201 in
• Valve Closed 35 mm 1.3780 in
• Valve Open 24.500 mm 0.9646 in
• Force, Valve Closed 211.4-233.4 N•m 47.5-52.5 lb
• Valve Open 579.0-631.0 N•m 130.2-141.9 lb
• Diameter Inside 17.750-18.250 mm 0.6988-0.7185 in
• Outside 26.23 mm 1.0327 in
• Wire, Ovate 4.110 x 3.280 mm 0.1618 x 0.1291 in
• Coil Direction Clockwise
• Total Number of Coils 6.90 - 7.10
• Identifier Orange


New Product Information for 2003

The purpose of New Product Information is to highlight or indicate important changes from the previous model year.

Changes may include one or more of the following items:

Torque values and/or fastener tightening strategies
Changed engine specifications
New sealants and/or adhesives
Disassembly and assembly procedure revisions
Engine mechanical diagnostic procedure revisions
New special tools required
A component comparison from the previous year
Torque Values and/or Fastener Tightening Strategies
The engine mechanical fastener tightening specifications have not changed for model year 2003.

Changed Engine Specifications
There are early and late design engine mechanical specifications for connecting rod bore diameter - pin end, piston pin bore diameter and piston pin diameter. Refer to Engine Mechanical Specifications .

There are changes in drill depth and tap depth to the engine block deck face holes for the cylinder head bolts. Refer to Thread Repair Specifications .

New Sealants and/or Adhesives
There are no changes to the sealants and/or adhesives used for model year 2003.

Disassembly and Assembly Procedure Revisions
The Lubrication System Priming Procedure has been replaced by the Lubrication Preluber Procedure. A new tool J 45299 has been developed to prime the engine with new clean engine oil.

There are early and late design crankshaft rear oil seals. The early design crankshaft rear oil seal requires the use of the installation tool J 42842 in order to set the correct depth. The late design crankshaft rear oil seal requires the use of a new installation tool J 44642 in order to set the correct depth. Refer to Crankshaft Rear Oil Seal Installation .

Engine Mechanical Diagnostic Procedure Revisions
Additional engine coolant leakage diagnostics have been added.

New Special Tools Required
*A new tool J 45299 has been developed to prime the engine with new clean engine oil.

*Starting in model year 2003 the bushing used in the fixture plate has been replaced by J 42385-2002. Refer to Thread Repair . For model year 2000 through 2002 use J 42385-302.

*There are early and late design crankshaft rear oil seals. The early design crankshaft rear oil seal requires the use of the installation tool J 42842 in order to set the correct depth. The late design crankshaft rear oil seal requires the use of a new installation tool J 44642 in order to set the correct depth. Refer to Crankshaft Rear Oil Seal Installation .

*The J 44213 has been replaced by the EN 46327 . Using the EN 46327 will allow the additional servicing of the camshaft sprockets without removing the engine front cover. A smaller diameter camshaft alignment pin hole in the camshaft sprockets will prevent the camshaft sprockets from sliding onto the J 44213 .

A Component Comparison from the Previous Year
*The oil filter adapter has been revised. The oil filter adapter has an additional mounting boss and corresponding fastener bolt.

*The oil filter adapter sealing has been revised. An oil filter adapter gasket replaces the previously used O-rings.

*The lower crankcase has been revised. The oil filter adapter mounting area on the lower crankcase has been modified to accommodate the changes made to the oil filter adapter and the sealing of the oil filter adapter gasket.

Notice: Do not mix early and late design components. Improper clamp loads will occur if cylinder head bolts are tightened using a mixture of early and late design components. Damage will occur to the powertrain if mixed components are used.

*The engine block holes in the engine block deck faces for the M11 cylinder head bolts have decreased in depth, they are drilled and tapped approximately 7 mm (0.276 in) shallower.

Notice: Do not mix early and late design components. The internal balance of the engine will be affected if early and late design components are used together. Damage will occur to the powertrain if mixed components are used.

*There are early and late design crankshaft, connecting rods, pistons and pistons pins. The early and late design components must not be interchanged.

Notice: The proper installation tool must be used with the proper component. Early and late design components are installed to different depths. Damage and/or leakage can occur if the improper installation tool is used.

*There are early and late design crankshaft rear oil seals. The early design crankshaft rear oil seal requires the use of the installation tool J 42842 in order to set the correct depth. The late design crankshaft rear oil seal requires the use of a new installation tool J 44642 in order to set the correct depth. Refer to Crankshaft Rear Oil Seal Installation .

*The diameter of the camshaft alignment pins to the camshaft sprockets have been reduced.

*The diameter of the camshaft alignment pin hole in the camshaft sprockets have been reduced.

*The diameter of the camshaft alignment pin hole in the camshafts have been reduced.



Engine Component Description
The Northstar V8 VIN Code 9 or Y is a 4.6 L (279 cu in) engine incorporating two intake and two exhaust valves per cylinder with individual cylinder head mounted camshafts for intake and exhaust functions (DOHC). The cylinder bore diameter is 93 mm (3.43 in) and the piston stroke is 84 mm (3.31 in). The cylinders are arranged in two banks of four with a 90° included angle. The left (front) bank of cylinders are number 2-4-6-8 and the right (rear) bank cylinders are 1-3-5-7. Engine firing order is 1-2-7-3-4-5-6-8.

Crankcase
The cylinder block is constructed of aluminum alloy by the die casting method and is constructed of two sections, an upper and a lower crankcase, split at the crankshaft center line. The grey cast iron cylinder liners are cast with the upper crankcase. The upper and lower crankcase sections are held in alignment by four dowel pins. Once machined, the sections must be kept together as a set. Sealing between the crankcase halves consists of a silicone rubber seal and a bead of anaerobic sealant along each side. Since the lower crankcase contains the lower main bearings, this casting adds to the structural rigidity of the engine assembly. Both upper and lower crankcases incorporate oil drain back passages isolated from the crankcase. These passages provide a direct path from the cylinder heads to the oil pan in order to prevent the needless aeration of the oil through contact with the rotating components.

Crankshaft
The crankshaft is a cast nodular iron design with five diameter main bearings. Crankshaft thrust is taken by the number three main bearing. The position sensor, also known as the reluctor wheel, is cast integrally with the crankshaft. The crankshaft is internally balanced and incorporates a one piece rear seal. A rolled fillet radius is incorporated on all bearing journals to improve fatigue strength.

Connecting Rods and Pistons
The connecting rods are forged steel and have full floating piston pins. These pins are slip fit in the bronze bushed rods and are retained in the piston by round wire retainers. The cast aluminum pistons use two low tension compression rings and one multi-piece oil ring. The top compression ring is nitrided steel. The second compression ring is coated cast iron. The oil ring is a three piece side seal type ring which incorporates a steel expander and two chrome plated steel rails. To provide a non-scuffing surface when the engine is new, the pistons are tin plated.

Camshaft Drive System
The four overhead camshafts are driven by three separate fine pitch chains. The primary drive chain connects the crankshaft with the intermediate shaft and sprocket located directly above the crankshaft behind the engine front cover. Each camshaft drive chain connects the intermediate sprocket with both intake and exhaust cams in the cylinder head. Two camshaft drive chains are used; one for each cylinder head. Each of the chains incorporates a hydraulic tensioner to minimize chain noise and provide accurate valve action by keeping slack out of the chain and continuously adjusting for chain wear. This is accomplished by providing engine oil pressure to each tensioner forcing a nylon pad into mesh with the slack side of the chain. As the chain stretches from wear, a ratchet mechanism inside the tensioner prevents the nylon pad from retracting when the engine is turned off and engine oil pressure ceases.

Cylinder Heads
The cylinder heads are semi permanent mold cast aluminum with powdered metal valve seat inserts and valve guides. Two 36.2 mm (1.425 in) intake valves and two 28 mm (1.102 in) exhaust valves are actuated by roller finger followers pivoting on a stationary hydraulic lash adjuster (SHLA). Separate intake and exhaust camshafts are supported by five bearings machined into the cylinder head with camshaft thrust taken by the first bearing (the left hand intake cam has an additional bearing to accommodate the water pump drive). The combustion chamber is roughly in the shape of a clover leaf with a nominal volume of 48.6 cc (2.965 cubic inch) and a centrally located spark plug.

Engine Cooling System
The left hand cylinder head intake camshaft extends outside the left hand cam cover providing drive mechanism for the coolant pump. A removable one piece lip seal prevents oil leakage around the camshaft. A drive pulley is pressed onto the end of the camshaft and provides drive for the engine coolant pump using a small multi rib drive belt and tensioner mechanism. The coolant pump assembly is located inside the water crossover casting. The water crossover distributes coolant to the cylinder block and collects it from the cylinder head for delivery to the radiator. The water crossover also provides important functions for the EGR System.

Induction System
The induction manifold is a plastic, lost core casting with a removable plastic sight shield cover.

Right and Left Bank Designation
Right hand (RH) and Left hand (LH) designations through the engine mechanical On-Vehicle Service section are viewed from the rear of the engine (left side of the vehicle). In certain cases where a location with respect to the vehicle is required, it will be referred to as right side or left side as viewed from inside the vehicle.

------------------
Cadillac Tech
ASE MASTER TECH since 1988

86 Northstar Fiero
85 RX7 former SCCA car
56 TR3 small mouth 6.0L
A.J. Whiteley

[This message has been edited by AJxtcman (edited 02-23-2007).]

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AJxtcman
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From: Rock Hill SC
Registered: Nov 2006


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Report this Post02-23-2007 07:21 AM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post

AJxtcman

1098 posts
Member since Nov 2006
2000 to 2003 VIN 9
Engine Mechanical Specifications (L37 (VIN 9))
Application Specification
Metric English
General
• Engine Type V-8
• Piston Displacement 4.6 Liter 279 cu in
• RPO L37
• VIN 9
• Compression Ratio 10.0:1
• Compression Pressure at Cranking Speed, Throttle Open 965-1172 KPa 140-170 psi
• Power 224 kW @ 5,600 RPM 300 hp @ 5,600 RPM
• Torque 400 N•m @ 4,000 RPM 295 lb ft @ 4,000 RPM
• Firing Order 1-2-7-3-4-5-6-8
Bearings
• Crankshaft, Main, Bearing Material Aluminum
• Production Clearance 0.015-0.055 mm 0.0006-0.0022 in
• Service - Maximum 0.0635 mm 0.0025 in
• Connecting Rod Bearing Material Aluminum
• Production Clearance 0.025-0.076 mm 0.0010-0.0030 in
• Service - Maximum 0.076 mm 0.0030 in
Camshaft
• Camshaft Material Hardened Cast Gray Iron
• Bearing Number 5
• Bearing Number on Left Cylinder Head Intake 6
• Bearing Journal Diameter 26.948-26.972 mm 1.0610-1.0619 in
• Bearing Bore Diameter, In Cylinder Head 27.013-27.033 mm 1.0635-1.0642 in
• Bearing Clearance 0.051-0.076 mm 0.0020-0.0030 in
• Production Limits 0.040-0.090 mm 0.0016-0.0035 in
• Service Limits - Maximum 0.090 mm 0.0035 in
• Runout 0.050 mm 0.0020 in
• Out-of-Round 0.006 mm 0.0002 in
• Straightness 0.007 mm 0.0003 in
• Thrust Width 22.990-23.090 mm 0.9051-0.9091 in
• Timing, @ 0.150 mm [0.006 in] Lift, Intake Opens 0 degrees
• Intake Centerline 122 degrees ATDC
• Intake Closes 251 degrees ATDC
• Exhaust Opens 225.5 degrees BTDC
• Exhaust Centerline 106 degrees BTDC
• Exhaust Closes 20.5 degrees ATDC
• Camshaft Lift, Intake 6.15 mm 0.2421 in
• Exhaust 5.94 mm 0.2339 in
• Valve Lift, Intake 10.500 mm 0.4134 in
• Exhaust 10.000 mm 0.3937 in
• Duration, @ 0.150 mm [0.006 in] Lift, Intake 251 degrees
• Exhaust 246 degrees
• Overlap, @ 0.150 mm [0.006 in] Lift 2.04 degrees
• Left Intake Water Pump Drive End, Diameter 15.852-15.902 mm 0.6241-0.6261 in
• Diameter within last 19.5 mm (0.7677 in) 15.872-15.882 mm 0.6249-0.6253 in
• Runout 0.150 mm 0.0059 in
Camshaft Drive
• Primary Drive Type Endless Chain
• Adjustment Hydraulic, Automatic
• Pitch 8 mm 0.315 in
• Width Single Row
• Secondary Drive Type Endless Chain
• Adjustment Hydraulic, Automatic
• Pitch 8 mm 0.315 in
• Width Single Row
Connecting Rods
• Diameter, Crankshaft End, Without Bearings 57.136-57.152 mm 2.2495-2.2501 in
• Taper, Maximum 0.005 mm 0.0002 in
• Piston Pin End, With Bushing 21.002-21.016 mm 0.8268-0.8274 in
• Taper, Maximum 0.007 mm 0.0003 in
• Without Bushing 23.453-23.493 mm 0.9234-0.9421 in
• Width 21.774 mm 0.8572 in
• Center to Center 151.000 mm 5.9449 in
• Side Clearance, Pair of Connecting Rods on Crankpin 0.200-0.500 mm 0.0079-0.0197 in
Crankshaft
• Journals Crankshaft, Main, Diameter 64.350-64.366 mm 2.5335-2.5341 in
• Runout #1, #5 0.022 mm 0.0009 in
• Runout #2, #3, #4 0.025 mm 0.0010 in
• Round 0.005 mm 0.0002 in
• Taper 0.005 mm 0.0002 in
• Width, #1, #2, #4, #5 24.540-24.660 mm 0.9661-0.9709 in
• Thrust #3, Wall Width 25.150-25.250 mm 0.9902-0.9941 in
• Runout 0.040 mm 0.0016 in
• Square 0.010 mm 0.0004 in
• Crankpin, Connecting Rod, Diameter 53.947-53.963 mm 2.1239-2.1245 in
• Round 0.005 mm 0.0002 in
• Taper 0.005 mm 0.0002 in
• Width 43.840-43.960 mm 1.7260-1.7307 in
• End Play, Production 0.050-0.500 mm 0.0020-0.0197 in
• Service - Maximum 0.500 mm 0.0197 in
• Flange, Engine Flywheel, Face Runout 0.025 mm 0.0010 in
• Rear Seal, Diameter 95.880-95.980 mm 3.7748-3.7787 in
• Runout 0.025 mm 0.0010 in
• Nose Diameter, 0.0-21.0 mm (0.000-0.827 in), From Front Face 34.500-34.750 mm 1.3583-1.3681 in
• Runout 0.100 mm 0.0039 in
• 21.0-53.00 mm (0.827-2.087 in), From Front Face 34.892-34.912 mm 1.3737-1.3745 in
• Runout 0.030 mm 0.0012 in
• 53.00 mm (2.087 in), From Front Face, to Rolled Fillet 33.450-33.550 mm 1.3169-1.3209 in
• Runout 0.100 mm 0.0039 in
• 89.94-110.54 mm (3.541-4.352 in), From Front Face 44.950-45.000 mm 1.7697-1.7717 in
• Runout 0.025 mm 0.0010 in
Crankshaft Balancer
• Hub Inside Diameter 34.847-34.864 mm 1.3719-1.3726 in
• Outside Diameter, Without Wear Sleeve 50.730-50.870 mm 1.9972-2.0028 in
• Runout 0.100 mm 0.0039 in
Cylinder Block
• Material Aluminum with Cast-in Grey Iron Sleeves
• Length 528.45 mm 20.8100 in
• Cylinder Bore Diameter @ 41 mm (1.6100 in) Below Deck Face 92.992-93.008 mm 3.6611-3.6617 in
• Out-of-Round, Production 0.010 mm 0.0004 in
• Service - Maximum Allowed 0.100 mm 0.0039 in
• Taper, Production 0.010 mm 0.0004 in
• Service - Maximum Allowed 0.100 mm 0.0039 in
• Piston Clearance @ 41 mm (1.6100 in) Below Deck Face 0.020-0.051 mm 0.0008-0.0020 in
• Stroke 84 mm 3.3071 in
• Deck Height 224.55 mm 8.8406 in
• Clearance - Above Deck Surface 0.45 mm 0.0177 in
• Face Flatness - Maximum Allowed 0.100 mm 0.0039 in
• Crankshaft Bearing Bore, Mains, Diameter 72.430-72.442 mm 2.8516-2.8521 in
• Crankshaft Rear Seal Bore, Diameter 115.962-116.038 mm 4.5654-4.5684 in
• Runout - Maximum Allowed 0.250 mm 0.0098 in
Cylinder Head
• Type DOHC -- 4 Valves Per Cylinder
• Material Aluminum
• Combustion Chamber Volume 48.6 cc 2.965 cu in
• Chamber Depth to Surface 10.470-10.710 mm 0.4122-0.4217 in
• Flatness, Without Resurfacing - Maximum 0.050 mm 0.0020 in
• Resurfacing Amount - Maximum 0.200 mm 0.0079 in
• Distance to Camshaft Bore Centerline 136.000 mm 5.3543 in
• Inside Diameter 5.969-5.989 mm 0.2350-0.2358 in
• Valve Guide-to-Valve Stem Clearance Production, Exhaust 0.050-0.100 mm 0.0020-0.0039 in
• Intake 0.028-0.068 mm 0.0011-0.0027 in
• Service, Exhaust 0.120 mm 0.0047 in
• Intake 0.110 mm 0.0043 in
• Valve Seating Surface, Angle 45.75 degrees
• Width, Exhaust 1.300-1.700 mm 0.0512-0.0669 in
• Intake 0.420-0.820 mm 0.0165-0.0323 in
• Runout - Maximum 0.050 mm 0.0020 in
• Relief, Angle 20 degrees
• Width, Exhaust 0.160-0.360 mm 0.0063-0.0142 in
• Intake 0.110-0.310 mm 0.0043-0.0118 in
• Runout - Maximum 0.050 mm 0.0020 in
• Undercut Angle, Exhaust 65 degrees
• Intake 60 degrees
Oil System
• Oil Pump Type Gerotor
• Minimum Pressure at Normal Operating Temperature @ Idle 35 kPa 5 psi
• Minimum Pressure at Normal Operating Temperature @ 2,000 RPM 250 kPa 35 psi
• Oil Pressure Recirculation Internal Piston Valve
• Oil Filter Type PF 58
• Oil Capacity with Filter 7.098 Liter 7.5 Quarts
• Without Filter 6.625 Liter 7 Quarts
Pistons
• Material Aluminum
• Diameter 92.957-92.972 mm 3.6597-3.6603 in
• Taper No Taper Measurement
• Pin Bore Diameter 21.003-21.008 mm 0.8269-0.8271 in
• Ring Groove Width, 1st Compression, Top 1.230-1.255 mm 0.0484-0.0494 in
• 2nd Compression 1.530-1.555 mm 0.0602-0.0612 in
• Oil Control 2.530-2.555 mm 0.0996-0.1006 in
• Inside Diameter, 1st Compression, Top, 84.720-84.970 mm 3.3354-3.3453 in
• 2nd Compression 83.260-83.510 mm 3.2779-3.2878 in
• Oil Control 85.570-85.820 mm 3.3689-3.3787 in
Piston Pins
• Material Steel
• Diameter 20.995-21.000 mm 0.8266-0.8268 in
• Length 62.000-61.500 mm 2.4409-2.4212 in
• Retention Snap Rings (2)
Piston Rings
• Compression 2
• Oil Ring 1
• Side Clearance, 1st Compression, Top 0.040-0.095 mm 0.0016-0.0037 in
• 2nd Compression 0.040-0.095 mm 0.0016-0.0037 in
• Oil Control None - Side Sealing
• Ring End Gap, 1st Compression, Top 0.250-0.400 mm 0.0098-0.0157 in
• 2nd Compression 0.350-0.050 mm 0.0138-0.0020 in
• Oil Control 0.250-0.760 mm 0.0098-0.0299 in
Rocker Arms, Followers
• Type Roller
• Ratio 1.68 to 1
• Roller Diameter 17.740-17.800 mm 0.6984-0.7008 in
Valves
• Exhaust, Length from Tip to Face OD 91.730-91.990 mm 3.6114-3.6217 in
• Head, Diameter 27.880-28.140 mm 1.0976-1.1079 in
• Runout - Maximum 0.380 mm 0.0150 in
• Chamfer, Angle 30 degrees
• Width - Minimum 0.380 mm 0.0150 in
• Margin Width 1.070 mm 0.0421 in
• Face, Angle 45 degrees
• Width - Minimum 1.500 mm 0.0591 in
• Runout - Maximum 0.038 mm 0.0015 in
• Valve Stem Diameter 5.920-5.940 mm 0.2331-0.2339 in
• Out-of-Round - Maximum Deviation 0.008 mm 0.0003 in
• Straightness - Maximum Deviation 0.013 mm 0.0005 in
• Intake, Length from Tip to Face OD 110.600-110.860 mm 4.3543-4.3646 in
• Head Diameter 36.090-36.350 mm 1.4209-1.4311 in
• Runout - Maximum 0.380 mm 0.0150 in
• Chamfer, Angle 30 degrees
• Width - Minimum 0.380 mm 0.0150 in
• Margin Width 0.890 mm 0.0350 in
• Face, Angle 45 degrees
• Width - Minimum 1.000 mm 0.0394 in
• Runout - Maximum 0.038 mm 0.0015 in
• Valve Stem Diameter 5.920-5.940 mm 0.2331-0.2339 in
• Out-of-Round - Maximum Deviation 0.008 mm 0.0003 in
• Straightness - Maximum Deviation 0.013 mm 0.0005 in
Valve Lifters, Stationary Hydraulic Lifter Adjuster - SHLA
• Type Stationary Hydraulic
• Diameter 11.986-12.000 mm 0.4719-0.4724 in
• Lifter Bore Diameter, In Cylinder Head, 12.013-12.037 mm 0.4730-0.4739 in
• Clearance 0.037-0.041 mm 0.0015-0.0016 in
Valve Springs
• Length Installed 35 mm 1.3780 in
• Free 40.790-43.690 mm 1.6059-1.7201 in
• Valve Closed 35 mm 1.3780 in
• Valve Open 24.500 mm 0.9646 in
• Force, Valve Closed 211.4-233.4 N•m 47.5-52.5 lb
• Valve Open 579.0-631.0 N•m 130.2-141.9 lb
• Diameter Inside 17.750-18.250 mm 0.6988-0.7185 in
• Outside 26.23 mm 1.0327 in
• Wire, Ovate 4.110 x 3.280 mm 0.1618 x 0.1291 in
• Coil Direction Clockwise
• Total Number of Coils 6.90 - 7.10

New Product Information
Same as VIN Y above
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AJxtcman

1098 posts
Member since Nov 2006
2004 - 2007 VIN Y

Engine Mechanical Specifications (LD8)
Application Specification
Metric English
General
• Engine Type V-8
• Displacement 4.6 Liter 279 cu in
• RPO LD8
• VIN Y
• Bore 93 mm 3.661 in
• Stroke 84 mm 3.3071 in
• Compression Ratio 10.0:1
• Engine Compression Test 965-1172 kPa 140-170 psi
• Firing Order 1-2-7-3-4-5-6-8
• Spark Plug Gap 1.270 mm 0.0500 in
Block
• Crankshaft Main Bearing Bore Diameter 72.430-72.442 mm 2.8516-2.8521 in
• Crankshaft Main Bearing Bore Out-of-Round 0.010 mm 0.0004 in
• Crankshaft Main Rear Oil Seal
• Bore 115.962-116.038 mm 4.5654-4.5684 in
• Runout 0.250 mm 0.0098 in
• Cylinder Bore Diameter @ 41 mm (1.610 in) Below Deck Face 92.992-93.008 mm 3.6611-3.6617 in
• Cylinder Bore Out-of-Round
• Production 0.010 mm 0.0004 in
• Service 0.100 mm 0.0039 in
• Cylinder Bore Taper
• Production 0.010 mm 0.0004 in
• Service 0.100 mm 0.0039 in
• Cylinder Head Deck Height 224.55 mm 8.8406 in
• Cylinder Head Deck Surface Flatness 0.100 mm 0.0039 in
Camshaft
• Camshaft End Play 0.120-0.220 mm 0.0050-0.0087 in
• Camshaft Journal Diameter 26.948-26.972 mm 1.0610-1.0619 in
• Camshaft Journal Out-of-Round 0.006 mm 0.0002 in
• Camshaft Journal to Bore Clearance
• Production 0.051-0.076 mm 0.0020-0.0030 in
• Service 0.040-0.090 mm 0.0016-0.0035 in
• Camshaft Lobe Duration @ 0.150 mm (0.006 in) Lift - Exhaust 236 degrees
• Camshaft Lobe Duration @ 0.150 mm (0.006 in) Lift - Intake 242 degrees
• Camshaft Lobe Lift - Exhaust 5.94 mm 0.2339 in
• Camshaft Lobe Lift - Intake 6.15 mm 0.2421 in
• Camshaft Lobe Overlap @ 0.150 mm (0.006 in) Lift 1.98 degrees
• Camshaft Runout 0.050 mm 0.0020 in
• Camshaft Thrust Surface
• Runout 0.037 mm 0.0015 in
• Width 22.990-23.090 mm 0.9051-0.9091 in
• Camshaft Timing @ 0.150 mm (0.006 in) Lift
• Intake Opens 1.3 degrees BTDC
• Intake Centerline 117.0 degrees ATDC
• Intake Closes 237.9 degrees ATDC
• Exhaust Opens 226.1 degrees BTDC
• Exhaust Centerline 111.0 degrees BTDC
• Exhaust Closes 5.1 degrees ATDC
Cooling System
• Thermostat Full Open Temperature 85°C 185°F
Connecting Rod
• Connecting Rod Bearing Clearance
• Production and Service 0.0250-0.0760 mm 0.0010-0.0030 in
• Connecting Rod Bore Diameter - Bearing End 57.136-57.152 mm 2.2495-2.2501 in
• Connecting Rod Bore Diameter - Pin End 23.002-23.014 mm 0.9056-0.9061 in
• Connecting Rod Bore Out-of-Round - Bearing End 0.006 mm 0.0002 in
• Connecting Rod Bore Out-of-Round - Pin End 0.005 mm 0.0002 in
• Connecting Rod Length Center to Center 151.00 mm 5.9449 in
• Connecting Rod Side Clearance 0.200-0.500 mm 0.0079-0.0197 in
• Connecting Rod Straightness 0.050 mm 0.0020 in
Crankshaft
• Connecting Rod Journal Diameter 53.947-53.963 mm 2.1239-2.1245 in
• Connecting Rod Journal Out-of-Round 0.005 mm 0.0002 in
• Connecting Rod Journal Taper 0.005 mm 0.0002 in
• Connecting Rod Journal Width 43.840-43.960 mm 1.7260-1.7307 in
• Crankshaft Balancer
• Surface Diameter 50.730-50.870 mm 1.9972-2.0028 in
• Hub Inside Diameter 34.847-34.864 mm 1.3719-1.3726 in
• Crankshaft End Play 0.050-0.500 mm 0.0020-0.0197 in
• Crankshaft Main Bearing Clearance
• Production 0.0150-0.0550 mm 0.0006-0.0022 in
• Service 0.0150-0.0635 mm 0.0006-0.0025 in
• Crankshaft Main Journal Diameter 64.350-64.366 mm 2.5335-2.5341 in
• Crankshaft Main Journal Out-of-Round 0.005 mm 0.0002 in
• Crankshaft Main Journal Taper 0.005 mm 0.0002 in
• Crankshaft Main Journal Thrust Wall Runout 0.040 mm 0.0016 in
• Crankshaft Main Journal Thrust Wall Square 0.010 mm 0.0004 in
• Crankshaft Main Journal Width #1, #2, #4, #5 24.540-24.660 mm 0.9661-0.9709 in
• Crankshaft Main Journal Width, Thrust #3 25.150-25.250 mm 0.9902-0.9941 in
• Crankshaft Nose Diameter
• From Front Face 0.00-21.00 mm (0.0000-0.8268 in) 34.500-34.750 mm 1.3583-1.3681 in
• From Front Face 21.00-53.00 mm (0.8268-2.0866 in) 34.892-34.912 mm 1.3737-1.3745 in
• From Front Face 53.00 to Rolled Fillet (2.0866-Rolled Fillet) 33.450-33.550 mm 1.3169-1.3209 in
• From Front Face 89.94-110.54 mm (3.5409-4.3520 in) 44.950-45.000 mm 1.7697-1.7717 in
• Crankshaft Nose Runout
• From Front Face 0.00-21.00 mm (0.0000-0.8268 in) 0.100 mm 0.0039 in
• From Front Face 21.00-53.00 mm (0.8268-2.0866 in) 0.030 mm 0.0012 in
• From Front Face 53.00 to Rolled Fillet (2.0866-Rolled Fillet) 0.100 mm 0.0039 in
• From Front Face 89.94-110.54 mm (3.5409-4.3520 in) 0.025 mm 0.0010 in
• Crankshaft Rear Flange
• Diameter 95.880-95.980 mm 3.7748-3.7787 in
• Runout 0.025 mm 0.0010 in
• Crankshaft Rear Flange Face to Engine Flywheel Runout 0.025 mm 0.0010 in
• Crankshaft Runout
• Main Journals #1, #5 0.022 mm 0.0009 in
• Main Journals #2, #4, #6 0.025 mm 0.0010 in
Cylinder Head
• Camshaft Bearing Bore Diameter 27.013-27.033 mm 1.0635-1.0642 in
• Camshaft Bearing Bore Out-of-Round 0.010 mm 0.0004 in
• Combustion Chamber Depth - at Measurement Point 10.470-10.710 mm 0.4122-0.4217 in
• Cylinder Head Height - Deck to Camshaft Centerline Bore 136.00 mm 5.3543 in
• Surface Flatness - Block Deck 0.050 mm 0.0020 in
• Surface Flatness - Exhaust Manifold Deck 0.220 mm 0.0087 in
• Surface Flatness - Intake Manifold Deck 0.220 mm 0.0087 in
• Valve Guide Bore - Exhaust 5.969-5.989 mm 0.2350-0.2359 in
• Valve Guide Bore - Intake 5.969-5.989 mm 0.2350-0.2359 in
• Valve Guide Installed Height - Exhaust 14.300 mm 0.5630 in
• Valve Guide Installed Height - Intake 14.720 mm 0.5795 in
• Valve Lifter Bore Diameter 12.013-12.037 mm 0.4730-0.4739 in
Exhaust Manifold
Flywheel
• Runout 0.300 mm 0.0118 in
Intake Manifold
• Surface Flatness 0.500 mm 0.0200 in
Lubrication System
• Oil Capacity - with Filter 7.098 Liter 7.5 Quarts
• Oil Capacity - without Filter 6.625 Liter 7.0 Quarts
Oil Pump
• Oil Pressure - Minimum @ Idle 35 kPa 5 psi
• Oil Pressure - Minimum @ 2,000 RPM 250 kPa 35 psi
Piston Rings
• Piston Ring End Gap
• First Compression Ring 0.250-0.400 mm 0.0098-0.0157 in
• Second Compression Ring 0.350-0.050 mm 0.0138-0.0020 in
• Oil Control Ring 0.250-0.760 mm 0.0098-0.0299 in
• Piston Ring to Groove Clearance
• First Compression Ring 0.040-0.095 mm 0.0016-0.0037 in
• Second Compression Ring 0.040-0.095 mm 0.0016-0.0037 in
• Oil Control Ring None - Side Sealing
• Piston Ring Thickness
• First Compression Ring 1.199-1.203 mm 0.0472-0.0474 in
• Second Compression Ring 1.499-1.504 mm 0.0590-0.0592 in
• Oil Control Ring 2.530-2.555 mm 0.0996-0.1006 in
Pistons and Pins
• Piston
• Piston Diameter @ 42 mm (1.6353 in) below Crown 92.957-92.972 mm 3.6597-3.6603 in
• Piston Pin Bore Diameter 23.002-23.007 mm 0.9056-0.9058 in
• Piston Ring Groove Inside Diameter
• First Compression Ring 84.750-85.000 mm 3.3366-3.3464 in
• Second Compression Ring 83.400-83.650 mm 3.2835-3.2933 in
• Oil Control Ring 85.670-85.920 mm 3.3728-3.3827 in
• Piston Ring Groove Width
• First Compression Ring 1.230-1.255 mm 0.0484-0.0494 in
• Second Compression Ring 1.530-1.555 mm 0.0602-0.0612 in
• Oil Control Ring 2.530-2.555 mm 0.0996-0.1006 in
• Piston to Bore Clearance 0.020-0.051 mm 0.0008-0.0020 in
• Pin
• Piston Pin Clearance to Connecting Rod Bore 0.002-0.014 mm 0.0001-0.0006 in
• Piston Pin Clearance to Piston Pin Bore 0.002-0.012 mm 0.0001-0.0005 in
• Piston Pin Diameter 22.995-23.000 mm 0.9053-0.9055 in
• Piston Pin End Play
• Piston Pin Length 61.500-62.000 mm 2.4213-2.4409 in
Starter
Valve System
• Valves
• Valve Face Angle 45 degrees
• Valve Face Runout 0.038 mm 0.0015 in
• Valve Face Width
• Exhaust 1.500 mm 0.0591 in
• Intake 1.000 mm 0.0394 in
• Valve Head Diameter
• Exhaust 28.880-29.140 mm 1.1370-1.1472 in
• Intake 36.090-36.350 mm 1.4209-1.4311 in
• Valve Length
• Exhaust 91.730-91.990 mm 3.6114-3.6217 in
• Intake 110.600-110.860 mm 4.3543-4.3646 in
• Valve Seat Angle 45.75 degrees
• Valve Seat Relief Angle 20 degrees
• Valve Seat Relief Width
• Exhaust 0.160-0.360 mm 0.0063-0.0142 in
• Intake 0.110-0.310 mm 0.0043-0.0118 in
• Valve Seat Runout 0.050 mm 0.0020 in
• Valve Seat Undercut Angle
• Exhaust 65 degrees
• Intake 60 degrees
• Valve Seat Width
• Exhaust 1.300-1.700 mm 0.0512-0.0669 in
• Intake 0.420-0.820 mm 0.0165-0.0323 in
• Valve Stem Diameter 5.920-5.940 mm 0.2331-0.2339 in
• Valve Stem Out-of-Round 0.008 mm 0.0003 in
• Valve Stem Straightness 0.013 mm 0.0005 in
• Valve Stem-to-Guide Clearance
• Exhaust
• Production 0.050-0.100 mm 0.0020-0.0039 in
• Service 0.050-0.120 mm 0.0020-0.0047 in
• Intake
• Production 0.028-0.068 mm 0.0011-0.0027 in
• Service 0.028-0.110 mm 0.0011-0.0043 in
• Valve Lifters
• Valve Lifter Diameter 11.986-12.000 mm 0.4719-0.4724 in
• Valve Lifter-to-Bore Clearance 0.037-0.041 mm 0.0015-0.0016 in
• Rocker Arms
• Valve Rocker Arm Ratio 1.68 to 1
• Valve Rocker Arm Roller Diameter 17.740-17.800 mm 0.6984-0.7008 in
• Valve Springs
• Valve Spring Coil Thickness 4.110 x 3.280 mm 0.1618 x 0.1291 in
• Valve Spring Diameter
• Inside 17.750-18.250 mm 0.6988-0.7185 in
• Outside 26.23 mm 1.0327 in
• Valve Spring Free Length 40.790-43.690 mm 1.6059-1.7201 in
• Valve Spring Height
• Closed 35.000 mm 1.3780 in
• Open 24.500 mm 0.9646 in
• Valve Spring Load
• Closed 211.4-233.4 N 47.5-52.4 lb
• Open 579.0-631.0 N 130.2-141.9 lb
• Valve Spring Total Number of Coils 6.90-7.10

New Product Information
The purpose of New Product Information is to highlight or indicate important changes from the previous model year.

Changes may include one or more of the following items:

Torque values and/or fastener tightening strategies
Changed engine specifications
New sealants and/or adhesives
Disassembly and assembly procedure revisions
Engine mechanical diagnostic procedure revisions
New special tools required
A component comparison from the previous year
Torque Values and/or Fastener Tightening Strategies
The engine mechanical fastener tightening specifications have not changed for model year 2004.

Changed Engine Specifications
There are no changes to the engine specifications for 2004.

New Sealants and/or Adhesives
There are no changes to the sealants and/or adhesives used for model year 2004.

Disassembly and Assembly Procedure Revisions
The Lubrication System Priming Procedure has been replaced by the Lubrication Preluber Procedure. A new tool J 45299 has been developed to prime the engine with new clean engine oil.

Engine Mechanical Diagnostic Procedure Revisions
There are no revisions to the engine mechanical diagnostic procedures for 2004.

New Special Tools Required
*A new tool J 45299 has been developed to prime the engine with new clean engine oil.

*Ensure the proper bushing is used in the cylinder head bolt hole thread repair fixture plate. Refer to Thread Repair .

A Component Comparison from the Previous Year
The thread pitch on the M11 cylinder head bolts and the engine block cylinder head bolt holes has been revised for MY2004. Determine the pitch of the threads by using a thread pitch gage or measure the length of the threads of the cylinder head bolt.

*The MY2003 and earlier cylinder head bolts have a pitch of 1.5 mm and the length of the threads are about 48 mm (1.890 in) long.

*New for MY2004 the cylinder head bolts have a pitch of 2.0 mm and the length of the threads are about 67 mm (2.638 in) long.

*The grounding of the ignition coil assembly is assisted through the use of a grounding strap between the camshaft cover and the cylinder head.

*The right side ignition coil assembly has a sight shield cover.

*The fuel injector sight shield has been revised.

*The generator and A/C compressor have been revised.

*The engine block-to-crankcase seal and sealer placement have been revised.

*The AIR valves have been changed from vacuum to electronic operation.

*The exhaust valve head size has increased to 29 mm (1.141 in).


There are no component changes for 2005.

New Sealants and/or Adhesives
There are sealant changes for 2006.

• RTV GM P/N 12378521 (Canadian P/N 88901148) is used in the sealing groove of the block in place of the right and left seals between the block and the lower crankcase.

• Sealant GM P/N 1052942 (Canadian P/N 10953466) or GM P/N 1052943 (Canadian P/N 10953491) is no longer required along side of the seals between the block and the lower crankcase.

• On oil distribution plates with a molded-in outer seal RTV GM P/N 12378521 (Canadian P/N 88901148) is used on top of the outer seal between the oil distribution plate and the lower crankcase.

• On oil distribution plates without a molded-in outer seal RTV GM P/N 12378521 (Canadian P/N 88901148) is used in the outer sealing groove between the oil distribution plate and the lower crankcase.

• RTV GM P/N 12378521 (Canadian P/N 88901148) is used in the sealing groove of the oil pan in place of the seal.

Disassembly and Assembly Procedure Revisions
• There are no disassembly procedure changes for 2006.

• The tightening of the oil pan bolts has been revised to a two pass sequence.

Engine Mechanical Diagnostic Procedure Revisions
There are no revisions to the engine mechanical diagnostic procedures for 2006.

New Special Tools Required
There are new special tools required for 2006.

• The crankshaft rear seal removal tool J 42841-A has been revised to fit both small or large engine flywheel bolt holes in the crankshaft.

• The crankshaft rear seal installation tool J 45930-A has been revised to fit both small or large engine flywheel bolt holes in the crankshaft.

• The valve retainer removing and installation tool J 43059 has been replaced by J-43059-A .

• The piston pin clip remover and installation tool J 43654 has been replaced by EN-46745 .

• The piston ring compressor J 8037 has been replaced by EN-47701

A Component Comparison from the Previous Year
There are component changes for 2006.

• J 38816-A is no longer needed to remove and install the water pump. The water pump now bolts onto the water crossover.

• The throttle body is now Electronic Throttle Control (ETC).

• The exhaust intermediate pipe support bracket now bolts to the bottom of the oil pan.

There is a new special tool required for 2007.

A sealant applicator tool EN-48072 is being used prior to installation of the crankshaft rear oil seal
This is the only change for 2007

------------------
Cadillac Tech
ASE MASTER TECH since 1988

86 Northstar Fiero
85 RX7 former SCCA car
56 TR3 small mouth 6.0L
A.J. Whiteley

[This message has been edited by AJxtcman (edited 02-23-2007).]

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AJxtcman

1098 posts
Member since Nov 2006
2004 to 2007 VIN 9
Mechanical Specifications (L37)
Application Specification
Metric English
General
• Engine Type V-8
• Displacement 4.6 Liter 279 cu in
• RPO L37
• VIN 9
• Bore 93 mm 3.661 in
• Stroke 84 mm 3.3071 in
• Compression Ratio 10.0:1
• Engine Compression Test 965-1172 kPa 140-170 psi
• Firing Order 1-2-7-3-4-5-6-8
• Spark Plug Gap 1.270 mm 0.0500 in
Block
• Crankshaft Main Bearing Bore Diameter 72.430-72.442 mm 2.8516-2.8521 in
• Crankshaft Main Bearing Bore Out-of-Round 0.010 mm 0.0004 in
• Crankshaft Main Rear Oil Seal
• Bore 115.962-116.038 mm 4.5654-4.5684 in
• Runout 0.250 mm 0.0098 in
• Cylinder Bore Diameter @ 41 mm (1.610 in) Below Deck Face 92.992-93.008 mm 3.6611-3.6617 in
• Cylinder Bore Out-of-Round
• Production 0.010 mm 0.0004 in
• Service 0.100 mm 0.0039 in
• Cylinder Bore Taper
• Production 0.010 mm 0.0004 in
• Service 0.100 mm 0.0039 in
• Cylinder Head Deck Height 224.55 mm 8.8406 in
• Cylinder Head Deck Surface Flatness 0.100 mm 0.0039 in
Camshaft
• Camshaft End Play 0.120-0.220 mm 0.0050-0.0087 in
• Camshaft Journal Diameter 26.948-26.972 mm 1.0610-1.0619 in
• Camshaft Journal Out-of-Round 0.006 mm 0.0002 in
• Camshaft Journal to Bore Clearance
• Production 0.051-0.076 mm 0.0020-0.0030 in
• Service 0.040-0.090 mm 0.0016-0.0035 in
• Camshaft Lobe Duration @ 0.150 mm (0.006 in) Lift - Exhaust 246 degrees
• Camshaft Lobe Duration @ 0.150 mm (0.006 in) Lift - Intake 251 degrees
• Camshaft Lobe Lift - Exhaust 5.94 mm 0.2339 in
• Camshaft Lobe Lift - Intake 6.15 mm 0.2421 in
• Camshaft Lobe Overlap @ 0.150 mm (0.006 in) Lift 2.04 degrees
• Camshaft Runout 0.050 mm 0.0020 in
• Camshaft Thrust Surface
• Runout 0.037 mm 0.0015 in
• Width 22.990-23.090 mm 0.9051-0.9091 in
• Camshaft Timing @ 0.150 mm (0.006 in) Lift
• Intake Opens 0.3 degrees ATDC
• Intake Centerline 122.0 degrees ATDC
• Intake Closes 246.0 degrees ATDC
• Exhaust Opens 229.3 degrees BTDC
• Exhaust Centerline 110.0 degrees BTDC
• Exhaust Closes 11.2 degrees ATDC
Cooling System
• Thermostat Full Open Temperature 85°C 185°F
Connecting Rod
• Connecting Rod Bearing Clearance
• Production and Service 0.0250-0.0760 mm 0.0010-0.0030 in
• Connecting Rod Bore Diameter - Bearing End 57.136-57.152 mm 2.2495-2.2501 in
• Connecting Rod Bore Diameter - Pin End 23.002-23.014 mm 0.9056-0.9061 in
• Connecting Rod Bore Out-of-Round - Bearing End 0.006 mm 0.0002 in
• Connecting Rod Bore Out-of-Round - Pin End 0.005 mm 0.0002 in
• Connecting Rod Length Center to Center 151.00 mm 5.9449 in
• Connecting Rod Side Clearance 0.200-0.500 mm 0.0079-0.0197 in
• Connecting Rod Straightness 0.050 mm 0.0020 in
Crankshaft
• Connecting Rod Journal Diameter 53.947-53.963 mm 2.1239-2.1245 in
• Connecting Rod Journal Out-of-Round 0.005 mm 0.0002 in
• Connecting Rod Journal Taper 0.005 mm 0.0002 in
• Connecting Rod Journal Width 43.840-43.960 mm 1.7260-1.7307 in
• Crankshaft Balancer
• Surface Diameter 50.730-50.870 mm 1.9972-2.0028 in
• Hub Inside Diameter 34.847-34.864 mm 1.3719-1.3726 in
• Crankshaft End Play 0.050-0.500 mm 0.0020-0.0197 in
• Crankshaft Main Bearing Clearance
• Production 0.0150-0.0550 mm 0.0006-0.0022 in
• Service 0.0150-0.0635 mm 0.0006-0.0025 in
• Crankshaft Main Journal Diameter 64.350-64.366 mm 2.5335-2.5341 in
• Crankshaft Main Journal Out-of-Round 0.005 mm 0.0002 in
• Crankshaft Main Journal Taper 0.005 mm 0.0002 in
• Crankshaft Main Journal Thrust Wall Runout 0.040 mm 0.0016 in
• Crankshaft Main Journal Thrust Wall Square 0.010 mm 0.0004 in
• Crankshaft Main Journal Width, #1, #2, #4, #5 24.540-24.660 mm 0.9661-0.9709 in
• Crankshaft Main Journal Width, Thrust #3 25.150-25.250 mm 0.9902-0.9941 in
• Crankshaft Nose Diameter
• From Front Face 0.00-21.00 mm (0.0000-0.8268 in) 34.500-34.750 mm 1.3583-1.3681 in
• From Front Face 21.00-53.00 mm (0.8268-2.0866 in) 34.892-34.912 mm 1.3737-1.3745 in
• From Front Face 53.00 to Rolled Fillet (2.0866-Rolled Fillet) 33.450-33.550 mm 1.3169-1.3209 in
• From Front Face 89.94-110.54 mm (3.5409-4.3520 in) 44.950-45.000 mm 1.7697-1.7717 in
• Crankshaft Nose Runout
• From Front Face 0.00-21.00 mm (0.0000-0.8268 in) 0.100 mm 0.0039 in
• From Front Face 21.00-53.00 mm (0.8268-2.8066 in) 0.030 mm 0.0012 in
• From Front Face 53.00 to Rolled Fillet (2.0866-Rolled Fillet) 0.100 mm 0.0039 in
• From Front Face 89.94-110.54 mm (3.5409-4.3520 in) 0.025 mm 0.0010 in
• Crankshaft Rear Flange
• Diameter 95.880-95.980 mm 3.7748-3.7787 in
• Runout 0.025 mm 0.0010 in
• Crankshaft Rear Flange Face to Engine Flywheel Runout 0.025 mm 0.0010 in
• Crankshaft Runout
• Main Journals #1, #5 0.022 mm 0.0009 in
• Main Journals #2, #4, #6 0.025 mm 0.0010 in
Cylinder Head
• Camshaft Bearing Bore Diameter 27.013-27.033 mm 1.0635-1.0642 in
• Camshaft Bearing Bore Out-of-Round 0.010 mm 0.0004 in
• Combustion Chamber Depth - at Measurement Point 10.470-10.710 mm 0.4122-0.4217 in
• Cylinder Head Height - Deck to Camshaft Centerline Bore 136.00 mm 5.3543 in
• Surface Flatness - Block Deck 0.050 mm 0.0020 in
• Surface Flatness - Exhaust Manifold Deck 0.220 mm 0.0087 in
• Surface Flatness - Intake Manifold Deck 0.220 mm 0.0087 in
• Valve Guide Bore - Exhaust 5.969-5.989 mm 0.2350-0.2359 in
• Valve Guide Bore - Intake 5.969-5.989 mm 0.2350-0.2359 in
• Valve Guide Installed Height - Exhaust 14.300 mm 0.5630 in
• Valve Guide Installed Height - Intake 14.720 mm 0.5795 in
• Valve Lifter Bore Diameter 12.013-12.037 mm 0.4730-0.4739 in
Exhaust Manifold
Flywheel
• Runout 0.300 mm 0.0118 in
Intake Manifold
• Surface Flatness 0.500 mm 0.0200 in
Lubrication System
• Oil Capacity - with Filter 7.098 Liter 7.5 Quarts
• Oil Capacity - without Filter 6.625 Liter 7.0 Quarts
Oil Pump
• Oil Pressure - Minimum @ Idle 35 kPa 5 psi
• Oil Pressure - Minimum @ 2,000 RPM 250 kPa 35 psi
Piston Rings
• Piston Ring End Gap
• First Compression Ring 0.250-0.400 mm 0.0098-0.0157 in
• Second Compression Ring 0.350-0.050 mm 0.0138-0.0020 in
• Oil Control Ring 0.250-0.760 mm 0.0098-0.0299 in
• Piston Ring to Groove Clearance
• First Compression Ring 0.040-0.095 mm 0.0016-0.0037 in
• Second Compression Ring 0.040-0.095 mm 0.0016-0.0037 in
• Oil Control Ring None - Side Sealing
• Piston Ring Thickness
• First Compression Ring 1.199-1.203 mm 0.0472-0.0474 in
• Second Compression Ring 1.499-1.504 mm 0.0590-0.0592 in
• Oil Control Ring 2.530-2.555 mm 0.0996-0.1006 in
Pistons and Pins
• Piston
• Piston Diameter @ 42 mm (1.6353 in) Below Crown 92.957-92.972 mm 3.6597-3.6603 in
• Piston Pin Bore Diameter 23.002-23.007 mm 0.9056-0.9058 in
• Piston Ring Groove Inside Diameter
• First Compression Ring 84.750-85.000 mm 3.3366-3.3464 in
• Second Compression Ring 83.400-83.650 mm 3.2835-3.2933 in
• Oil Control Ring 85.670-85.920 mm 3.3728-3.3827 in
• Piston Ring Groove Width
• First Compression Ring 1.230-1.255 mm 0.0484-0.0494 in
• Second Compression Ring 1.530-1.555 mm 0.0602-0.0612 in
• Oil Control Ring 2.530-2.555 mm 0.0996-0.1006 in
• Piston to Bore Clearance 0.020-0.051 mm 0.0008-0.0020 in
• Pin
• Piston Pin Clearance to Connecting Rod Bore 0.002-0.014 mm 0.0001-0.0006 in
• Piston Pin Clearance to Piston Pin Bore 0.002-0.012 mm 0.0001-0.0005 in
• Piston Pin Diameter 22.995-23.000 mm 0.9053-0.9055 in
• Piston Pin End Play
• Piston Pin Length 61.500-62.000 mm 2.4213-2.4409 in
Starter
Valve System
• Valves
• Valve Face Angle 45 degrees
• Valve Face Runout 0.038 mm 0.0015 in
• Valve Face Width
• Exhaust 1.500 mm 0.0591 in
• Intake 1.000 mm 0.0394 in
• Valve Head Diameter
• Exhaust 28.880-29.140 mm 1.1370-1.1472 in
• Intake 36.090-36.350 mm 1.4209-1.4311 in
• Valve Length
• Exhaust 91.730-91.990 mm 3.6114-3.6217 in
• Intake 110.600-110.860 mm 4.3543-4.3646 in
• Valve Seat Angle 45.75 degrees
• Valve Seat Relief Angle 20 degrees
• Valve Seat Relief Width
• Exhaust 0.160-0.360 mm 0.0063-0.0142 in
• Intake 0.110-0.310 mm 0.0043-0.0118 in
• Valve Seat Runout 0.050 mm 0.0020 in
• Valve Seat Undercut Angle
• Exhaust 65 degrees
• Intake 60 degrees
• Valve Seat Width
• Exhaust 1.300-1.700 mm 0.0512-0.0669 in
• Intake 0.420-0.820 mm 0.0165-0.0323 in
• Valve Stem Diameter 5.920-5.940 mm 0.2331-0.2339 in
• Valve Stem Out-of-Round 0.008 mm 0.0003 in
• Valve Stem Straightness 0.013 mm 0.0005 in
• Valve Stem-to-Guide Clearance
• Exhaust
• Production 0.050-0.100 mm 0.0020-0.0039 in
• Service 0.050-0.120 mm 0.0020-0.0047 in
• Intake
• Production 0.028-0.068 mm 0.0011-0.0027 in
• Service 0.028-0.110 mm 0.0011-0.0043 in
• Valve Lifters
• Valve Lifter Diameter 11.986-12.000 mm 0.4719-0.4724 in
• Valve Lifter-to-Bore Clearance 0.037-0.041 mm 0.0015-0.0016 in
• Rocker Arms
• Valve Rocker Arm Ratio 1.68 to 1
• Valve Rocker Arm Roller Diameter 17.740-17.800 mm 0.6984-0.7008 in
• Valve Springs
• Valve Spring Coil Thickness 4.110 x 3.280 mm 0.1618 x 0.1291 in
• Valve Spring Diameter
• Inside 17.750-18.250 mm 0.6988-0.7185 in
• Outside 26.23 mm 1.0327 in
• Valve Spring Free Length 40.790-43.690 mm 1.6059-1.7201 in
• Valve Spring Height
• Closed 35.000 mm 1.3780 in
• Open 24.500 mm 0.9646 in
• Valve Spring Load
• Closed 211.4-233.4 mm 47.5-52.4 lb
• Open 579.0-631.0 mm 130.2-141.9 lb
• Valve Spring Total Number of Coils 6.90-7.10

New Product Information Same as VIN Y above
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ryan.hess
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Report this Post02-23-2007 09:32 AM Click Here to See the Profile for ryan.hessSend a Private Message to ryan.hessDirect Link to This Post
Crank reluctor wheel measurements?
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AJxtcman
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Report this Post02-23-2007 07:41 PM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post
This will start as VIN Y & 9 engine controls
I hope the info is in here Ryan.
2000 Cadillac DeVille - Engine - Engine Controls - 4.6L - Description and Operation
Catagories list
Powertrain Control Module (PCM)
Information Sensors/Switches Description
Powertrain Control Module Controlled Air Conditioning
Knock Sensor (KS) System
Electric Cooling Fan
Electronic Ignition (EI) System
Air Induction System
Fuel System Description
Fuel Supply Component Description
Fuel Metering Modes of Operation
Fuel Metering System Component Description
Evaporative Emission Control System
Secondary Air Injection System Description
Exhaust Gas Recirculation (EGR) System
Crankcase Ventilation System

Powertrain Control Module (PCM)
Powertrain
The powertrain used in this vehicle consists of a twin cam V8 engine mated to a 4T80-E transaxle. The powertrain has electronic controls to reduce exhaust emissions while maintaining excellent driveability and fuel economy. The powertrain control module (PCM) manages the operation of the engine control system.

The powertrain control module is designed to maintain exhaust emission levels to Federal or California standards while providing excellent driveability and fuel efficiency. Review the components and wiring diagrams in order to determine which systems are controlled by the PCM. The PCM monitors numerous engine and vehicle functions. The following are some of the functions that the PCM controls:

• Engine fueling

• Ignition control (IC)

• Knock sensor (KS) system

• Evaporative Emission (EVAP) system

• Secondary Air Injection (AIR) system (if equipped)

• Exhaust Gas Recirculation (EGR) system

• Automatic transmission functions

• A/C clutch control

• Cooling fan control

Powertrain Control Module Function
The PCM constantly looks at the information from various sensors and other inputs, and controls systems that affect vehicle performance and emissions. The PCM also performs diagnostic tests on various parts of the system. The PCM can recognize operational problems and alert the driver via the malfunction indicator lamp (MIL). When the PCM detects a malfunction, it stores a diagnostic trouble code (DTC). The problem area is identified by the particular DTC that is set. The PCM supplies a buffered voltage (5V or 12V) to various sensors and switches. The input and output devices in the control module include analog to digital converters, signal buffers, counters, multiple function drivers, and output drivers. The multiple function drivers (i.e., EGR control, fuel pump relay) are electronic switches that supply ignition voltage to energize the circuit. The output drivers are electronic switches that, when energized, complete the ground path. Most PCM controlled components are operated via output drivers. The PCM monitors these driver circuits for proper operation. In most cases, if a problem is detected, a DTC corresponding to the controlled device will set.

Torque Management
Torque management is a function of the PCM that reduces engine power under certain conditions. Torque management is performed for three reasons:

• To prevent overstress of powertrain components

• To limit engine power when brakes are applied

• To prevent damage to the vehicle during certain abusive maneuvers

The PCM uses manifold vacuum, intake air temperature, spark retard, engine speed, engine coolant temperature, A/C clutch status, and EGR valve position to calculate engine output torque. It then looks at torque converter status, transaxle gear ratio, and brake switch inputs and determines if any torque reduction is required. If torque reduction is required, the PCM retards spark as appropriate to reduce engine torque output. In the case of abusive maneuvers, the PCM may also shut off fuel to certain cylinders to reduce engine power.

There are four instances when engine power reduction is likely to be experienced:

• During transaxle upshifts and downshifts

• Heavy acceleration from a standing start

• If brakes are applied with moderate to heavy throttle

• When the driver is performing stress-inducing (abusive) maneuvers such as shifting into gear at high throttle angles

In the first two instances, the driver is unlikely to even notice the torque management actions. In the other cases, engine power output will be moderate at full throttle.

When the PCM determines that engine power reduction is required, it calculates the amount of spark retard necessary to reduce power by the desired amount. This spark retard is then subtracted from the current spark advance. In the case of abusive maneuvers, the PCM will momentarily disable fuel injectors to obtain the necessary amount of torque reduction.

Traction Control
Traction control is a function of the PCM and electronic brake and traction control module (EBTCM) to reduce wheel slip during acceleration. When wheel slip is detected, the EBTCM applies the front brakes, and the PCM reduces engine power. Refer to Diagnostic System Check - ABS in Antilock Brake System for an explanation of the EBTCMs role in traction control. The PCM continuously sends the EBTCM a PWM signal to indicate the torque output of the powertrain. This signal, referred to as the Delivered Torque signal, is used by the EBTCM to determine the required action when it sees the front wheels slipping. The EBTCM may decide to apply the front brakes only, or apply the front brakes and signal the PCM to reduce the torque output of the powertrain. The EBTCM requests reduced torque using another PWM signal. This signal, referred to as the Desired Torque signal, is used by the PCM to determine the amount of torque reduction requested by the EBTCM. The PCM adjusts the ignition timing in response to the Desired Torque signal.

The Desired Torque signal varies within a range of 95 percent and 5 percent duty cycle. A duty cycle at 95 percent indicates no torque reduction. A duty cycle at 10 percent indicates full torque reduction. The Desired Torque signal to the PCM will normally be at a 90 percent duty cycle. The EBTCM will decrease the duty cycle of the signal by the amount of torque reduction desired. The PCM responds to the signal by adjusting the ignition timing. The PCM may shut off the fuel to one or more cylinders unless the following conditions are present:

• The coolant temperature is below -40°C (-40°F) or above 131°C (268°F).

• A low coolant level is present.

• The engine speed is below 600 RPM.

The PCM will re-enable the fuel injectors as the need for traction control ends.

Traction control will be disable when certain DTCs set. The PCM will request a TRACTION OFF light/message via Class 2 serial data when the DTCs set.

Class 2 Serial Data
The Class 2 serial data circuit allows the control modules to communicate with each other. The modules send a series of digital signals pulsed from high to low voltage (approximately 7 volts to 0 volts). These signals are sent in variable pulse widths of one or two bits. A string of these bits creates a message that is sent in a prioritized data packet. This allows more than one module to send messages at the same time without overloading the serial data line.

The speed, or BAUD rate, at which the control modules communicate depends on the message content. Large message content lowers the BAUD rate while small message content increases the BAUD rate. The average BAUD rate is approximately 10.4 kps (10,400 bits per second).

When the key is ON, each module sends a State of Health message to the other control modules using the Class 2 serial data line. This ensures that the modules are working properly. When the module stops communicating, a loss of the state of health message occurs. The control modules that expect to receive the message detect the loss, and will set a loss of the state of health diagnostic trouble code (DTC).

Data Link Connector (DLC)
The data link connector (DLC) provides a Class 2 data circuit that allows bi-directional communication between the scan tool, the PCM, and other system control modules. Usually located under the instrument panel, the DLC provides power and ground for the scan tool. Some common uses of the scan tool are listed below:

• Identifying stored diagnostic trouble codes (DTCs)

• Clearing DTCs

• Performing output control tests

• Reading serial data for diagnostic analysis

Service Engine Soon/Malfunction Indicator Lamp (MIL)
The service engine soon/malfunction indicator lamp (MIL) is located in the instrument panel cluster (IPC). The MIL is controlled by the PCM and is used to indicate that the PCM has detected a problem that affects vehicle emissions, may cause powertrain damage, or severely impacts driveability.

Trip
A trip is an interval of time during which the diagnostic test runs. A trip may consist of only a key cycle to power up the PCM, allow the diagnostic to run, then cycle the key off to power down the PCM. A trip may also involve a PCM power up, meeting specific conditions to run the diagnostic test, then powering down the PCM. The definition of a trip depends on the diagnostic. Some diagnostic tests run only once per trip (i.e., catalyst monitor) while other tests run continuously during each trip (i.e., misfire, fuel system monitors).

Warm-up Cycle
The PCM uses warm-up cycles to run some diagnostics, and to clear any diagnostic trouble codes (DTCs). A warm-up cycle occurs when the engine coolant temperature raises 22°C (40°F) from start-up. The engine coolant must also achieve a minimum temperature of 71°C (160°F). The PCM counts the number of warm-up cycles in order to clear the malfunction indicator lamp (MIL). The PCM will clear the DTCs when 40 consecutive warm-up cycles occur without a malfunction.

Diagnostic Trouble Code Display
DTCs can only be displayed with the use of a scan tool.

DTC Status
When the scan tool displays a DTC, the status of the DTC is also displayed. The following DTC statuses will be indicated only when they apply to the DTC that is set.

Fail This Ign. (Fail This Ignition): Indicates that this DTC failed during the present ignition cycle.

Last Test Fail: Indicates that this DTC failed the last time the test ran. The last test may have run during a previous ignition cycle if an A or B type DTC is displayed. For type C DTCs, the last failure must have occurred during the current ignition cycle to appear as Last Test Fail.

MIL Request: Indicates that this DTC is currently requesting the MIL. This selection will report type B DTCs only when they have requested the MIL. (failed twice).

Test Fail SCC (Test Failed Since Code Clear): Indicates that this DTC that has reported a failure since the last time DTCs were cleared.

History: Indicates that the DTC is stored in the PCMs History memory. Type B DTCs will not appear in History until they have requested the MIL (failed twice). History will be displayed for all type A DTCs and type B DTCs (which have requested the MIL) that have failed within the last 40 warm-up cycles. Type C DTCs that have failed within the last 40 warm-up cycles will also appear in History.

Not Run SCC (Not Run Since Code Clear): DTCs will be listed in this category if the diagnostic has not run since DTCs were last cleared. This status is not included with the DTC display since the DTC can not be set if the diagnostic has not run. This information is displayed when DTC Info is requested using the scan tool.


Clearing Diagnostic Trouble Codes
Use a scan tool to clear DTCs from the PCM memory. Disconnecting the vehicle battery to clear the PCM memory is not recommended. This may or may not clear the PCM memory and other vehicle system memories will be cleared. Do not disconnect the PCM connectors solely for clearing DTCs. This unnecessarily disturbs the connections and may introduce a new problem. Before clearing DTCs the scan tool has the capability to save any data stored with the DTCs and then display that data at a later time. Capture DTC info before beginning diagnosis (refer to Capturing DTC Info). Do not clear DTCs until you are instructed to do so within a diagnostic procedure.

Many PCM DTCs have complex test and failure conditions. Therefore, simply clearing DTCs and watching to see if the DTC sets again may not indicate whether a problem has been corrected. To verify a repair after it is complete, you must look up the test conditions and duplicate those conditions. If the DTC runs and passes, chances are good that the problem is fixed.

Freeze Frame Data
Government regulations require that engine operating conditions be captured whenever the MIL is illuminated. The data captured is called Freeze Frame data. The Freeze Frame data is very similar to a single record of operating conditions. Whenever the MIL is illuminated, the corresponding record of operating conditions is recorded as Freeze Frame data. A subsequent failure will not update the recorded information.

The Freeze Frame data parameters stored with a DTC failure include the following:

• Air fuel ratio

• Mass air flow sensor

• Fuel trim (both short term and long term for both cylinder banks)

• Engine speed

• Intake air temperature

• Engine coolant temperature

• Vehicle speed

• TP angle

• MAP/BARO

• Fuel System status

Freeze frame data can only be overwritten with data associated with a misfire or fuel trim malfunction. Data from these faults take precedence over data associated with any other fault. The Freeze Frame data will not be erased unless the associated history DTC is cleared.

Failure Records Data
When a diagnostic test fails, the PCM stores the information as Failure Records data. Unlike Freeze Frame data, Failure Records are stored for multiple DTCs or non-emission related DTCs (DTCs that do not illuminate the MIL). The Failure Records information is updated the first time the test fails during each ignition cycle.

Important: Always capture the Freeze Frame and Failure Records information with the scan tool BEFORE proceeding with diagnosis. Loss of this data may prevent accurate diagnosis of an intermittent condition.


Freeze Frame/Failure Records data may be retrieved through the scan tool. If more than one DTC is set review the odometer or engine run time data located in the Freeze Frame/Failure Records info to determine the most current failure. The stored information will look like normal PCM data.

Capturing DTC Info (Capture Info)
Selecting this option on the scan tool allows the technician to record the Freeze Frame and Failure Records that may be stored in the PCMs memory. Capture DTC info before beginning diagnosis. This is a step in the OBD System Check. At the end of the diagnostic tables, you are instructed to clear DTCs, verify that the repair was successful and then to review captured information. The captured information will contain any additional DTCs and related data that was stored originally (if multiple DTCs were stored).

Storing And Erasing Freeze Frame Data
Government regulations require that engine operating conditions be captured whenever the MIL is illuminated. The data captured is called freeze frame data. The freeze frame data is very similar to a single record of operating conditions. Whenever the MIL is illuminated, the corresponding record of operating conditions is recorded to the freeze frame buffer.

Each time a diagnostic test reports a failure, the current engine operating conditions are recorded in the freeze frame buffer. A subsequent failure will update the recorded operating conditions. The following operating conditions for the diagnostic test which failed typically include the following parameters:

• Air fuel ratio

• Air flow rate

• Fuel trim

• Engine speed

• Engine load

• Engine coolant temperature

• Vehicle speed

• TP angle

• MAP/BARO

• Injector base pulse width

• Loop status

Freeze frame data can only be overwritten with data associated with a misfire or fuel trim malfunction. Data from these faults take precedence over data associated with any other fault. The freeze frame data will not be erased unless the associated history DTC is cleared.

Storing and Erasing Failure Records Data
When a PCM DTC sets, the PCM does several things. Among them is to save useful data and input parameter information for service diagnosis. This information is referred to as Freeze Frame/Failure Records. You will see references to these in many PCM DTC diagnostic tables because this information can be useful in pinpointing a problem even if the problem is not present when the vehicle is in the service bay.

Freeze Frame/Failure Records data may be retrieved through the DTC menu on scan tool. If more than one DTC is set review the odometer or engine run time data located in the Freeze Frame/Failure Records info to determine the most current failure.

Keep in mind that once Freeze Frame or Failure Record is selected, the parameter and input data displayed will look just like the normal PCM data except the parameters will not vary since it is displaying stored data.

Capturing DTC Info (Capture Info)
Selecting this option on the scan tool allows the technician to record the Freeze Frame and Failure Records that may be stored in the PCMs memory. This can be useful if the PCM or battery must be disconnected and later review of the stored information may be desired.

PCM Snapshot Using A Scan Tool
The scan tool can be set up to take a snapshot of the parameters available via serial data. The snapshot function records live data over a period of time. The recorded data can be played back and analyzed. The scan tool can also graph parameters singly or in combinations of parameters for comparison. The snapshot can be triggered manually at the time a symptom is noticed, or set up in advance to trigger when a DTC sets. An abnormal value captured in the recorded data may point to a system or component that needs to be investigated further. The snapshot will remain in the scan tool memory even after the tool is disconnected from its power source. Refer to the scan tool user instructions for more information on the snapshot function.

Information Sensors/Switches Description
A/C Pressure Sensor
The PCM uses the A/C pressure sensor to monitor the high pressure side of the A/C system. The PCM supplies the sensor with a 5 volt reference and a ground. The sensor returns a signal voltage relative to the A/C refrigerant pressures. The PCM uses this information to turn ON the engine coolant fans when the A/C pressure is too high. If the sensor indicates that the A/C refrigerant pressure is too high or too low, the PCM will disengage the A/C compressor. If the PCM detects an A/C pressure sensor signal above or below the possible range of the sensor, DTC P0532 or DTC P0533 will set.

Crank Request
The crank request circuit is used to signal the PCM that the ignition switch is in the START position. With the ignition switch in the OFF position, the PCM should detect zero volts on the crank request circuit. With the ignition switch in the START position, the crank request circuit applies a fused ignition voltage to the PCM. The PCM uses the crank request signal, and other inputs to decide whether, or not to allow starter operation.

Engine Coolant Temperature (ECT) Sensor




The engine coolant temperature (ECT) sensor is a thermistor mounted in the engine coolant stream. The ECT sensor resistance varies from 100,000 ohms at -40°C (-40°F) to 70 ohms at 130°C (266°F). The PCM uses the ECT signal to calculate the coolant temperature. The PCM applies 5 volts to the ECT signal circuit through a pull-up resistor. When the engine coolant temperature is cold, the ECT sensor resistance is high. This causes the PCM to detect a high ECT signal voltage. When the engine coolant temperature increases, the sensor resistance lowers. The PCM should detect a low ECT signal voltage

The scan tool displays the engine coolant temperature in degrees. After engine startup, the coolant temperature should steadily rise to approximately 90°C (194°F). Then, when the thermostat opens, the temperature should stabilize. If the engine has not been run for several hours (overnight), the ECT sensor and IAT sensor scan tool displays should read close to each other. Engine coolant temperature affects most PCM controlled systems. A hard fault in the ECT sensor circuit should set DTC P0117 or P0118. An intermittent fault should set DTC P1114 or DTC P1115. To check ECT sensor resistance relative to temperature, refer to the Temperature vs Resistance table.

EGR Pintle Position Sensor
The EGR pintle position sensor is potentiometer used to indicate the amount of EGR valve opening. The PCM supplies the pintle position sensor with a 5 volt reference and a ground. The pintle position sensor provides a signal voltage to the PCM. By monitoring the voltage on the signal line, the PCM is able to determine if the EGR valve responds properly to commands from the PCM. As the EGR valve position changes, the pintle position signal voltage will change. With the EGR valve closed, the signal voltage is near 0 volts. However, the pintle position signal voltage increases as the EGR valve opens. When the PCM commands the EGR valve fully open, the pintle position signal voltage should be above 4 volts. If the PCM detects an excessively low pintle position signal voltage (circuit is open or shorted to ground), DTC P0405 will set.

When the ignition switch is in the RUN position, the PCM learns the EGR closed valve pintle position. When the PCM commands the EGR valve closed, the PCM compares the closed valve pintle position to the actual EGR position. If the actual EGR position indicates that the EGR valve is still open, DTC P1404 will set.

The PCM controls the EGR valve using an ignition voltage driver and ground located within the PCM. When the PCM commands the EGR valve open, the PCM compares the actual EGR position to the desired EGR position. If the actual EGR is less than the desired EGR by a calibrated amount, DTC P0404 will set. If an electrical malfunction occurs in the EGR valve control circuit, DTC P0403 will set.

Engine Oil Pressure Sensor
The engine oil pressure sensor is a rheostat mounted in the oil filter adapter. The PCM supplies the sensor with a 5 volt reference and a ground. The sensor varies the 5 volt input voltage relative to the oil pressure at various engine speeds. The PCM uses the signal voltage to calculate the amount of fuel in the tank.

The PCM sends the oil pressure information via Class 2 to the instrument panel cluster (IPC). The IPC uses the information to control the oil pressure indicator.

Fuel Tank Pressure Sensor
The PCM monitors the fuel tank pressure sensor to detect vacuum decay and excess vacuum during the EVAP system tests. The fuel tank pressure sensor measures the difference between the air pressure (or vacuum) in the tank and the outside air pressure. The PCM supplies a 5 volt reference and a ground for the fuel tank pressure sensor. The fuel tank pressure sensor provides a signal to the PCM that ranges between 0.1 and 4.9 volts.

Fuel Level Sensor PCM
The fuel level sensor is a rheostat mounted on the fuel sender assembly. The PCM supplies the sensor with a 5 volt reference and a ground. The sensor varies the 5 volt input voltage based on the level of fuel in the tank. The PCM uses the signal voltage to calculate the amount of fuel in the tank.

The fuel level sensor is part of the fuel sender assembly. The PCM uses the fuel level input to make sure that the level of fuel in the tank is sufficient to run the EVAP tests. The PCM also sends the fuel level information via Class 2 to the instrument panel cluster (IPC). The IPC uses the information to control the fuel level gauge.

The PCM performs the key ON and RUN tests to determine the status of the L-terminal circuit. During the key ON test, if the PCM detects a high signal voltage, DTC P0621 will set. DTC P0621 will also set if, during the RUN test, the PCM detects a low signal voltage. The PCM also sends a Class 2 serial data message to illuminate the charging telltale.

Generator L Terminal
The L-terminal circuit connects the generator to the PCM. The PCM applies ignition voltage to the L-terminal signal circuit through a resistor. The PCM should detect a low signal voltage input when the key is in the RUN position with the engine OFF, or when the charging system malfunctions. During engine operation, the PCM should detect a high signal voltage.

Generator F Terminal
The F-terminal circuit connects the generator to the PCM. The PCM uses this circuit to monitor the pulse width modulation (PWM) of the field circuit. When the key is in the RUN position and the engine is OFF, the PCM should detect a duty cycle near 0 percent. However, when the engine is running, the duty cycle should be between 5 percent and 100 percent.

The PCM monitors the PWM signal using a key ON test and a RUN test. During each test, if the PCM detects an out of range PWM signal, DTC P0622 will set. When the DTC sets, the PCM will send a Class 2 serial data message to illuminate the appropriate telltales.

Heated Oxygen Sensors (HO2S)
The heated oxygen sensors allow the PCM to maintain an air/fuel ratio that provides the best performance, fuel economy, and emission control. There are three heated oxygen sensors mounted in the exhaust gas stream. HO2S bank 1 sensor 1 and bank 2 sensor 1 are mounted in the right and left exhaust manifolds. HO2S bank 1 sensor 2 is mounted in the exhaust pipe after the converter. These sensors produce a voltage due to the difference in oxygen content between the air and the exhaust gas stream.

The PCM uses the fuel control heated oxygen sensors (HO2S bank 1 sensor 1 and bank 2 sensor 1) to decide what fuel mixture command to give the fuel injectors. The PCM supplies a 450 millivolt reference voltage to the sensors. The sensors vary the reference voltage in response to the oxygen content in the exhaust gas stream. When the oxygen content is low (a rich condition), the PCM will detect a signal voltage near 900 millivolts. When the oxygen content is high (a lean condition), the PCM will detect a signal voltage near 100 millivolts. The PCM adjusts the injector pulse width to correct for a rich or a lean condition. The PCM uses HO2S bank 1 sensor 2 to determine how well the three-way catalyst is controlling emissions.

The PCM compares the signals from HO2S bank 1 sensor 1 and bank 2 sensor 1 to the signal from HO2S bank 1 sensor 2. If the catalyst is operating efficiently, the PCM should detect a HO2S bank 1 sensor 2 signal less active than the signals from HO2S bank 1 sensor 1 and bank 2 sensor 1.

Intake Air Temperature (IAT) Sensor




The intake air temperature (IAT) sensor is a thermistor integrated with the mass air flow (MAF) sensor. The IAT sensor resistance varies from 100,000 ohms at 40°C (40°F) to 70 ohms at 130°C (266°F). The PCM uses the IAT signal to calculate the intake air temperature. The PCM applies 5 volts to the IAT signal circuit through a pull-up resistor. When the intake temperature is cold, the IAT sensor resistance is high. This causes the PCM to detect a high IAT signal voltage. As the underhood temperatures increase, the IAT sensor resistance lowers. The PCM should detect a low IAT signal voltage.

The scan tool displays the intake air temperature in degrees. The IAT sensor display should read close to ambient air temperature when the engine is cold. As the underhood temperature increases, the IAT sensor display should also increase. If the engine has not been run for several hours (overnight), the IAT sensor and ECT sensor scan tool displays should read close to each other. A hard fault in the IAT sensor circuit should set DTC P0112 or P0113. An intermittent fault should set DTC P1111 or DTC P1112. To check IAT sensor resistance relative to temperature, refer to the Temperature vs Resistance table.

Manifold Absolute Pressure (MAP) Sensor




The manifold absolute pressure (MAP) sensor responds to changes in intake manifold pressure. The PCM supplies a 5 volt reference and a ground for the MAP sensor. The MAP sensor provides a signal to the PCM relative to the pressure changes in the manifold. The MAP sensor signal voltage to the PCM varies from below 2 volts at idle (low manifold absolute pressure - high vacuum) to above 4 volts with the key ON, engine not running or at wide-open throttle (high manifold absolute pressure - low vacuum).

If the PCM detects a voltage that is lower than the possible range of the MAP sensor, DTC P0107 will set. A signal voltage higher that the possible range of the MAP sensor will set DTC P0108. An intermittent low or high voltage will set DTC P1107 or P1106 respectively.

Mass Air Flow (MAF) Sensor




The mass air flow (MAF) sensor measures the amount of air flow into the engine in a given time. The MAF sensor produces a signal as air passes through the sensor and into the engine. The amount of air flow determines the frequency of the signal. If the air flow through the sensor increases, the frequency of the signal will increase. If the air flow through the sensor decreases, the frequency of the signal will decrease. Normally, the frequency will vary from approximately 2000 hertz at idle to about 10,000 hertz at maximum engine load. The PCM uses the MAF sensor information to provide the correct fuel delivery for all engine operating conditions.

The scan tool displays the MAF value in grams per second (g/s). At idle, the scan tool should display a MAF value of 4 g/s - 7 g/s on a fully warmed engine. Values should change rather quickly on acceleration. However, the values should remain fairly stable at any given RPM.

If the PCM detects a signal frequency lower than the possible range of a normally operating MAF sensor, DTC P0102 will set. If the PCM detects a signal frequency higher than the possible range of a normally operating MAF sensor, DTC P0103 will set. If the actual MAF sensor frequency does not match a PCM calculated MAF value, DTC P0101 will set.

Throttle Position (TP) Sensor




The throttle position (TP) sensor is a potentiometer used to indicate the amount of throttle opening. The PCM supplies the TP sensor with a 5 volt reference and a ground. The TP sensor provides a signal voltage to the PCM relative to throttle blade angle. By monitoring the voltage on the signal line, the PCM calculates throttle position. As the throttle valve changes (accelerator pedal moves), the TP sensor output voltage will change. With the throttle closed, the signal voltage is low (below 1 volt). However, the TP sensor voltage increases as the throttle valve opens. At Wide Open Throttle (WOT), the TP sensor voltage should be above 4 volts.

The TP signal is one of the most important sensor inputs used by the PCM for controlling fuel and most of the PCM-controlled outputs. A malfunction in the TP sensor or related wiring should set DTC P0122 or DTC P0123. An intermittent condition will set DTC P1121 or DTC P1122. If the actual TP sensor signal does not match a PCM calculated TP value, DTC P0121 will set.

Knock Sensor
The PCM uses a knock sensor (KS) to detect abnormal vibration in the engine (detonation/spark knocking). Mounted in the engine block, under the intake manifold, the knock sensor produces an AC signal at all engine speeds and loads. The PCM then adjusts the spark timing based on the amplitude and frequency of the KS signal.

A knock sensor module is no longer used to diagnose the knock sensor system. The circuitry is integrated into the PCM. The PCM uses the knock sensor signal to calculate an average voltage. Then, the PCM assigns a voltage range above and below the average voltage value. The PCM checks the knock sensor and related wiring by comparing the actual knock signal to the assigned voltage range. A normal knock sensor signal should vary outside the assigned voltage range.

If the PCM malfunctions in a manner that will not allow proper diagnosis of the knock sensor and related wiring, DTC P0325 will set. If the PCM detects a knock signal input within the assigned voltage range, DTC P0327 will set. Refer to Knock Sensor (KS) System for a complete description of the knock sensor system.

Torque Converter Clutch (TCC)/Extended Travel Brake Switches
The PCM uses the input from the torque converter clutch (TCC) and extended travel brake switches to determine the state of the brake pedal (applied or released). The PCM uses the TCC switch input to mainly control the transaxle torque converter clutch (TCC). The PCM sends the extended travel brake switch input, via Class 2, to the EBTCM for braking and traction control management. The switches receive power through a fused ignition feed (hot in RUN and START). With the ignition in the RUN or CRANK position, and the brakes not applied, the PCM should detect ignition voltage. With the brakes applied, the PCM should detect zero volts.

The cruise control module also uses the input from the TCC brake switch. The cruise control system will disengage cruise operation when the TCC brake switch input indicates that the brakes are applied.

Powertrain Control Module Controlled Air Conditioning
I skipped this section

Knock Sensor (KS) System
Purpose
Varying octane levels in todays gasoline may cause detonation in some engines. Detonation is caused by an uncontrolled explosion (burn) in the combustion chamber. This uncontrolled explosion could produce a flame front opposite that of the normal flame front produced by the spark plug. The rattling sound normally associated with detonation is the result of two or more opposing pressures (flame fronts) colliding within the combustion chamber. Though light detonation is sometimes considered normal, heavy detonation could result in engine damage. To control spark knock, a knock sensor (KS) system is used. This system is designed to retard spark timing when spark knock is detected in the engine. The KS system allows the engine to use maximum spark advance for optimal driveability and fuel economy.

Operation
The PCM uses a knock sensor (KS) to detect abnormal vibration in the engine (detonation/spark knocking). Mounted in the engine block, under the intake manifold, the knock sensor produces an AC signal at all engine speeds and loads. The PCM then adjusts the spark timing based on the amplitude and frequency of the KS signal.

A knock sensor module is no longer used to diagnose the knock sensor system. The circuitry is integrated into the PCM. The PCM uses the knock sensor signal to calculate an average voltage. Then, the PCM assigns a voltage range above and below the average voltage value. The PCM checks the knock sensor and related wiring by comparing the actual knock signal to the assigned voltage range. A normal knock sensor signal should vary outside the assigned voltage range (as shown in the normal knock sensor figure). If PCM detects a signal voltage within the assigned voltage range, DTC P0327 will set (as shown in the abnormal knock sensor figure).





(1) Upper Fail Region
(2) Knock Sensor Calculated Average
(3) Knock Sensor Signal (Normal)
(4) Lower Fail Region




(1) Upper Fail Region
(2) Knock Sensor Calculated Average
(3) Knock Sensor Signal (Failed)
(4) Lower Fail Region

Diagnosis
If the PCM malfunctions in a manner which will not allow proper diagnosis of the KS circuits, DTC P0325 will set.

DTC P0327 is designed to diagnose the knock sensors, and related wiring. Problems encountered with the KS system should set a DTC. However, refer to Detonation/Spark Knock in Symptoms if no DTC sets, and the customers complaint of detonation points to the KS system.

Electric Cooling Fan
The electric cooling fans cool the engine coolant flowing through the radiator. The electric cooling fans also cool the refrigerant (R134a) flowing through the A/C condenser.

The engine cooling fan system consists of two electric cooling fans and three fan relays that are controlled by the PCM. The cooling fans receive power from two separate 30A maxifuses located in the Underhood Fuse Block Assembly. The relays are wired in a series/parallel arrangement that allows the PCM to operate both fans together at low or high speed.

During low speed operation, the PCM supplies the ground path for the low speed fans relay through the low speed fans control circuit. This energizes the relay coil, closes the relay contacts, and supplies current to the engine cooling fans. The ground path for the right engine cooling fan is through the series/parallel cooling fan relay and the left engine cooling fan. The result is a series circuit with both fans running at low speed.

To command high speed cooling fan operation the PCM first supplies the ground path for the low speed cooling fans relay through the low speed fans control circuit. After a 3 second delay, the PCM supplies the ground path for the high speed cooling fan relay and the series/parallel cooling fan relay through the high speed fans control circuit. During high speed operation, both engine cooling fans are supplied current through their respective maxifuse and each fan has its own ground path.

PCM will command fan operation under the following conditions:

Low Speed Fan Operation
The engine coolant temperature exceeds approximately 106°C (229°F).
The transmission fluid temperature exceeds 150°C (302°F).
The A/C operation is requested.
After the vehicle is shut OFF if the coolant temperature at key-off is more than 151°C (304°F) and system voltage was more than 12 volts. The fans will stay ON for approximately 3 minutes.
The fans will switch from low to OFF when the coolant drops below 102°C (216°F).

High Speed Fan Operation
The engine coolant temperature reaches 112°C (234°F).
The transmission temperature is more than 151°C (304°F).
When certain DTCs set
The fans will switch from high to low, except when DTCs set, when the coolant drops below 106°C (229°F).


Electronic Ignition (EI) System
Ignition System Overview
The electronic ignition system controls fuel combustion by providing a spark to ignite the compressed air/fuel mixture at the correct time. To provide optimum engine performance, fuel economy, and control of exhaust emissions, the PCM controls the ignition system. The electronic ignition system has the following advantages over a mechanical distributor system:

No moving parts
Less maintenance
Remote mounting capability
No mechanical load on the engine
More coil cool down time between firing events
Elimination of mechanical timing adjustments
Increased available ignition coil saturation time
Operation
The electronic ignition system does not use the conventional distributor and coil. The ignition system consists of the following components/circuits:

Eight ignition coils
Eight ignition control (IC) circuits
Two ignition control modules (one per cylinder bank)
Camshaft position (CMP) sensor
Crankshaft position (CKP) sensor A
Crankshaft position (CKP) sensor B
Related connecting wires
Powertrain control module (PCM)
Crankshaft Position Sensors
The PCM uses dual crankshaft position (CKP A and CKP B) sensors to determine crankshaft position. The CKP sensors are mounted in the engine block approximately 21.5 degrees apart from each other. Three wires connect each CKP sensor to the PCM. The PCM supplies an ignition voltage and a ground for each CKP sensor. During engine rotation, a slotted ring, machined into the crankshaft, causes the sensors to return a series of ON and OFF pulses to the PCM. The PCM uses these pulses to decode the position of the engine crankshaft.

The PCM uses two basic methods of decoding the engine position: Angle Based and Time Based (using either CKP A or CKP B sensor input). During normal operation, the PCM uses the angle based method. In order to operate in this mode, the PCM must receive signal pulses from both CKP sensors. The PCM uses the signal pulses to determine an initial crankshaft position, and to generate MEDRES (24X reference) and LORES (4X reference) signals. Once the initial crank position is determined, the PCM continuously monitors both sensors for valid signal inputs. As long as both signal inputs remain, the PCM will continue to use the angle based mode.

When either CKP signal is lost, the PCM will compare the MEDRES signal to the camshaft position (CMP) sensor signal. If the PCM detects a valid CMP signal, and the MEDRES to CMP signal correlation is correct, the PCM determines that CKP sensor A is at fault. However, if the MEDRES to CMP correlation is incorrect, the PCM determines that CKP sensor B is at fault.

If the PCM detects a loss of signal for CKP sensor A, DTC P0335 will set. The PCM will switch from angle based mode to Time Based mode B using CKP sensor B signal input. If the PCM detects a loss of signal for CKP sensor B, DTC P0385 will set. The PCM will switch from angle based mode to Time Based mode A using CKP sensor B signal input. A noisy signal input from either CKP sensor will cause the ignition system to re-sync. If the number of ignition system re-sync is more than a calibrated amount, DTC P1372 will set.

Camshaft Position Sensor
The camshaft position (CMP) sensor is mounted in the front of the right cylinder head assembly. The CMP sensor signal, when combined with the CKP sensor signal, enables the PCM to determine exactly which cylinder is on a firing stroke. The PCM can then properly synchronize the ignition system, fuel injectors and knock control. The PCM supplies an ignition voltage and a ground for the CMP sensor. If a problem is detected with the CMP circuit, DTC P0340 or P0341 will set.

Ignition Coils/Modules
The electronic ignition system uses an individual ignition coil for each cylinder. There are two separate ignition module assemblies located in the camshaft cover of each cylinder bank. Each ignition module assembly contains an ignition control module and four ignition coils. Each ignition coil connects directly to a spark plug using a boot. This arrangement eliminates the need for secondary ignition wires. The ignition module assemblies receive power from a fused ignition feed. Both ignition module assemblies connect to chassis ground. A Reference Low and four ignition control (IC) circuits connect each ignition module assembly to the PCM. The PCM uses the individual IC circuits to control coil sequencing and spark timing for each ignition coil. The IC circuits transmit timing pulses from the PCM to the ignition control module to trigger the ignition coil and fire the spark plug. The PCM controls ignition system sequencing and timing events.

This ignition system produces very high energy to fire the spark plug. There is no energy loss because of ignition wire resistance, or the resistance of the waste spark system. Also, since the firing is sequential, each coil has seven ignition events to saturate as opposed to the three in a waste spark arrangement.

Noteworthy Ignition Information
There are important considerations to point out when servicing the ignition system. The following noteworthy information will list some of these, to help the technician in servicing the ignition system.

The ignition coils secondary voltage output capabilities are very high - more than 40,000 volts. Avoid body contact with ignition high voltage secondary components when the engine is running, or personal injury may result!
The crankshaft position sensor clearance is very important! The sensor must not contact the reluctor wheel at any time, or sensor damage will result. If the reluctor wheel contacts the sensors, destruction of the sensors will occur.
Ignition timing is not adjustable. There are no timing marks on the crankshaft pulley.
If a boot remains attached to a coil or spark plug, twist the boot prior to removal using the correct tool. Do not use pliers, screwdrivers, or any unauthorized tools to remove the boot.
Check the boot for a missing or damaged internal spring.
Do not re-install any component that has visible signs of damage.
Install the boots onto the coils (until bottomed out). Then install the assembly onto the spark plugs. If this is not possible due to space limitations, just-start the boots onto the spark plugs and then install the coil assembly as straight down onto the plugs as possible.
Ensure the boots are installed right side up.
Repair a torn perimeter seal with RTV sealant.
Adhere to the torque specifications when installing the cassette to the cam cover and the module to the cassette.
Powertrain Control Module (PCM)
The PCM is responsible for maintaining proper spark and fuel injection timing for all driving conditions. To provide optimum driveability and emissions, the PCM monitors input signals from the following components in calculating ignition control (IC) spark timing:

Engine coolant temperature (ECT) sensor
Intake air temperature (IAT) sensor
Mass air flow (MAF) sensor
Trans range inputs from transaxle range switch
Throttle position (TP) sensor
Vehicle speed sensor (VSS)
Reference Low Circuits
The reference low circuits provide a common ground between the PCM, and the ignition control modules. These circuits reduce the electrical ground shifts that may occur between the PCM and the ignition control modules. A malfunction in the reference low circuits may cause a poor driveability condition.

Results of Incorrect Operation
An Ignition control circuit that is open, grounded, or short to voltage will set an ignition control circuit DTC. If a fault occurs in the IC output circuit when the engine is running, the engine will experience a misfire. DTCs P0351-P0358 indicate that a malfunction has been detected on an Ignition Control circuit. DTCs P1359 and P1360 will set when the PCM detects random malfunctions in ignition control circuit.

Air Induction System SKIPPED


Fuel System Description
System Operation
The function of the fuel and air control system is to manage fuel and air delivery to each cylinder to optimize the performance and driveability of the engine under all driving conditions. The fuel supply is stored in a high density polyethylene (HDPE) fuel tank located in front of the rear wheels. The fuel sender allows retrieval of fuel from the tank and also provides information on fuel level. A fuel pump contained in the modular fuel sender pumps fuel through nylon pipes and an in-line fuel filter to the fuel rail. The pump is designed to provide fuel at a pressure above the regulated pressure needed by the injectors. Fuel is then distributed through the fuel rail to eight injectors inside the intake manifold. Fuel pressure is controlled by a pressure regulator mounted on the fuel rail. The fuel system in this vehicle is recirculating, this means that excess fuel that is not injected into the cylinders is sent back to the fuel tank by a separate nylon pipe. This removes air and vapors from the fuel as well as keeping the fuel cool during hot weather operation. Each fuel injector is located directly above each cylinder's two intake valves. An accelerator pedal in the passenger compartment is linked to a throttle valve in the throttle body by a cable. The throttle body regulates air flow from the air cleaner into the intake manifold, which then distributes this air to each cylinder's two intake valves. This allows the driver to control the air flow into the engine, which then controls the power output of the engine.

Engine Fueling
Unleaded fuel must be used with all gasoline engines for proper emission control system operation. Using unleaded fuel will also minimize spark plug fouling and extend engine oil life. Leaded fuel can damage the emission control system, and its use can result in loss of emission warranty coverage.

All vehicles with gasoline engines are equipped with an evaporative emission control (EVAP) System that minimizes the escape of fuel vapors to the atmosphere. Information on this system is found in Driveability and Emissions (Powertrain and Emissions System).

The Northstar engine is fueled by eight individual injectors, one for each cylinder, that are controlled by the PCM. The PCM controls each injector by energizing the injector coil for a brief period generally once every other engine revolution. The length of this brief period, or pulse, is carefully calculated by the PCM to deliver the correct amount of fuel for proper driveability and emissions control. The length of time the injector is energized is called the pulse width and is measured in milliseconds (thousandths of a second).

While the engine is running, the PCM is constantly monitoring its inputs and recalculating the appropriate pulse width for each injector. The pulse width calculation is based on the injector flow rate (mass of fuel the energized injector will pass per unit of time), the desired air/fuel ratio, and actual air mass in each cylinder and it is adjusted for battery voltage, short term and long term fuel trim. The calculated pulse is timed to occur as each cylinders intake valves are closing to attain largest duration and most vaporization.

Fueling during crank is slightly different than during engine run. As the engine begins to turn, a prime pulse may be injected to speed starting. As soon as the PCM can determine where in the firing order the engine is, it begins pulsing injectors. The pulse width during crank is based on coolant temperature and barometric pressure.

The Northstar fueling system has several automatic adjustments to compensate for differences in fuel system hardware, driving conditions, fuel used, and vehicle aging. The basis for fuel control is the pulse width calculation described above. Included in this calculation are an adjustment for battery voltage, short term fuel trim, and long term fuel trim. The battery voltage adjustment is necessary since changes in voltage across the injector affect injector flow rate. Short term and long term fuel trims are fine and gross adjustments to pulse width designed to maximize driveability and emissions control. These fuel trims are based on feedback from oxygen sensors in the exhaust stream and are only used when the fuel control system is in closed loop.

Under certain stringent conditions, the fueling system will not energize injectors, individually or in groups, for a period of time. This is referred to as Fuel shut-off. Fuel shut-off is used to improve traction, save fuel, improve starting, and protect the vehicle under certain extreme or abusive conditions.

In case of a major internal problem, the PCM is equipped with a back-up fueling system that will run the engine until service can be performed.

Notice: Do not operate the engine in the back-up fuel for extended periods. Back-up fueling will negatively impact driveability and fuel economy, and may cause damage to the emissions system.

As part of the fueling system, the PCM records and sends data about fueling to the IPC from which the IPC calculates fuel economy, range, and fuel used displays. The PCM calculates the amount of fuel delivered to the engine through the injectors based on injector pulse width and flow rate. This data is accumulated and sent to the IPC periodically via the data link.

The PCM controls the fuel injectors based on information it receives from several information sensors. Each injector is fired individually in engine firing order, which is called Sequential Multiport Fuel Injection. This allows precise fuel metering to each cylinder and improves driveability under all driving conditions.

Fuel Quality
Due to increasing awareness towards vehicle emissions, evaporative and exhaust, and their impact on the environment, federal regulations are limiting certain characteristics of fuel. These limitations are causing driveability problems that are extremely difficult to diagnose. In order to make a diagnosis, a basic understanding of fuel and its effects on the vehicles fuel system must be gained.

Octane
Octane is a measure of a fuel's ability to resist spark knock. Spark knock occurs in the combustion chamber just after the spark plug fires, when the air/fuel mixture in the cylinder does not completely burn. The remaining mixture spontaneously combusts due to temperature and pressure. This secondary explosion causes a vibration that is heard as a knock (ping). Fuel with a high octane number has a greater resistance to spark knock. This vehicle requires 91 octane ([R+M]/2 method) in order to ensure proper performance of the fuel control system. Using fuel with an octane rating lower than 91 can create spark knock, which would cause the PCM to retard ignition timing to eliminate the knock. In a case such as this, poor engine performance and reduced fuel economy could result. Also, in severe knock cases, engine damage may occur.

Volatility
Volatility is a fuel's ability to change from a liquid state to a vapor state. Since liquid gasoline will not burn, it must vaporize before entering the combustion chamber. The rate at which gasoline vaporizes determines the amount of evaporative emissions released from the fuel system, and therefore has made volatility an environmental concern. The federal government has lowered the maximum allowable volatility, but certain driveability conditions have resulted.

Volatility can be determined through three different tests: the Vapor-Liquid Ratio, the Distillation Curve, and the Reid Vapor Pressure Test (RVP). The Vapor-Liquid Ratio test determines what temperatures must exist to create a vapor-liquid ratio of 20. The distillation curve is a graph showing the relationship between temperature and the percentage of fuel evaporated. The fuel components that boil at relatively low temperatures (below about 90°F) are known as light ends, and those that boil at about 300°F are known as heavy ends. The light ends are important for cold starting and cold weather driveability. Heavy ends provide engine power and are important for hot weather driveability. It is the proper mixture of these components that provide proper operation across a wide range of temperatures. However, the distillation curve of a gasoline usually requires laboratory testing. The Reid Vapor Pressure (RVP) test measures the pressure (psi) vaporized fuel exerts within a sealed container when heated to 100°F. Volatility increases proportional to RVP. While RVP can easily be measured in the field, it may be misleading because it is possible for two fuels with the same RVP to have different distillation curves, and therefore, different driveability characteristics.

As stated, improper volatility can create several driveability problems. Low volatility can cause poor cold starts, slow warm ups, and poor overall cold weather performance. It may also cause deposits in the crankcase, combustion chambers, and spark plugs. Volatility that is too high could cause high evaporative emissions and purge canister overload, vapor lock, and hot weather driveability conditions. Since volatility is dependent on temperature, different fuels are used during certain seasons of the year, thus creating problems during sudden temperature changes.

Fuel System Deposits
Fuel system deposits can cause various driveability problems. Deposits usually occur during hot soaks after key Off. Poor fuel quality or driving patterns such as short trips followed by long cool down periods can cause injector deposits. This occurs when the fuel remaining in the injector tip evaporates and leaves deposits. Leaking injectors can increase injector deposits. Deposits on fuel injectors affect their spray pattern, which in turn could cause reduced power, unstable idle, hard starts, and poor fuel economy.

Intake valve deposits can also be related to fuel quality. While most fuels contain deposit inhibitors, some do not, and the effectiveness of deposit inhibitors varies by manufacturer. If intake valve deposits occur, fuel may be suspected. These deposits can cause symptoms such as excessive exhaust emissions, power loss, and poor fuel economy.

Sulfur Content
The sulfur content in fuel is also regulated to a certain standard. Premium grades of fuel generally have a lower sulfur content than the less expensive blends. A high sulfur content can promote the formation of acidic compounds that could deteriorate engine oil and increase engine wear. It could also produce excessive exhaust emissions or a rotten egg smell from the exhaust system.

Oxygenated Fuels and Alcohol Content
Notice: Do not use fuels containing methanol in order to prevent damage and corrosion to the fuel system.

Methanol can corrode metal parts in the fuel system, and can also damage plastic and rubber parts.

Oxygenated fuels contain oxygen in their chemical structure. The advantages that oxygenated fuels offer are improved octane quality, better combustion, and reduced carbon monoxide emissions. To provide cleaner air, all gasolines in the United States are now required to contain additives that will help prevent deposits from forming in the engine and fuel system. Therefore, nothing should be added to the fuel. The most commonly used oxygenated fuels are ethanol (grain alcohol) and MTBE (Methyl Tertiary Butyl Ether).

Fuel Supply Component Description
On-Board Refueling Vapor Recovery System (ORVR)
The on-board refueling vapor recovery system (ORVR) is an on-board vehicle system to recover fuel vapors during the vehicle re-fueling operation. The flow of liquid fuel down to the fuel tank filler neck provides a liquid seal. The purpose of the ORVR is to prevent re-fueling vapor from exiting the fuel tank filler neck.

The ORVR components include:

• Fuel tank

• Fuel tank filler pipe

• EVAP canister

• Vapor lines

• Check valve

• Modular fuel sender--fuel tank pressure sensor located on modular fuel sender cover

• Fuel limiter vent valve (FLVV)

• Pressure vacuum relief valve

• Vapor recirculation line

• Variable orifice valve

The on-board refueling vapor recovery system (ORVR) is an on-board vehicle system designed to recover fuel vapors during the vehicle refueling operation. The flow of liquid fuel down the filler neck provides a liquid seal which prevents vapor from leaving the fuel system by transporting vapor to the EVAP canister for use by the engine. Listed below are the ORVR system components with a brief description of their operation:

• Fuel tank--Contains the modular fuel sender, fuel limiter vent valve, and three rollover valves.

• Fuel filler pipe--The pipe which carries fuel from the fuel nozzle to the fuel tank.

• EVAP canister--The EVAP canister receives refueling vapor from the fuel system, stores the vapor and releases the vapor to the engine upon demand.

• Vapor lines--Transports fuel vapor from the tank assembly to the EVAP canister.

• Check valve--The check valve limits fuel spit-back from the fuel tank during the refueling operation by allowing fuel flow only into the fuel tank. This check valve is located at the bottom of the fuel filler pipe.

• Modular fuel sender assembly--This assembly pumps fuel to the engine from the fuel tank.

• Fill limiter vent valve (FLVV)--This valve acts as a shut-off valve located in the fuel tank and has the following functions:

- Controls the fuel tank fill level by closing the primary vent from the fuel tank.

- Prevents fuel from exiting the fuel tank via the vapor line to the canister.

- Provides fuel-spillage protection in the event of a vehicle rollover by closing the vapor path from the tank to the EVAP canister.

• Pressure/vacuum relief valve--The pressure/vacuum relief valve provides venting of excessive fuel tank pressure and vacuum. The valve is located in the fuel filler neck on a plastic fuel tank.

• Vapor recirculation line--The vapor recirculation line is used to transport vapor from the fuel tank to the top of the fill pipe during the refueling to reduce vapor loading to the enhanced EVAP canister.

• Variable orifice valve--The variable orifice valve regulates the amount of vapor allowed to enter the vapor recirculation line.

Fuel Tank




The fuel storage tank is made of high density polyethylene and is located in front of the rear wheels. It is held in place by two metal straps attached to the under body of the vehicle. The tank shape includes a sump to maintain a constant supply of fuel around the fuel pump strainer during low fuel conditions or aggressive maneuvers. The tank also contains a fuel vapor vent valve with roll-over protection. The vent valve also features a two phase vent calibration which increases fuel vapor flow to the canister when operating temperatures increase the tank pressure beyond an established threshold.

Fuel Tank Filler Pipe




(1) Fuel Tank Filler Pipe
(2) Fuel Tank Filler Pipe Clamp
(3) Fuel Tank

To help prevent refueling with leaded fuel, the fuel filler pipe has a built-in restrictor and deflector. The opening in the restrictor will accept only the smaller unleaded gasoline fuel nozzle which must be fully inserted to bypass the deflector. The filler pipe is attached to the tank by a section of hose and a clamp. The tank is vented during filling by an internal vent tube inside the filler pipe.

Fuel Filler Cap




(1) Fuel Tank Filler Cap
(2) Fuel Tank Filler Pipe
(3) Fuel Filler Door

The Enhanced EVAP fuel tank pipe cap has a tether connected to the fuel filler pipe door.

Notice: If a fuel tank filler pipe cap requires replacement, use only a fuel tank filler pipe cap with the same features. Failure to use the correct fuel tank filler pipe cap can result in a malfunction of the fuel system. A loose or incorrect fuel tank filler pipe cap can set a DTC.

Fuel Tank Vapor Pressure Sensor




The fuel tank pressure sensor is used to detect small leaks in the evaporative emission system. The fuel tank pressure sensor is a three wire strain gauge sensor much like that of the common GM MAP sensor. However, this sensor has very different electrical characteristics due to its pressure differential design. The sensor measures the difference between the air pressure (or vacuum) in the fuel tank and the outside air pressure. The sensor mounts at the top of the fuel tank. A three wire electrical harness connects it to the powertrain control module (PCM). The PCM supplies a five volt reference voltage and ground to the sensor. The sensor will return a voltage between 0.1 and 4.9 volts. When the air pressure in the fuel tank is equal to the outside air pressure, such as when the fuel fill cap is removed, the output voltage of the sensor will be 1.3 to 1.7 volts.

Enhanced Evaporative Emission (EVAP) Service Port




The enhanced EVAP service port is located in the evaporative purge hose located between the purge solenoid and the EVAP canister. The service port is identified by a green colored cap. The port contains a schrader valve and fittings to allow the connection of the J 41413 , evaporative pressure/purge diagnostic system.

Modular Fuel Sender - Fuel Level Sensor
The modular fuel sender assembly mounts to the threaded opening of the plastic fuel tank with a multi-lipped seal and lock ring. The spring loaded reservoir, containing the exterior inlet strainer, electric fuel pump, and pump strainer, maintains contact with the tank bottom. This design provides:

• Optimum fuel level in the integral fuel reservoir during all fuel tank levels and driving conditions.

• Improved tank fuel level measuring accuracy.

• Improved coarse straining and added pump inlet filtering.

• More extensive internal fuel pump isolation for noiseless operation.

The modular fuel sender assembly consists of the following major components:

• A fuel sender cover assembly

• A fuel sender

• Fuel pipes--above cover

• A fuel sender support assembly

• A fuel pump

• A fuel pump strainer

• A fuel pump reservoir

• A fuel sender strainer

• A fuel level sensor assembly

Modular Fuel Sender - Fuel Flow




(1) Fuel Feed
(2) Fuel Return
(3) Convoluted Fuel Tube (Flex Pipe)
(4) Secondary Umbrella Valve
(5) External Fuel Pump Strainer
(6) Fuel Flow from External Strainer
(7) Fuel Pump Strainer
(8) Fuel Pump

The modular fuel sender assembly maintains optimum fuel level in the reservoir (bucket). Fuel entering the reservoir (bucket) is drawn in by:

• The first stage of the fuel pump through the external strainer. And/Or

• The secondary umbrella valve, Or

• The return fuel pipe, whenever the level of fuel is below the top of the reservoir.

The fuel pump used in this system is part of the fuel sender assembly. The fuel pump lower connector assembly prevents the transmission of vibration and noise generated by the pump to the fuel tank.

Fuel enters the lower inlet port (secondary umbrella valve located inside of lower inlet port) of the electric fuel pump after being filtered by the external fuel strainer, and the fuel pump strainer. The initial function of the pump is to fill the reservoir.

The second stage separates vapor from the fuel in the pump. This vapor separation maximizes hot fuel handling and permits the vapor to return to the fuel tank at lower pressure and temperature. By creating positive fuel pressure, the pump then discharges the liquid fuel into the third stage of the pump. The pump outlet allows the fuel volume to flow through a check valve into the fuel pump flex pipe. The check valve seat is molded inside the connector body. The check valve body and retainer are assembled into the connector body. The check valve restricts fuel back flow.

After the fuel pump flex pipe, the fuel exits the assembly through the fuel feed output fitting on the molded cover. The cover also contains a fuel return provision which connects to one of three hollow support pipes.

Modular Fuel Sender Assembly




(1) Fuel Tank Pressure Sensor
(2) Fuel Pipes
(3) Fuel Pump
(4) External Fuel Sender Strainer
(5) Fuel Level Sensor Assembly
(6) Fuel Sender Cover

These quick-connect end fittings allow fuel feed and fuel return. Electrical power to the fuel pump enters the unit by way of a connector which is attached to the cover. An internal wire harness and connector assembly connects to the fuel pump and level sensor. The modular design adds additional functions that improve accuracy and ensure constant, steady fuel supply under all conditions. All components and subassemblies of the modular sender attach to a common cover and access the fuel tank through a single opening. The modular fuel sender assembly is spring loaded to the bottom of the fuel tank. This bottom referencing permits continuous fuel pickup and accurate fuel level sensing. The reservoir assembly is the lower section of the modular unit which encases the fuel pump. A retainer attaches to the top of the reservoir. Fuel is captured and maintained in reservoir at a level sufficient to submerge pump.

A rubber bumper (pad) is assembled between the bottom of the reservoir and the fuel sender strainer. This promotes noise isolation by acting as a buffer between the reservoir bottom and the fuel tank, and provides a fastening mechanism for the fuel level sensor assembly to the reservoir.

Two quick-connect pipe end fittings are molded onto the cover of the modular unit for ease of unit removal from the fuel tank. These quick-connect end fittings allow fuel feed and fuel return.

The tank also contains a fuel vapor vent valve with roll-over protection. The vent valve also features a two phase vent calibration which increases fuel vapor flow to the canister when operating temperatures increase the tank pressure beyond an established threshold.

Modular Fuel Sender Serviceable Components
The serviceable components on the modular fuel sender are the fuel sender strainer, and the fuel level sensor assembly.

The strainer acts as a coarse filter to filter contaminants, separate water from fuel, and to provide a wicking action that helps draw fuel into the fuel pump.

Fuel stoppage at the strainer indicates that the fuel tank contains an abnormal amount of sediment or water. Therefore, the fuel tank should be removed, cleaned, and the filter strainer replaced. Refer to Fuel System Cleaning .

Fuel Level Sender Assembly




The fuel sender assembly consists of the float, the wire float arm, and the ceramic resistor card. The fuel level sensor is mounted on the modular fuel sender assembly and located in series with the voltage supply circuit from the PCM. As the position of the float varies with the fuel level, the ceramic resistor card produces variable resistance between the PCM and ground. The PCM uses the variable resistance to calculate the expected vapor pressures within the fuel system. The vapor pressure is critical in determining if the evaporative emission system is operating properly. The PCM also uses the variable resistance to indicate actual fuel level for the fuel level gauge. The fuel level gauge is controlled by the IP cluster. The IP cluster receives fuel level information from the PCM through the Class 2 communication circuit.

In-Line Fuel Filter (Typical)




(1) Fuel Filter Housing
(2) Fuel Filter Element

A in-line filter is used in the fuel feed pipe ahead of the fuel injection system. The filter element is made of paper, and is designed to trap particles in the fuel that may damage the injection system. A plastic quick-connect type fitting is used at the inlet of the filter and a threaded fitting is used on the engine side of the filter.

Fuel Feed, Return, and EVAP Pipes - Engine Compartment
The fuel feed pipe delivers the fuel from the fuel tank to the fuel rail assembly. The fuel feed pipe carries excess fuel from the outlet port of the fuel rail back to the fuel tank. The canister purge pipe transfers fuel vapors to the charcoal canister.

Fuel Feed, Return, EVAP Pipes, and Canister - Chassis




(1) Fuel Tank Vapor Hose To EVAP Canister
(2) Vent Hose To EVAP Canister
(3) Purge Hose To EVAP Canister
(4) In-line Fuel Filter
(5) Fuel Feed Pipe
(6) Fuel Return Pipe
(7) Retainer

The fuel feed, return, vacuum and EVAP pipes are assembled as a harness. Retaining clips hold the pipes together and provide a means for attaching the pipes to the vehicle. Quick-connect type fittings are used at the ends of the fuel feed and return and at the in-line fuel filter. They are described below. Sections of the pipes that are exposed to chafing, high temperature, or vibration are protected with heat resistant rubber hose and/or coextruded conduit.


Nylon Fuel Pipes
Nylon fuel pipes are designed to perform the same function as the steel or rubber fuel pipes they replace. Nylon pipes are constructed to withstand maximum fuel system pressure, exposure to fuel additives, and changes in temperature. Nylon fuel pipes are somewhat flexible and can be formed around gradual turns under the vehicle. However, if forced into sharp bends, nylon pipes will kink and restrict fuel flow. Also, once exposed to fuel, nylon pipes may become stiffer and more likely to kink if bent too far. Special care should be taken when working on a vehicle with nylon fuel pipes.

Caution: In order to Reduce the Risk of Fire and Personal Injury:

• If nylon fuel pipes are nicked, scratched or damaged during installation, Do Not attempt to repair the sections of the nylon fuel pipes. Replace them.

• When installing new fuel pipes, Do Not hammer directly on the fuel harness body clips as it may damage the nylon pipes resulting in a possible fuel leak.

• Always cover nylon vapor pipes with a wet towel before using a torch near them. Also, never expose the vehicle to temperatures higher than 115°C (239°F) for more than one hour, or more than 90°C (194°F) for any extended period.

• Before connecting fuel pipe fittings, always apply a few drops of clean engine oil to the male pipe ends. This will ensure proper reconnection and prevent a possible fuel leak. (During normal operation, the O-rings located in the female connector will swell and may prevent proper reconnection if not lubricated.)


Quick-Connect Fittings




Quick-connect type fittings provide a simplified means of installing and connecting fuel system components. There are two types of quick-connect fittings, each used at different locations in the fuel system. Each type consists of a unique female socket and a compatible male connector. O-rings, located inside the female socket, provide the fuel seal. Integral locking tabs or fingers hold the fittings together. The quick-connect fittings used at the fuel filter and other connections at the rear of the vehicle have hand releasable locking tabs. The fittings used at the engine fuel pipes have locking tabs that require a special tool to release.
Fuel Metering Modes of Operation
The PCM has several operating modes for fuel control, depending on the information it receives from the sensors.

Starting Mode
When the key is first turned On, the PCM will turn on the fuel pump relay for two seconds. The fuel pump runs and builds up pressure in the fuel system. The PCM then monitors the MAF, IAT, ECT, TP sensors and ignition control (IC) module signal to determine the required injector pulse width for starting.

Clear Flood Mode
If the engine is flooded with fuel during starting and will not start, Clear Flood Mode can be manually selected. To select Clear Flood Mode, push the accelerator to wide open throttle (WOT). With this signal, the PCM will completely turn Off the injectors and will maintain this as long as it sees a WOT condition with engine speed below 1000 RPM.

Run Mode
The run mode has two conditions: Open Loop and Closed Loop. When the engine is first started and engine speed is above 400 RPM, the system goes into Open Loop operation. In Open Loop, the PCM ignores the signals from the oxygen sensors and calculates the required injector pulse width based primarily on inputs from the MAF, IAT and ECT sensors. The system will stay in Open Loop until the following conditions are met:

One oxygen sensor has varying voltage output, showing that it is hot enough to operate properly.
The ECT sensor indicates above 80°C.
A calibrated time delay has elapsed after starting the engine. This delay allows all sensors to stabilize.
When these conditions are satisfied, the PCM goes into Closed Loop operation. In Closed Loop, the PCM adjusts the calculated injector pulse width for each bank of injectors based on the signals from each oxygen sensor.

Acceleration Mode
The PCM monitors changes in TP and MAF sensor signals to determine when the vehicle is being accelerated. The PCM will then increase injector pulse width to provide more fuel for improved driveability.

Deceleration Mode
The PCM monitors changes in TP and MAF sensor signals to determine when the vehicle is being decelerated. The PCM will then decrease injector pulse width or even shut Off injectors for short periods to reduce exhaust emissions.

Battery Voltage Correction Mode
When the PCM sees a low battery voltage condition, it can compensate to maintain acceptable vehicle driveability. It does this by:

Increasing the injector pulse width to maintain the proper amount of fuel delivered.
Increasing the idle speed to increase generator output.
Load Management Control Mode
When the HVAC controller has a request for rear window defog at idle, the HVAC controller sends a message via UART serial data to the PCM to increase the desired idle speed. The changes to desired idle speed are as follows. At idle in park/neutral desired idle speed will be at least 1040 RPM. When a gear other than park or neutral is selected, the desired idle speed will be at least 704 RPM.

Fuel Shutoff Mode
The PCM has the ability to completely turn all the injectors Off or selectively turn Off some of the injectors when certain conditions are met. These fuel shut-off modes allow the powertrain to protect itself from damage and also improve its driveability.

The PCM will disable all eight injectors under the following conditions:

Ignition Off--Prevents engine run-on
Ignition On but no ignition reference signal--Prevents flooding or backfiring
High engine speed--Above red line
High vehicle speed--Above rated tire speed
Extended high speed closed throttle coastdown--Reduces emissions and increases engine braking
The PCM will selectively disable up to four injectors under the following conditions:

Torque management enabled--Transaxle shifts or abusive maneuvers
Traction control enabled--In conjunction with front brakes applying
Low coolant condition--Protects engine from overheating


Fuel Metering System Component Description
The fuel metering system consists of the following parts:

The fuel supply components (fuel tank, pump, pipes).
The fuel pump electrical circuit.
The fuel rail.
The fuel injectors.
The fuel pressure regulator.
The throttle body.
The idle air control (IAC) valve.
The throttle position (TP) sensor.
System Overview
The fuel tank stores the fuel supply. An electric fuel pump attaches to the fuel sender assembly inside the fuel tank. The fuel pump sends fuel through the fuel feed pipe and an in-line fuel filter to the fuel rail assembly. The pump provides fuel at a pressure greater than is needed by the injectors. The fuel pressure regulator, part of the fuel rail assembly, keeps fuel available to the injectors at a regulated pressure. A separate fuel return pipe returns the unused fuel to the fuel tank.

Fuel Pump Electrical Circuit
The fuel pump relay is located below the rear seat inside the rear electrical center. The fuel pump relay allows the fuel pump to be energized by the PCM. When the ignition is first turned On, the PCM energizes the fuel pump relay for two seconds. This allows the fuel pump to run for two seconds and build up fuel pressure for cranking. The PCM then waits for ignition reference pulses from the ignition coils. Once the PCM sees references pulses, the PCM energizes the relay to run the fuel pump.

Fuel Rail Assembly




The fuel rail consists of five parts:

The pipe that carries fuel to each injector.
The fuel pressure regulator.
The fuel pressure test port.
The fuel rail ground strap.
Eight individual fuel injectors.
The fuel rail is mounted on the intake manifold and distributes fuel to each cylinder through the individual injectors.

Fuel is delivered from the pump through the fuel feed pipe to the inlet port of the fuel rail pipe. From the fuel feed inlet, fuel is directed to the front rail pipe, then a crossover to the rear pipe, then through the rear rail pipe to the fuel pressure regulator. Fuel in excess of injector needs flows back through the pressure regulator assembly to the outlet port of the fuel rail. Fuel then flows through the fuel return pipe to the fuel tank to begin the cycle again.

A eight digit identification number is stamped on the fuel rail assembly. The model identification contains the Julian date, the year, and the shift. Refer to this model identification number if servicing or part replacement is required.

Fuel Injectors
The top-feed fuel injector assembly is a solenoid operated device, controlled by the PCM, that meters pressurized fuel to a single engine cylinder. The PCM energizes the injector solenoid, which opens a ball valve, allowing fuel to flow past the ball valve, and through a recessed flow director plate. The director plate has multiple machined holes that control the fuel flow, generating a conical spray pattern of finely atomized fuel at the injector tip. Fuel is directed at the intake valve, causing it to become further atomized and vaporized before entering the combustion chamber. An injector stuck partly open can cause a loss of pressure after engine shutdown. Consequently, long cranking times would be noticed on some engines.

Fuel Pressure Regulator




(1) Regulator Assembly
(2) Pressure Regulator Spring
(3) O-Ring -- Backup
(4) O-Ring -- Large
(5) Filter Screen
(6) Relief Valve
(7) O-Ring -- Small

The fuel pressure regulator is a diaphragm-operated relief valve with fuel pump pressure on one side, and regulator spring pressure and intake manifold vacuum on the other side. The function of the regulator is to maintain a constant fuel pressure across the director spray plate under all operating conditions. The pressure regulator compensates for engine load by increasing fuel pressure as engine intake manifold vacuum drops. The pressure regulator is mounted on the fuel rail.

The cartridge regulator is serviced as a separate component. When servicing the fuel pressure regulator, insure that the back-up O-ring, large O-ring, filter screen, and small O-ring are properly placed on the pressure regulator.

With the ignition On, and engine Off (zero vacuum), system fuel pressure at the pressure test connection should be 284-325 kPa (41-47 psi). If the pressure regulator supplies fuel pressure which is too low or too high, a driveability condition will result.

Throttle Body Assembly
The throttle body assembly attaches to the intake manifold. The throttle body controls air flow into the engine, thereby controlling engine output. The vehicle operator opens the throttle valve within the throttle body through the accelerator controls. During engine idle, the throttle valves are almost closed. A fixed air bypass orifice and the idle air control (IAC) valve handle the air flow control. The throttle body also provides the location for mounting the throttle position (TP) sensor.

Idle Air Control (IAC) Valve




(1) IAC Valve Assembly
(2) Throttle Blade
(3) Pintle

The purpose of the IAC valve is to control engine idle speed, while preventing stalls due to changes in engine load. The throttle blade when closed allows a small amount of air into the intake manifold. However, most of the air for closed throttle engine operation passes through the IAC valve, bypassing the throttle blade. By moving a conical valve known as a pintle in toward the seat (to decrease air flow), or out away from the seat (to increase air flow), a controlled amount of air can be bypassed. If engine speed is too low, more air is bypassed in order to increase RPM. If engine speed is too high, less air is bypassed in order to decrease RPM. The PCM moves the IAC valve in small steps, called counts. These can be measured and displayed with a scan tool, which plugs into the data link connector (DLC). The PCM calculates the proper position of the IAC valve during idle based upon the battery voltage, the coolant temperature, the engine load, and the engine RPM. If the RPM drops below specification and the throttle valve is closed, the PCM senses a near stall condition and calculates a new valve position in order to prevent stalling.

Engine idle speed is a function of total air flow into the engine. Idle speed is based on IAC valve pintle position, crankcase ventilation valve flow, throttle valve opening, bypass orifice air flow, and calibrated vacuum loss through accessories.
Controlled idle speed is programmed into the PCM, which determines the correct IAC valve pintle position to maintain the desired idle speed for all engine operating conditions and loads.
The minimum idle air rate is set at the factory with a stop screw. This setting allows enough air flow by the throttle valve to cause the IAC valve pintle to be positioned a calibrated number of steps (counts), from the seat, during controlled idle operation.
If the IAC valve is disconnected or disabled with the engine running, the PCM may loose track of the IAC valve position causing erratic or incorrect idle speed. If this occurs, reset the IAC valve by doing the following:

Start and idle the engine foe 15 seconds.
Turn the ignition switch to the LOCK/OFF position.
Wait 15 seconds.
Restart the engine and inspect for proper idle operation.
Throttle Position (TP) Sensor
The TP sensor is a potentiometer that is mounted on the throttle body and provides the PCM with information on throttle valve angle. The PCM provides a 5 volt reference signal and a ground to the TP sensor and the sensor returns a signal voltage that changes with throttle valve angle. At closed throttle (close to 0 degrees) the TP sensor output signal is low (below 1 volt) and at WOT (greater than 80 degrees) the TP sensor output signal is high (above 4 volts). Because the TP sensor is not adjustable, the PCM must account for build tolerances that could affect the TP sensor output at closed throttle. The PCM uses a learning algorithm so that it can correct for variations of up to 6 degrees of throttle angle.

The PCM uses TP information to modify fuel control based on throttle valve angle. For example, power enrichment occurs when the throttle angle approaches WOT. Acceleration enrichment occurs when the throttle angle increases rapidly (similar to an accelerator pump on a carburetor). A faulty TP sensor may cause various driveability conditions and should set a DTC.

Accelerator Controls
The accelerator control system is cable type. There are no linkage adjustments. Therefore, the specific cable for each application must be used. The accelerator cable is routed through the groove in the throttle body lever.





(1) Accelerator Control Cable
(2) Accelerator Pedal Assembly
(3) Accelerator Pedal Retainer


Evaporative Emission Control System
EVAP System Components
The EVAP system contains the following components:

• The EVAP fuel vapor canister

• The EVAP purge solenoid valve

• The EVAP vent valve

• The EVAP fuel tank pressure sensor

• The fuel tank

• The fuel vapor and vent lines

Enhanced EVAP System Operation
The EVAP control system collects the fuel vapors from the fuel tank. When the engine is not running, a canister filled with activated carbon (charcoal) stores the fuel vapors. When the engine is running, the stored fuel vapors are drawn from the canister, then mixed with the intake air flow, and consumed in the normal combustion process.

The PCM uses the EVAP purge valve to control the flow of the fuel vapors from the canister. The PCM supplies the ground to energize the EVAP purge valve (purge ON). The PCM controls the ON and OFF time of the EVAP purge valve by a pulse width modulated (PWM) signal. The PCM determines the EVAP purge valve PWM duty cycle based on certain operating conditions (i.e., mass air flow, engine coolant temperature, manifold absolute pressure, and intake air temperature).

Diagnosis
The PCM tests the EVAP system by applying vacuum to a sealed system, then monitoring the rate of vacuum decay. The PCM determines the vacuum decay using the signal from the fuel tank pressure sensor. The PCM tests the EVAP system for the following conditions:

• Large and small leaks--P0440 and P0442

• Excess vacuum--P0446

• Purge flow during non-commanded conditions--P1441

• Fuel pressure sensor and--P0452, P0453

• Fuel level sensor faults--P0461, P0462 and P0463

• EVAP purge (P0443), and vent valve (P0449) solenoid malfunctions

The PCM tests the EVAP system, when the following conditions are met:

• No TP sensor, MAP sensor, VSS, IAT sensor, ECT sensor, HO2S sensor, fuel trim, fuel level sensor, misfire, fuel Injectors, EGR pintle position, fuel tank pressure sensor, fuel level sensor, or MAF sensor DTCs are set.

• Battery voltage is between 10 and 18 volts.

• Barometric pressure is more than 72 kPa.

• Fuel level is steady between 15 and 85 percent.

At an appropriate time, the PCM turns ON the EVAP purge and EVAP vent valves. This opens the EVAP purge valve and closes the EVAP vent valve. The engine draws a small vacuum on the entire EVAP system. After achieving the desired vacuum level, the PCM turns OFF the EVAP purge valve. The PCM detects a leak by monitoring decrease in the vacuum level over a period of time. A small leak in the system causes DTC P0442 to set. A large leak, EVAP or a malfunctioning purge valve will causes an insufficient vacuum level in the system and will set DTC P0440. A large leak may be the result of the following conditions:

• Disconnected or malfunctioning fuel tank pressure sensor

• Missing or malfunctioning fuel cap

• Disconnected, damaged, pinched, or blocked EVAP purge line

• Disconnected or damaged EVAP vent hose

• Disconnected, damaged, pinched, or blocked fuel tank vapor line

• Disconnected or malfunctioning EVAP purge valve

• Disconnected or malfunctioning EVAP vent valve

• An open ignition feed circuit to the EVAP vent or purge valve

• Damaged EVAP canister

• Leaking fuel sender assembly O-ring

• Leaking fuel tank or fuel filler neck

The PCM also tests the EVAP system for a restricted or blocked vent path. First, the PCM turns ON the EVAP purge and EVAP vent valves. As indicated above, this opens the EVAP purge valve and closes the EVAP vent valve. The engine draws a small vacuum on the entire EVAP system. Then, at the appropriate vacuum level, the PCM turns OFF the EVAP purge and EVAP vent valves. This closes the EVAP purge valve and opens the EVAP vent valve. At this time, the PCM monitors the vacuum decay using the signal from the fuel tank pressure sensor. Unless a blocked vent path is present, the PCM should detect a quick decay of the vacuum. DTC P0446 will set if a blocked vent path is present. DTC P0446 may be the result of the following conditions:

• Malfunctioning EVAP vent valve--stuck closed

• Plugged, kinked, or pinched vent hose

• Shorted EVAP vent valve control circuit

To check for a continuous purge condition, the PCM turns OFF the EVAP purge valve and turns ON the EVAP vent valve. This closes the EVAP purge valve and opens the EVAP vent valve. The PCM again monitors the vacuum level in the EVAP system. With the purge valve closed and the vent valve opened, the PCM should detect no vacuum in the EVAP system unless a continuous purge conditions is present. DTC P1441 will set if the PCM detects a continuous purge condition. Any of the following conditions will set DTC P1441:

• EVAP purge valve leaking

• EVAP purge and engine vacuum source lines switched at the valve

• EVAP purge valve control circuit grounded


Secondary Air Injection System Description
The two AIR pumps used on this vehicle lower tail pipe emissions during start-up. The AIR system consists of the following items:

AIR pumps
Check valves
Vacuum solenoid
System hoses/piping
AIR relays, fuses, and related wiring
The PCM uses the AIR relays to control the AIR pumps. The PCM also controls the AIR vacuum solenoid that supplies vacuum to the AIR check valves. With the AIR system inactive, the AIR check valves prevent air flow in either direction. With the AIR system active, the PCM applies ground to one of the AIR relays, and the vacuum solenoid. After a few seconds, the PCM applies ground to the other AIR relay. Fresh air flows from the pumps, through the system hoses, pass the check valves, and into the exhaust stream. The air helps the catalyst to quickly get to a working temperature; thus lowering the tail pipe emissions on a start-up.

The PCM tests the AIR system for the following conditions:

AIR system (overall system including both banks, and results in DTC P0410)
AIR system bank 1 (DTC P1415)
AIR system bank 2 (DTC P1416)
AIR relays (DTC P0418, and DTC P0419)
AIR vacuum control solenoid (DTC P0412)
The PCM runs two tests to diagnose the AIR system, Passive and Active. Both tests contain two parts, and involve a response from the fuel control HO2 sensors (HO2S bank 1 sensor 1 and HO2S bank 2 sensor 2) as follows:

PASSIVE TEST PART 1
The PCM performs the passive test part 1 during the normal operation of the AIR system (start-up). The PCM initiates this test only once per key cycle. When the PCM enables the AIR System, the PCM freezes the fuel trim system, then checks the voltage from the HO2 sensors. If the PCM detects HO2S voltages below the calibrated value for the calibrated amount of time, the PCM starts part 2 of the passive test.

PASSIVE TEST PART 2
The PCM performs part 2 of the passive test to watch the response of the HO2 sensors with the AIR system turned OFF. With the AIR system turned OFF, the PCM unfreezes the fuel trim system, then watches the HO2S voltages. If the PCM detects HO2S voltages that switch from lean to rich value for a specific amount of time, the PCM passes the AIR system.

ACTIVE TEST PART 1
The PCM performs part 1 of the active test during warmed-up, closed-loop fuel control. When the PCM turns ON the AIR system, the PCM freezes the fuel trim system, then checks the voltage from the HO2 sensors. If the PCM detects HO2S voltages below the calibrated value for the calibrated amount of time, the PCM starts part 2 of the active test.

ACTIVE TEST PART 2
The PCM performs part 2 of the active test to watch the response of the HO2 sensors with the AIR system turned OFF. During warmed-up, closed-loop fuel control, the PCM turns OFF the AIR system. The PCM unfreezes the fuel trim system, then watches the HO2S voltages. If the PCM detects HO2S voltages that switch from lean to rich value for a specific amount of time, the PCM passes the AIR system.

If both passive tests pass, the PCM takes no further action. If either part of the passive test fails, or is inconclusive, the PCM initiates the Active tests. If the PCM determines that the HO2S voltages did not respond as expected during the tests, DTC P0410 will set. If the PCM determines that the HO2S voltage for a specific bank did not respond as expected, DTC P1415 or DTC P1416 will set, depending upon the bank.
Exhaust Gas Recirculation (EGR) System
Purpose
The exhaust gas recirculation (EGR) system is used to lower the emission levels of oxides of nitrogen (NOx) that form during the combustion process. NOx levels are based on the amount of oxygen in the combustion chamber, and the length of time that combustion temperatures exceed 1500°F. The EGR system lowers the combustion temperatures, thus lowering the level of NOx.

Operation




(1) Cap-Sensor
(2) Sensor-EGR Pintle Position
(3) Pole Piece-Primary
(4) Bobbin and Coil Assembly
(5) Sleeve-Armature
(6) Valve-Pintle
(7) Armature and Base Assembly

The EGR valve is designed to supply EGR to the engine. The EGR valve consists of a sealed bobbin and coil assembly (solenoid). Inside the solenoid is a sleeve-armature assembly that contains a pintle and valve, two seals, retaining washers, a seal spring, and armature spring, and a bearing. The bearing seals the pintle valve shaft from the exhaust chamber. Also, a shield, held in place by a compression spring, deflects exhaust gas from the shaft and armature.





(1) Linear EGR Valve
(2) Exhaust Gas
(3) To Cylinders
(4) Pintle

The PCM uses the pintle valve to control the EGR flow into the engine. Exhaust gas is routed from the intermediate exhaust pipe to the valve through a feedpipe. When the PCM commands the EGR valve open, the exhaust flows through the EGR valve, past the pintle and into the engine via the crossover water pump housing. When the throttle valve opens, the exhaust gas mixes with the incoming air. When the combination of air/fuel/exhaust gas is burned in the chamber, a portion of the heat energy is absorbed by the exhaust gas. This helps to lower the level of NOx emissions.

The PCM monitors the pintle position using the signal from the EGR pintle position sensor. The sensor is an integral part of the EGR valve. The PCM supplies the pintle position sensor with a 5 volt reference and a ground. The pintle position sensor provides a signal voltage to the PCM. By monitoring the voltage on the signal line, the PCM is able to determine if the EGR valve responds properly to commands from the PCM. As the EGR valve position changes, the pintle position signal voltage will change. With the EGR valve closed, the signal voltage is near 0 volts. However, the pintle position signal voltage increases as the EGR valve opens.

EGR Diagnosis
Too much EGR flow tends to weaken combustion, causing the engine to run rough and/or stall. With too much EGR flow at idle, cruise, or cold operation, any of the following conditions may occur:

Engine stalls after cold start.
Vehicle surge during cruise operation.
Engine stalls during closed throttle conditions.
Rough idle
DTC P0300 (misfire detected)
If the EGR valve is stuck open, the engine may not run.

Too little or no EGR flow allows combustion temperatures to get too high during acceleration and load conditions. This could cause:

Spark knock (detonation), especially on light acceleration
Engine overheating
Emission test failure
DTC P0401
Poor fuel economy
EGR flow diagnosis is included in DTC P0401 diagnostic table. Pintle position error and control circuit diagnosis is covered in DTCs P0403, P0404, P0405, and P1404. If EGR diagnostic trouble codes are encountered, refer to the appropriate DTC tables for diagnosis.

Crankcase Ventilation System SKIPPED

------------------
Cadillac Tech
ASE MASTER TECH since 1988

86 Northstar Fiero
85 RX7 former SCCA car
56 TR3 small mouth 6.0L
A.J. Whiteley

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AJxtcman

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Late 2003 and 2004 PCM




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Report this Post02-23-2007 08:13 PM Click Here to See the Profile for ryan.hessSend a Private Message to ryan.hessDirect Link to This Post
 
quote
Originally posted by AJxtcman:
This will start as VIN Y & 9 engine controls
I hope the info is in here Ryan.


Any crank position signal information? Crank pulses vs crank angle?
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Report this Post02-23-2007 08:21 PM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post
I have it in another book. It is in a training course. I will look for it now.
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AJxtcman

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I am having problems Ryan

Scan Tool Data Definitions

The Engine Scan Tool Data Definitions contains a brief description of all engine related parameters available on the scan tool. The list is in alphabetical order. A given parameter may appear in any one of the data lists. In some cases, the parameter may appear more than once or in more than one data list in order to group certain related parameters together.

12 Volt Reference
The scan tool displays OK or Fault. This parameter indicates the state of the IGN 1 input to the PCM.

24X Crank sensor (Data)
The scan tool displays RPM. This parameter displays engine speed based on the correlation of CKP sensor A and B signals.

5 Volt Reference A
The scan tool displays OK or Fault. This parameter indicates the state of the 5 volt reference A circuit. This circuit supplies the reference voltage to the TP sensor , MAP sensor , and EGR pintle position sensor .

5 Volt Reference B
The scan tool display OK or Fault. This parameter indicates the state of the 5 volt reference B circuit. This circuit supplies the reference voltage to the A/C pressure sensor , and the fuel tank pressure sensor .

A/C High Side Pressure
The scan tool range is 0.00-5.00 volts. This parameter indicates the A/C high side pressure sensor input to the PCM.

A/C Relay
The scan tool displays ON or OFF. This parameter indicates the PCM commanded state of the A/C Relay Control circuit.

Actual EGR Position
The scan tool range is 0-100 percent . Represents the actual position of the EGR pintle in percent. Zero percent displayed indicates a fully extended pintle (EGR valve closed).

Air Fuel Ratio
The scan tool displays the PCM commanded air to fuel. Air fuel ratio should normally be around 14.2:1 - 14.7:1. A lower air fuel ratio indicates a richer air to fuel mixture. A higher air fuel ratio indicates a leaner commanded air to fuel mixture.

AIR Pump Relay
The scan tool displays ON or OFF.

This parameter indicates the PCM commanded state of the AIR pump relay(s).

AIR Solenoid
The scan tool displays ON or OFF.

This parameter indicates the PCM commanded state of the AIR vacuum solenoid.

Auto Learn Timer
The scan tool indicates ACTIVE or INACTIVE. This parameter indicates the status of the vehicle theft deterrent system password learn.

BARO
The scan tool range is 10-105 kPa / 0.00-5.00 volts. The barometric pressure reading is determined from the MAP sensor signal. The PCM monitors the MAP signal during key up and wide-open throttle (WOT) conditions. The barometric pressure compensates for altitude differences.

CKP sensor Status
The scan tool displays Angle, Time A, or Time B. This parameter indicates the engine position sensing mode. With both CKP sensors A and B working properly, this parameter should display Angle. If the PCM detects an incorrect condition with CKP sensor A, the PCM will command TIME B mode. If the PCM detects an incorrect condition with CKP sensor B, the PCM will command Time A mode.

CMP sensor (Data)
The scan tool displays 0-16384 RPM. This parameter indicates engine speed as calculated from the CMP sensor signal.

Crank Request
The scan tool displays Yes or No. Yes is displayed when the key is in the Crank position.

Cruise Inhibited Signal Command
The scan tool displays Yes or No. Yes displayed indicates that the PCM is commanding the SMCC module to inhibit cruise control operation. Should display Yes with park, neutral, reverse or low gear selected.

Cruise Requested
The scan tool displays YES or NO. With cruise control engaged, this parameter indicates YES.

Current Gear
The scan tool displays the numbers 1, 2, 3, or 4. The PCM looks at trans range position and the gear commanded by the PCM. The actual forward gear that the transaxle is in will be the lower of the two because the manual valve can override the PCM commanded gear. The scan tool displays which gear the transmission is in.

Cycles Of Misfire Data
The scan tool displays 0-100. This parameter indicates which cycle of the 100 engine cycles that the PCM collects misfire data.

Desired EGR Position
The scan tool range is 0-100 percent . The parameter indicates the PCM commanded EGR pintle position. The desired EGR position should stay close to actual EGR position.

Desired Idle Speed
The scan tool range is 0-3187 RPM. The PCM commands the desired idle speed. The PCM compensates for various engine loads based on engine coolant temperature in order to keep the engine at the desired speed.

Desired Torque ABS/TCS
The scan tool displays 0-100 percent . This parameter indicates the desired amount of torque requested by the EBTCM.

ECT
The scan tool range is -40°C to 140°C (-40°F to 284°F). This parameter indicates the engine coolant temperature based on input from the engine coolant temperature sensor .

EGR Closed Pintle Position
The scan tool range is 0-255 counts. This parameter indicates the closed valve position of the EGR in counts.

EGR Flow Test Count
The scan tool range is 0-255 counts. This parameter Indicates the number of EGR flow test samples collected during the current ignition cycle.

EGR Pintle Position
The scan tool range is 0.00-5.00 volts. This parameter Indicates the EGR pintle position sensor signal voltage being monitored by the PCM. A low voltage indicates a fully extended pintle (closed valve). A voltage near 5 volts indicates a fully retracted pintle (open valve).

Engine Load
The scan tool range is 0-100 percent . This parameter indicates the calculated engine load based on engine speed, and MAF sensor readings. The engine load increases with an increase in RPM or airflow.

Engine Oil Level
The scan tool displays OK or Low. The parameter displays Low if the engine oil level remains low (about 1 quart or more) for a sufficient period of time.

Engine Oil Pressure
The scan tool displays OK or Low. This parameter displays whether or not sufficient engine oil pressure is present.

Engine Run Time
The scan tool displays Hours, Minutes, Seconds. This indicates the amount of engine run time. When the ignition is cycled off, the timer will reset to zero.

Engine Speed
The scan tool range is 0 to 16384 RPM. This parameter indicates the engine speed calculated by the PCM. The engine speed should remain close to desired idle under various engine loads with the engine idling.

EVAP Canister Purge
The scan tool range is 0-100 percent . This parameter indicates the PCM commanded duty cycle of the EVAP purge valve. a display of 0 percent indicates no purge while a display of 100 percent indicates full purge.

EVAP Purge Solenoid
The scan tool displays ON or OFF. This parameter indicates the PCM commanded state of the EVAP canister purge valve.

EVAP Test Abort Reason
The scan tool displays Not Aborted, Lost Enable, Small Leak, Veh. Not at Rest. This parameter indicates the reason the EVAP system test was aborted.

EVAP Test Result
The scan tool displays No Result, Aborted, Passed, Failed-DTC P0440, Failed-DTC P0442, Failed-DTC P0446, Failed-DTC P1441. This parameter indicates the results of the EVAP system tests.

EVAP Test State
The scan tool displays Wait For Purge, Test Running, Test Complete. This parameter indicates the state of the EVAP Service Bay test.

EVAP Vent Sol.
The scan tool displays Open or Closed. This parameter indicates the PCM commanded state of the EVAP vent solenoid.

Extended Travel Brake
The scan tool displays Applied, or Released. This parameter indicates the extended travel brake switch input to the PCM.

Fuel Level
The scan tool displays Liters, Gallons. This parameter displays the volume of fuel in the tank based on input from the fuel level sensor .

Fuel Level Sensor
The scan tool displays 0-5 volts. This parameter displays the fuel level input to the PCM.

Fuel Pump Relay
The scan tool displays ON or OFF. This parameter indicates the PCM commanded state of the fuel pump relay control circuit.

Fuel Tank Pressure
The scan tool range -17.5 to 7.5 inches H2O (-33 to 14 mmHg) / 0 to 5 volts. This parameter indicates the fuel tank pressure sensor input to the PCM. The PCM uses the signal to determine the fuel tank pressure. The PCM uses the fuel tank pressure sensor input to determine the status of the EVAP system diagnostics.

Fuel Trim Cell
This parameter indicates the current fuel trim cell.

Generator L Terminal
The scan tool displays OK or No Output. This parameter indicates the PCM commanded state of the generator L terminal. The PCM uses the L terminal to command the generator voltage regulator ON and OFF.

Generator PWM
The scan tool displays 0-100 percent . This parameter indicates the generator field duty cycle as commanded by the voltage regulator. The PCM monitors the duty cycle using the generator F terminal circuit.

HO2S Bank 1 Sensor 1
The scan tool range is 0-1275 mV (0-1.275 volts). This parameter indicates the output voltage for HO2S bank 1 sensor 1 (rear bank fuel control oxygen sensor). The voltage should fluctuate constantly within a range between about 50 mV (lean exhaust) and 800 mV (rich exhaust) while operating in Closed Loop.

HO2S Bank 1 Sensor 2
The scan tool range is 0-1275 mV (0-1.275 volts). This parameter indicates the output voltage for HO2S bank 1 sensor 2 (post catalyst oxygen sensor). The voltage should fluctuate within a range between about 50 mV (lean exhaust) and 800 mV (rich exhaust) while operating in Closed Loop. The post-catalyst HO2S output voltage will fluctuate slowly over a longer period of time, compared to the fuel control oxygen sensor s. This is due to the oxygen storage capacity of an efficiently operating catalyst.

HO2S Bank 2 Sensor 1
The scan tool range is 0-1275 mV (0-1.275 volts). This parameter indicates the output voltage for HO2S bank 2 sensor 1 (front bank fuel control oxygen sensor). The voltage should fluctuate constantly within a range between about 50 mV (lean exhaust) and 800 mV (rich exhaust) while operating in Closed Loop.

HO2S Warm-up Bn1 Sen 2
The scan tool displays Seconds. This parameter indicates the time to warm-up for HO2S bank 1 sensor 2.

IAC Position
The scan tool range is 0-255 counts. This parameter displays the PCM commanded position of the idle air control pintle in counts. A larger number of counts indicates a retracted IAC valve which allows more air the idle air passage. The IAC position should respond quickly to changes in engine load in order to maintain the desired idle RPM.

IAT
The scan tool range is -40°C to 140°C (-40°F to 284°F). This parameter indicates the temperature of the intake air based on the signal voltage from the intake air temperature sensor .

Ignition 0
The scan tool displays ON, or OFF. This parameter indicates the status of the ignition 0 input to the PCM.

Ignition 1
The scan tool range is 0-25.5 volts. This parameter indicates the system voltage detected by the PCM.

Injector PWM Bank 1 / Bank 2
The scan tool range 0-985 milliseconds. This parameter indicates the PCM commanded pulse width for the bank 1 and bank 2 injectors.

IPC Fuel Disable
The scan tool displays Active, or Inactive. This parameter indicates the status of the theft deterrent fuel disable command.

Knock Retard
The scan tool range 0-45 degrees. This parameter indicates the amount of timing retard commanded by the PCM.

Long Term FT Avg. Bn1
The scan tool range is -99 to 99 percent . This parameter indicates the average Long Term FT correction for bank 1 calculated by the PCM during the current ignition cycle.

Long Term FT Avg Bn 2
The scan tool range is -99 to 99 percent . This parameter indicates the average Long Term FT correction for bank 2 calculated by the PCM during the current ignition cycle.

Long Term FT Bank 1
The scan tool range is -99 to 99 percent . This parameter indicates the Long Term FT correction for bank 1 as commanded by the PCM.

Long Term FT Bank 2
The scan tool range is -99 to 99 percent . This parameter indicates the Long Term FT correction for bank 2 as commanded by the PCM.

Loop Status
The scan tool displays Open, or Closed. This parameter indicates the state of the fuel control system. A CLOSED display indicates that the PCM is using the signals from the heated oxygen sensor s to control the fuel system.

Loss of Match Counter
The scan tool range is 0-255 counts. This parameter indicates the loss of CKP sensor A and CKP sensor B signal correlation.

Low Res. Ref. Pulses
The scan tool range is 0-255 counts. This parameter indicates the low res reference signal calculated by the PCM. The PCM determines the low res signal from CKP sensor s A and B.

Low Speed Fan Relay
The scan tool displays ON, or OFF. This parameter indicates the PCM commanded state of the low speed cooling fans.

MAF
The scan tool range is 0-655 grams per second (g/s). This parameter indicates the volume of air entering the engine.

MAF Frequency
The scan tool range is 0-65535 Hz. This parameter indicates the MAF sensor frequency based on the volume of air entering the engine. The PCM converts the signal frequency to grams per second (g/s).

MAP
The scan tool range is 10-105 kPa / 0-5 volts. This parameter indicates the manifold absolute pressure sensor input to the PCM.

Med. Res. Ref. Pulses
The scan tool range 0-255 counts. This parameter indicates the reference pulses based on the CKP signal input.

MIL
The scan tool displays ON, or OFF. This parameter indicates the PCM commanded state of the malfunction indicator lamp (MIL).

Misfire Current #1 through #8
The scan tool range is 0-255 counts. This parameter indicates the possible misfires being detected on each cylinder during the last 2000 cylinder firing events. The counters may normally display some activity, but the activity should be very low and equal for all cylinders.

Misfire Cycle Delay Counter
The scan too range is 0-255 counts. If the misfire diagnostic is interrupted, due to vehicle operation outside the conditions for running DTC P0300, this parameter indicates the number of engine cycles left before the test misfire test is re-enabled.

Misfire History #1 through #8
The scan tool range is 0-255 counts. This parameter indicates the total level of misfire that has been detected on each cylinder. The misfire history counters will not update or show any activity until a misfire or DTC P0300 has become active. The misfire history counter will update every 200 cylinder firing events.

Non-Driven Wheel Speed
The scan tool range is 0-255 km/h (0-158 mph). This parameter indicates the speed of the rear wheels. The PCM receives the information from the EBTCM via class 2 serial data.

Odometer
The scan tool range is 0-1677722. This parameter indicates the actual vehicle miles stored in the PCM.

PCM Ride Control Signal
The scan tool displays NORMAL, or FIRM.

Short Term FT Bank 1
The scan tool range is -99 to 99 percent . This parameter indicates the Short Term FT correction for bank 1 as commanded by the PCM.

Short Term FT Bank 2
The scan tool range is -99 to 99 percent . This parameter indicates the Short Term FT correction for bank 2 as commanded by the PCM.

Short Term FT Avg Bn 1
The scan tool range is -99 to 99 percent . This parameter indicates the average Short Term FT correction for bank 1 calculated by the PCM during the current ignition cycle.

Short Term FT Avg Bn 2
The scan tool range is -99 to 99 percent . This parameter indicates the average Short Term FT correction for bank 2 calculated by the PCM during the current ignition cycle.

SP/High Speed Fan Relays
The scan tool displays ON, or OFF. This parameter indicates the PCM commanded state of the series parallel, and the cool fan 1 relays.

Spark
The scan tool range is 0-64 degrees. This parameter indicates the amount of spark advance commanded by the PCM.

Start-up ECT
The scan tool range is -40°C to 140°C (-40°F to 284°F). This parameter indicates the engine coolant temperature at start-up.

Starter Relay Status
The scan tool displays ON, or OFF. This parameter indicates the PCM commanded state of the starter relay control circuit.

TCC Brake Switch
The scan tool displays Applied, or Released. This parameter indicates the torque converter clutch brake switch input to the PCM.

TCC Slip Speed
The scan tool range is 0-8192 RPM. This parameter indicates the amount of slip between the engine and transaxle input shaft.

Total Misfire Current Count
The scan tool range is 0-255 counts. This parameter indicates the total number of cylinder firing events that were detected as being misfires during the last 200 crankshaft revolution sample period.

TP Angle
The scan tool range is 0-100 percent . This parameter indicates the throttle angle calculated by the PCM from the TP sensor voltage input.

TP sensor
The scan tool range is 0-5 volts. This parameter indicates the TP sensor voltage input to the PCM.

Traction Control Torque
The scan tool range is 0-100 percent . This parameter indicates the available torque that the engine is delivering to the drive wheels.

Vehicle Speed
The scan tool range is 0-255 km/h (0-158 mph). This parameter indicates the vehicle speed calculated by the PCM from the vehicle speed sensor .

VTD Password
The scan tool displays OK, or Incorrect. This parameter indicates the validity of the vehicle theft deterrent password.

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DTC P0335 CKP Sensor A Circuit Performance




Circuit Description
The PCM uses dual crankshaft position (CKP A and CKP B) sensors to determine crankshaft position. The PCM supplies an ignition voltage and a ground for each sensor. During engine rotation, a slotted ring, machined into the crankshaft, causes the sensors to return a series of ON and OFF pulses to the PCM. The PCM uses these pulses to decode the position of the engine crankshaft.

The PCM uses two basic methods of decoding the engine position: Angle Based and Time Based (using either CKP A or CKP B sensor input). During normal operation, the PCM uses the angle based method. In order to operate in this mode, the PCM must receive signal pulses from both CKP sensors. The PCM uses the signal pulses to determine an initial crankshaft position, and to generate MEDRES (24X reference) and LORES (4X reference) signals. Once the initial crank position is determined, the PCM continuously monitors both sensors for valid signal inputs. As long as both signal inputs remain, the PCM will continue to use the angle based mode.

When either CKP signal is lost, the PCM will compare the MEDRES signal to the camshaft position (CMP) sensor signal. If the PCM detects a valid CMP signal, and the MEDRES to CMP signal correlation is correct, the PCM determines that CKP sensor A is at fault. However, if the MEDRES to CMP correlation is incorrect, the PCM determines that CKP sensor B is at fault. If the PCM determines that CKP sensor A is at fault, DTC P0335 will set. The PCM will switch from angle based mode to Time Based mode B using CKP sensor B signal input.

Conditions for Running the DTC
The engine is cranking or running.

Conditions for Setting the DTC
The PCM detects a loss of CKP sensor A signal.

Action Taken When the DTC Sets
The PCM illuminates the malfunction indicator lamp (MIL) during the second consecutive trip in which the diagnostic test runs and fails.
The PCM stores the conditions present when the DTC set as Freeze Frame/Failure Records data.
Conditions for Clearing the MIL/DTC
The PCM will turn the MIL OFF after the third consecutive trip in which the diagnostic runs and passes.
The history DTC will clear after 40 consecutive warm-up cycles have occurred without a malfunction.
The DTC can be cleared by using the scan tool Clear DTC Information function.
Diagnostic Aids
Notice: Use the connector test adapter kit J 35616-A for any test that requires probing the following items:

• The PCM harness connectors

• The electrical center fuse/relay cavities

• The component terminals

• The component harness connector

Using this kit will prevent damage caused by the improper probing of connector terminals.

Ignition system DTCs set with the ignition in the START position if the starter relay or the starter is inoperative. When the PCM enables starter operation, the PCM also initiates the diagnostic test routines for DTCs P0335, P0340, and P0385. The PCM will not receive signal input from the CKP and CMP sensors if a condition exists which prevents the engine from cranking. When this occurs, the DTCs will set.

If DTC P0615 is set, diagnose DTC P0615 first. If DTC P0335, P0340, and/or P0385 are set and no trouble is found, check for the following conditions:

Is there a no-crank condition or an intermittent no-crank condition?
Was an attempt made to crank the engine with the shift lever not in P/N?
Procedures for Selecting Crank Position Sensing Decode Mode
When diagnosing the crankshaft position sensors, it may be necessary to enable a specific decode mode (Angle, Time A, or Time B). To enable a specific crank decode, using the scan tool, perform the following steps:

Turn the ignition to the RUN/ON position.
Select Engine Output Controls.
Select Crank Position Sensing Decode Mode.
Select the desired mode (Angle, Time A, or Time B) by pressing SELECT STATE.
Command the decode mode by pressing COMMAND STATE.
The commanded state remains valid for the current ignition cycle. A specific decode mode can not be commanded with the engine running, or after commanding a desired decode mode. To command a different decode mode, you must cycle the ignition OFF and ON.

Test Description
The numbers below refer to the step numbers on the diagnostic table.

This step determines if the ignition feed circuit to the CKP A, CKP B, and the CMP is shorted to a ground. If all three DTCs are set, this indicates the circuit is shorted to a ground or a sensor is internally shorted. All three DTCs set because the ignition feed circuits are internally connected within the PCM. The engine will not start with this condition.

DTC P0386 indicates an intermittent loss of CKP sensor B signal while in Time B mode. DTC P0386 only sets after the PCM detects a loss of CKP sensor A signal and has switched to Time B mode.

During normal operation, the PCM uses the Angle Mode to determine engine position. In order to operate in this mode, the PCM must receive valid input from both CKP sensors. If the PCM detects a loss of CKP sensor A signal, the PCM switches to a Time B mode using CKP sensor B input to determine engine position. If the PCM detects a loss of CKP sensor B, the PCM switches to a Time A mode using CKP sensor A input to determine engine position.

During engine operation, if moving the harnesses and connectors related to CKP sensor A results in a switch to Time B mode, may also cause an engine stall condition, an intermittent condition in the harnesses or connectors is present. If the harnesses and connectors are OK, CKP sensor A may be the cause of the intermittent condition.

In order to test the CKP sensor A signal circuit, the PCM must be commanded to Time A mode using the scan tool. This allows the PCM to monitor input signals from CKP sensor A. Refer to Diagnostic Aids for the procedures to selecting the Crank Decode Mode.

This step determines if the CMP sensor is shorted internally. If the 12 Volt Reference parameter changes from Fault to OK, the condition is with the sensor.

This step determines if the CKP A sensor is shorted internally. If the 12 Volt Reference parameter changes from Fault to OK, the condition is with the sensor.

This step determines if the CKP B sensor is shorted internally. If the 12 Volt Reference parameter changes from Fault to OK, the condition is with the sensor.
DTC P0336 Crankshaft Position (CKP) Sensor A Performance




Circuit Description
The PCM uses dual crankshaft position (CKP A and CKP B) sensors to determine crankshaft position. The PCM supplies an ignition voltage and a ground for each sensor. During engine rotation, a slotted ring, machined into the crankshaft, causes the sensors to return a series of ON and OFF pulses to the PCM. The PCM uses these pulses to decode the position of the engine crankshaft.

The PCM uses two basic methods of decoding the engine position: Angle Based and Time Based (using either CKP A or CKP B sensor input). During normal operation, the PCM uses the angle based method. In order to operate in this mode, the PCM must receive signal pulses from both CKP sensors. The PCM uses the signal pulses to determine an initial crankshaft position, and to generate MEDRES (24X reference) and LORES (4X reference) signals. Once the initial crank position is determined, the PCM continuously monitors both sensors for valid signal inputs. As long as both signal inputs remain, the PCM will continue to use the angle based mode.

When either CKP signal is lost, the PCM will compare the MEDRES signal to the camshaft position (CMP) sensor signal. If the PCM detects a valid CMP signal, and the MEDRES to CMP signal correlation is correct, the PCM determines that CKP sensor A is at fault. However, if the MEDRES to CMP correlation is incorrect, the PCM determines that CKP sensor B is at fault. If the PCM determines that CKP sensor B is at fault, DTC P0385 will set. The PCM will switch from angle based mode to Time Based mode A using CKP sensor A signal input. If, after switching to Time Base A mode, the PCM detects an intermittent loss of CKP sensor A signal, DTC P0336 will set.

Conditions for Running the DTC
• The engine is cranking or running.

• DTC P0385 has set.

Conditions for Setting the DTC
The PCM detects an intermittent loss of CKP sensor A signal.

Action Taken When the DTC Sets
The PCM illuminates the malfunction indicator lamp (MIL) during the second consecutive trip in which the diagnostic test runs and fails.
The PCM stores the conditions present when the DTC set as Freeze Frame/Failure Records data.
Conditions for Clearing the MIL/DTC
The PCM will turn the MIL OFF after the third consecutive trip in which the diagnostic runs and passes.
The history DTC will clear after 40 consecutive warm-up cycles have occurred without a malfunction.
The DTC can be cleared by using the scan tool Clear DTC Information function.
Diagnostic Aids
Notice: Use the connector test adapter kit J 35616-A for any test that requires probing the following items:

• The PCM harness connectors

• The electrical center fuse/relay cavities

• The component terminals

• The component harness connector

Using this kit will prevent damage caused by the improper probing of connector terminals.

If the condition is intermittent, refer to Intermittent Conditions in Symptoms.


Procedures for Selecting Crank Position Sensing Decode Mode
When diagnosing the crankshaft position sensors, it may be necessary to enable a specific decode mode (Angle, Time A, or Time B). To enable a specific crank decode, using the scan tool, perform the following steps:

• Turn the ignition to the RUN/ON position.

• Select Engine Output Controls.

• Select Crank Position Sensing Decode Mode.

• Select the desired mode (Angle, Time A, or Time B) and press SELECT STATE.

• Command the decode mode by pressing COMMAND STATE.

The commanded state remains valid for the current ignition cycle. A specific decode mode can not be commanded with the engine running, or after commanding a desired decode mode. To command a different decode mode, you must cycle the ignition OFF and ON.

Test Description
The numbers below refer to the step numbers on the diagnostic table.

During normal operation, the PCM uses the Angle Mode to determine engine position. In order to operate in this mode, the PCM must receive valid input from both CKP sensors. If the PCM detects a loss of CKP sensor A signal, the PCM switches to a Time B mode using CKP sensor B input to determine engine position. If the PCM detects a loss of CKP sensor B, the PCM switches to a Time A mode using CKP sensor A input to determine engine position. If the PCM detects a loss of CKP sensor B signal, DTC P0385 will set. DTC P0336 will only set if a problem with CKP sensor A occurs while in Time A mode. DTC P0385 must be diagnosed first.

To properly verify any repair to CKP sensor A harnesses/connectors, the system must be commanded to operate in Time A mode. This forces the PCM to use CKP sensor A to determine engine position. If the system is functioning normally, DTC P0336 should not reset.
DTC P0385 Crankshaft Position (CKP) Sensor B Circuit




Circuit Description
The PCM uses dual crankshaft position (CKP A and CKP B) sensors to determine crankshaft position. The PCM supplies an ignition voltage and a ground for each sensor. During engine rotation, a slotted ring, machined into the crankshaft, causes the sensors to return a series of ON and OFF pulses to the PCM. The PCM uses these pulses to decode the position of the engine crankshaft.

The PCM uses two basic methods of decoding the engine position: Angle Based and Time Based (using either CKP A or CKP B sensor input). During normal operation, the PCM uses the angle based method. In order to operate in this mode, the PCM must receive signal pulses from both CKP sensors. The PCM uses the signal pulses to determine an initial crankshaft position, and to generate MEDRES (24X reference) and LORES (4X reference) signals. Once the initial crank position is determined, the PCM continuously monitors both sensors for valid signal inputs. As long as both signal inputs remain, the PCM will continue to use the angle based mode.

When either CKP signal is lost, the PCM will compare the MEDRES signal to the camshaft position (CMP) sensor signal. If the PCM detects a valid CMP signal, and the MEDRES to CMP signal correlation is correct, the PCM determines that CKP sensor A is at fault. However, if the MEDRES to CMP correlation is incorrect, the PCM determines that CKP sensor B is at fault. If the PCM determines that CKP sensor B is at fault, DTC P0385 will set. The PCM will switch from angle based mode to Time Based Mode A using CKP sensor A signal input.

Conditions for Running the DTC
• Engine speed is more than 20 RPM .

• MAF is more than 2.5 gps.

Conditions for Setting the DTC
The PCM detects a loss of CKP sensor B signal.

Action Taken When the DTC Sets
The PCM illuminates the malfunction indicator lamp (MIL) during the second consecutive trip in which the diagnostic test runs and fails.
The PCM stores the conditions present when the DTC set as Freeze Frame/Failure Records data.
Conditions for Clearing the MIL/DTC
The PCM will turn the MIL OFF after the third consecutive trip in which the diagnostic runs and passes.
The history DTC will clear after 40 consecutive warm-up cycles have occurred without a malfunction.
The DTC can be cleared by using the scan tool Clear DTC Information function.
Diagnostic Aids
Notice: Use the connector test adapter kit J 35616-A for any test that requires probing the following items:

• The PCM harness connectors

• The electrical center fuse/relay cavities

• The component terminals

• The component harness connector

Using this kit will prevent damage caused by the improper probing of connector terminals.

If the condition is intermittent, refer to Intermittent Conditions in Symptoms.

Ignition system DTCs set with the ignition in the START position if the starter relay or the starter is inoperative. When the PCM enables starter operation, the PCM also initiates the diagnostic test routines for DTCs P0335, P0340, and P0385. If a condition exists which prevents the engine from cranking, the PCM will not receive signal input from the CKP and CMP sensors, and the DTCs will set.

If DTC P0615 is set, diagnose DTC P0615 first. If DTC P0335, P0340, and/or P0385 are set and no trouble is found, check for the following conditions:

• Is there a no-crank condition or an intermittent no-crank condition?

• Was an attempt made to crank the engine with the shift lever not in P/N?


Procedures for Selecting Crank Position Sensing Decode Mode
When diagnosing the crankshaft position sensors, it may be necessary to enable a specific decode mode (Angle, Time A, or Time B). To enable a specific crank decode, using the scan tool, perform the following steps:

• Turn the ignition to the RUN/ON position.

• Select Engine Output Controls.

• Select Crank Position Sensing Decode Mode.

• Select the desired mode (Angle, Time A, or Time B) and press SELECT STATE.

• Command the decode mode by pressing COMMAND STATE.

The commanded state remains valid for the current ignition cycle. A specific decode mode can not be commanded with the engine running, or after commanding a desired decode mode. To command a different decode mode, you must cycle the ignition OFF and ON.
DTC P0386 Crankshaft Position (CKP) Sensor B Performance
Circuit Description
The PCM uses dual crankshaft position (CKP A and CKP B) sensors to determine crankshaft position. The PCM supplies an ignition voltage and a ground for each sensor. During engine rotation, a slotted ring, machined into the crankshaft, causes the sensors to return a series of ON and OFF pulses to the PCM. The PCM uses these pulses to decode the position of the engine crankshaft.

The PCM uses two basic methods of decoding the engine position: Angle Based and Time Based, using either CKP A or CKP B sensor input. During normal operation, the PCM uses the angle based method. In order to operate in this mode, the PCM must receive signal pulses from both CKP sensors. The PCM uses the signal pulses to determine an initial crankshaft position, and to generate MEDRES (24X reference) and LORES (4X reference) signals. Once the initial crank position is determined, the PCM continuously monitors both sensors for valid signal inputs. As long as both signal inputs remain, the PCM will continue to use the angle based mode.

When either CKP signal is lost, the PCM will compare the MEDRES signal to the camshaft position (CMP) sensor signal. If the PCM detects a valid CMP signal, and the MEDRES to CMP signal correlation is correct, the PCM determines that CKP sensor A is at fault. However, if the MEDRES to CMP correlation is incorrect, the PCM determines that CKP sensor B is at fault. If the PCM determines that CKP sensor A is at fault, DTC P0335 will set. The PCM will switch from angle based mode to time based Mode B using CKP sensor B signal input. If, after switching to time based Mode B, the PCM detects an intermittent loss of CKP sensor B signal, DTC P0386 will set.

Conditions for Running the DTC
• The engine is cranking or running.

• DTC P0335 has set.

• No cam faults present.

• Engine speed is more than 20 RPM.

• PCM has switched to Time B mode.

Conditions for Setting the DTC
The PCM detects an intermittent loss of CKP sensor B signal.

Action Taken When the DTC Sets
The PCM illuminates the malfunction indicator lamp (MIL) during the second consecutive trip in which the diagnostic test runs and fails.
The PCM stores the conditions present when the DTC set as Freeze Frame/Failure Records data.
Conditions for Clearing the MIL/DTC
The PCM will turn the MIL OFF after the third consecutive trip in which the diagnostic runs and passes.
The history DTC will clear after 40 consecutive warm-up cycles have occurred without a malfunction.
The DTC can be cleared by using the scan tool Clear DTC Information function.
Diagnostic Aids
Notice: Use the connector test adapter kit J 35616-A for any test that requires probing the following items:

• The PCM harness connectors

• The electrical center fuse/relay cavities

• The component terminals

• The component harness connector

Using this kit will prevent damage caused by the improper probing of connector terminals.

If the condition is intermittent, refer to Intermittent Conditions in Symptoms.


Procedures for Selecting Crank Position Sensing Decode Mode
When diagnosing the crankshaft position sensors, it may be necessary to enable a specific decode mode (Angle, Time A, or Time B). To enable a specific crank decode, using the scan tool, perform the following steps:

• Turn the ignition to the RUN/ON position.

• Select Engine Output Controls.

• Select Crank Position Sensing Decode Mode.

• Select the desired mode (Angle, Time A, or Time B) and press SELECT STATE.

• Command the decode mode by pressing COMMAND STATE.

The commanded state remains valid for the current ignition cycle. A specific decode mode can not be commanded with the engine running, or after commanding a desired decode mode. To command a different decode mode, you must cycle the ignition OFF and ON.

Test Description
The numbers below refer to the step numbers on the diagnostic table:

During normal operation, the PCM uses the Angle Mode to determine engine position. In order to operate in this mode, the PCM must receive valid input from both CKP sensors. If the PCM detects a loss of CKP sensor A signal, the PCM switches to a Time B Mode using CKP sensor B input to determine engine position. If the PCM detects a loss of CKP sensor B, the PCM switches to a Time A Mode using CKP sensor A input to determine engine position. If the PCM detects a loss of CKP sensor A signal DTC P0335 will set. DTC P0386 will only set if a problem with CKP sensor B occurs while in Time B Mode. DTC P0335 must be diagnosed first.

To properly verify any repair to CKP sensor A harnesses/connectors, the system must be commanded to operate in Time B mode. This forces the PCM to use CKP sensor B to determine engine position. If the system is functioning normally, DTC P0386 should not reset.
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AJxtcman
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Report this Post02-23-2007 09:05 PM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post

AJxtcman

1098 posts
Member since Nov 2006
This is from 99 and prior. The crank part # is different. I am still looking for info.

Reluctor Ring
The reluctor ring is cast onto the crankshaft between the 3 and 4 main journals. The reluctor ring has 24 evenly spaced notches or air gaps and an additional 8 unevenly spaced notches for a total of 32.

As the crankshaft makes one complete revolution, both the A and B sensors will produce 32 ON-OFF pulses per revolution. In addition, the A sensor is positioned 27 degrees of crankshaft revolution before the B sensor. This creates a unique pattern of ON-OFF pulses sent to the ignition control module so that it can recognize crankshaft position.

------------------
Cadillac Tech
ASE MASTER TECH since 1988

86 Northstar Fiero
85 RX7 former SCCA car
56 TR3 small mouth 6.0L
A.J. Whiteley

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AJxtcman
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Report this Post02-23-2007 09:50 PM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post

AJxtcman

1098 posts
Member since Nov 2006
Crank is different for 2006 FWD
2006 Cadillac DTS

Electronic Ignition (EI) System Description
Electronic Ignition (EI) System Operation
The electronic ignition (EI) system produces and controls the high energy secondary spark. This spark ignites the compressed air/fuel mixture at precisely the correct time, providing optimal performance, fuel economy, and control of exhaust emissions. The engine control module (ECM) primarily collects information from the crankshaft position (CKP) and camshaft position (CMP) sensors to control the sequence, dwell, and timing of the spark.

Crankshaft Position (CKP) Sensor
The crankshaft position (CKP) sensor circuits consist of an engine control module (ECM) supplied 5-volt reference circuit, a low reference circuit, and an output signal circuit. The CKP sensor is an internally magnetic biased digital output integrated circuit sensing device. The sensor detects magnetic flux changes of the teeth and slots of a 58-tooth reluctor wheel on the crankshaft. Each tooth on the reluctor wheel is spaced at 60-tooth spacing, with 2 missing teeth for the reference gap. The CKP sensor produces an ON/OFF DC voltage of varying frequency, with 58 output pulses per crankshaft revolution. The frequency of the CKP sensor output depends on the velocity of the crankshaft. The CKP sensor sends a digital signal, which represents an image of the crankshaft reluctor wheel, to the ECM as each tooth on the wheel rotates past the CKP sensor. The ECM uses each CKP signal pulse to determine crankshaft speed and decodes the crankshaft reluctor wheel reference gap to identify crankshaft position. This information is then used to determine the optimum ignition and injection points of the engine. The ECM also uses CKP sensor output information to determine the camshaft relative position to the crankshaft, to control camshaft phasing, and to detect cylinder misfire.

Crankshaft Reluctor Wheel
The crankshaft reluctor wheel is part of the crankshaft. The reluctor wheel consists of 58 teeth and a reference gap. Each tooth on the reluctor wheel is spaced 6 degrees apart with a 12-degree space for the reference gap. The pulse from the reference gap is known as the sync pulse. The sync pulse is used to synchronize the coil firing sequence with the crankshaft position, while the other teeth provide cylinder location during a revolution.

Camshaft Position (CMP) Sensor
The camshaft position (CMP) sensor is triggered by a notched reluctor wheel built onto the exhaust camshaft sprocket. The CMP sensor provides four signal pulses every camshaft revolution. Each notch, or feature of the reluctor wheel is of a different size which is used to identify the compression stroke of each cylinder and to enable sequential fuel injection. The CMP sensor is connected to the engine control module (ECM) by the following circuits:

• A 5-volt reference circuit

• A low reference circuit

• A signal circuit

Ignition Coil/Module
Each ignition coil/module has the following circuits:

• An ignition voltage circuit

• A ground

• An ignition control (IC) circuit

• A low reference circuit

The engine control module (ECM) controls the individual coils by transmitting timing pulses on the IC circuit of each ignition coil/module to enable a spark event.

The spark plugs are connected to each coil by a short boot. The boot contains a spring that conducts the spark energy from the coil to the spark plug. The spark plug electrode is tipped with platinum for long wear and higher efficiency.

Engine Control Module (ECM)
The engine control module (ECM) controls all ignition system functions, and constantly corrects the spark timing. The ECM monitors information from various sensor inputs that include the following:

• The throttle position (TP) sensor

• The engine coolant temperature (ECT) sensor

• The mass air flow (MAF) sensor

• The intake air temperature (IAT) sensor

• The vehicle speed sensor (VSS)

• The engine knock sensor (KS)

• The manifold absolute pressure (MAP) sensor

Modes of Operation
During normal operation the engine control module (ECM) controls all ignition functions. If either the crankshaft position (CKP) or camshaft position (CMP) sensor signal is lost, the engine will continue to run because the ECM will default to a limp home mode using the remaining sensor input. Each coil is internally protected against damage from excessive voltage. If one or more coils were to fail in this manner, a misfiring condition would result. Diagnostic trouble codes are available to accurately diagnose the ignition system with a scan tool.

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AJxtcman

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Member since Nov 2006
Crankshaft Position Sensor Replacement 2006+
Removal Procedure




Remove the intake manifold. Refer to Intake Manifold Replacement .
Disconnect the crankshaft position (CKP) sensor wiring harness electrical connector (1) from the CKP sensor.



Remove the CKP sensor bolt. (cylinder heads shown removed, for clarity).
Remove the CKP sensor.
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Report this Post02-24-2007 09:35 AM Click Here to See the Profile for DeabionniSend a Private Message to DeabionniDirect Link to This Post
Wow, AJxtcman,


Thanks for taking the time to post all of this information. This stuff is waaayyyy over my head, but maybe soon people like Ryan, Will, and others will be able to figure out how to use a 2000+ N* in their Fiero and use the stock Caddy PCM. Once that happens, I believe that the N* swap will become as commonplace as the 3800SC swap.

Keep up the good work guys!
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Report this Post02-24-2007 07:42 PM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post
 
quote
Originally posted by Deabionni:

Wow, AJxtcman,


Thanks for taking the time to post all of this information. This stuff is waaayyyy over my head, but maybe soon people like Ryan, Will, and others will be able to figure out how to use a 2000+ N* in their Fiero and use the stock Caddy PCM. Once that happens, I believe that the N* swap will become as commonplace as the 3800SC swap.

Keep up the good work guys!


I had a Northstar and was looking for a 4spd manual trans. This led me to a Fiero. I don't think I would have ever have bought a Fiero. I think the 3800 SC is a better combo. I worked with a Fiero fanatic for the past three year up until last September. I used to tell him the the P car stands for Piece of sh!t. I have grown found of them now. If I did not work at a Caddy dealer and if I did another it would be a 3800 SC. If I do another it will be a Northstar because they are FREE and all the part are FREE to me. I drive by three Fiero's every day and wonder about taking on another.
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Report this Post02-26-2007 07:25 AM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post
AS FAR AS I KNOW NO COMPANY OFFERS ANY TUNING SOFTWARE FOR THE PCM. IT RUNS A SEIMENS PCM, BUT THE 4.0L RUNS A DELPHI AND DIFFERENT SOFTWARE PROTOCAL. THE AURORA PCM MAY BE TUNABLE.
.
.
2000 EK,KD, KE,KF, KS,KY, Modles
Powertrain Control Module Connector End Views
Table 1: Powertrain Control Module (PCM) Connector C1
Table 2: Powertrain Control Module (PCM) Connector C2


Powertrain Control Module (PCM) Connector C1



Connector Part Information
• Complete Assembly (W/O TPA) - 12191488

• TPA (Blue) - 12176408

• Terminal - 12084913

Pin
Wire Color
Circuit No.
Function

1
ORN
1799
Camshaft Position PCM Input

2
LT BLU/WHT
1800
Crankshaft Position Sensor A Signal

3-4
--
--
Not used

5
DK GRN
890
Fuel Tank Pressure Sensor Signal

6
PPL
806
Crank Request

7-9
--
--
Not Used

10
TAN
472
Intake Air Temperature (IAT) Sensor Signal

11
PPL
773
Transaxle Range Switch C Input

12
YEL
772
Transaxle Range Switch B Input

13
BLK/WHT
771
Transaxle Range Switch A Input

14
YEL
573
Crankshaft Position Sensor B Signal

15
--
--
Not Used

16
DK BLU/WHT
1231
Transaxle Input Speed Sensor Low

17
RED/BLK
1230
Transaxle Input Speed Sensor High

18
PPL
1807
Class 2 Serial Data (between EBTCM and PCM)

19
PNK
1390
PCM Ignition 0 Feed

20
ORN
2240
PCM Battery Feed

21
ORN
2240
PCM Battery Feed

22
RED
2127
Cylinder 7 IC Control

23
LT GRN
432
Manifold Absolute Pressure (MAP) Sensor Signal

24
--
--
Not Used

25
DK GRN
335
Low Speed Cooling Fans Control Circuit

26
DK GRN/WHT
817
4K/Mi Speed

27
LT GRN/BLK
444
IAC B Low

28
LT GRN/WHT
1749
IAC B High

29
LT BLU/WHT
1747
IAC A High

30
LT BLU/BLK
1748
IAC A Low

31
DK GRN
676
HO2S Bank 1 Sensor 1 Heater Control Circuit High

32
BRN/WHT
419
MIL Control

33
YEL/BLK
3122
HO2S Bank 2 Sensor 1 Heater Control Circuit Low

34
TAN/BLK
464
Delivered Torque Output

35
DK GRN
83
Cruise Inhibit Output

36
--
--
Not Used

37
BLK
1744
Fuel Injector #1 Control

38
PNK/BLK
1746
Fuel Injector #3 Control

39
LT GRN/BLK
1745
Fuel Injector #2 Control

40
BLK/WHT
845
Fuel Injector #5 Control

41
WHT
776
Transaxle Range Switch Parity Input

42
YEL
492
Mass Air Flow (MAF) Sensor Signal

43
ORN/BLK
463
Desired Torque Input

44
GRY
847
Extended Travel Brake Switch Input

45-49
--
--
Not Used

50
DK BLU/WHT
1677
HO2S Bank 1 Sensor 2 Signal Low

51
DK GRN/WHT
1678
HO2S Bank 1 Sensor 2 Signal High

52
TAN/WHT
1664
HO2S Bank 1 Sensor 1 Signal Low

53
PPL/WHT
1665
HO2S Bank 1 Sensor 1 Signal High

54
TAN/WHT
1669
HO2S Bank 2 Sensor 1 Signal Low

55
PPL/WHT
1668
HO2S Bank 2 Sensor 1 Signal High

56
YEL
400
VSS Sensor Input High

57
PPL
401
VSS Sensor Input Low

58
RED
631
Camshaft Position Sensor Ignition Feed

59
PPL
1807
Class 2 Serial Data (between IPC, DLC, and PCM)

60
BLK/WHT
451
PCM Power Ground

61
PPL
2121
Cylinder 1 IC Control

62
DK BLU
417
Throttle Position (TP) Sensor Signal

63
PNK
39
PCM Ignition 1 Feed

64-65
--
--
Not Used

66
PNK/BLK
429
AIR Pump Solenoid Control

67
LT BLU/WHT
1229
Pressure Control Solenoid Low

68
YEL/BLK
3112
HO2S Bank 1 Sensor 1 Heater Control Circuit Low

69
RED/BLK
1228
Pressure Control Solenoid High

70
DK GRN/WHT
465
Fuel Pump Relay Control

71
RED
1676
EGR Valve Control

72
PPL
1490
Powertrain Induced Chassis Pitch Status Output (RTD Lift/Dive)

73
WHT
1310
EVAP Vent Solenoid Control

74
--
--
Not Used

75
BRN
436
AIR Pump A Relay Control

76
LT BLU/BLK
844
Fuel Injector #4 Control

77
YEL/BLK
846
Fuel Injector #6 Control

78
--
--
Not Used

79
DK BLU/WHT
878
Fuel Injector #8 Control

80
RED/BLK
877
Fuel Injector #7 Control



Powertrain Control Module (PCM) Connector C2



Connector Part Information
• Complete Assembly (W/O TPA) - 12191488

• TPA (Clear) - 12176409

• Terminal - 12084913

Pin
Wire Color
Circuit No.
Function

1-2
--
--
Not Used

3
BLK/WHT
451
PCM Power Ground

4
BLK
2760
Intake Air Temperature (IAT) Ground

5
--
--
Not Used

6
ORN/BLK
469
Manifold Absolute Pressure (MAP) Sensor Ground

7-8
--
--
Not Used

9
YEL
2174
Reference Low (Front/Even Bank Ignition Assembly)

10
--
--
Not Used

11
BLK
2762
Transaxle Fluid Temperature (TFT) Sensor Ground

12
BLK
2753
EGR Pintle Position Sensor Ground

13
BLK
2759
Fuel Level Sensor and Fuel Tank Pressure Sensor Ground

14
BLK
2751
AC Pressure Sensor Ground

15
BLK/WHT
451
PCM Power Ground

16
--
--
Not Used

17
GRY
2709
5 Volt Reference B - Fuel Tank Pressure Sensor Feed

18
--
--
Not Used

19
DK BLU
496
Knock Sensor Signal

20
TAN/BLK
231
Engine Oil Pressure Switch Input

21
LT BLU
2123
Cylinder #3 IC Control

22
RED/WHT
2122
Cylinder #2 IC Control

23
BRN
1174
Low Oil Level Switch Input

24
LT BLU/BLK
396
Cruise Engaged Input

25
LT GRN
2867
Crankshaft Position Sensor B Ignition Feed

26
BLK/WHT
451
PCM Power Ground

27
--
--
Not Used

28
YEL
2868
Crankshaft Position Sensor B Ground

29-30
--
--
Not Used

31
YEL
410
Engine Coolant Temperature (ECT) Sensor Signal

32
YEL/BLK
1227
Transaxle Fluid Temperature (TFT) Sensor Signal

33-34
--
--
Not Used

35
GRY
1716
Knock Sensor Ground

36
--
--
Not Used

37
RED
1226
Transaxle Pressure Manifold Switch C Input

38-39
--
--
Not Used

40
RED
225
Generator L Terminal Control

41
--
--
Not Used

42
DK GRN/WHT
428
EVAP Canister Purge Valve Control

43
LT GRN
1222
Shift Solenoid A Control

44
TBD
447
Starter Relay Control

45
YEL/BLK
1223
Shift Solenoid B Control

46
TAN/BLK
422
Torque Converter Clutch (TCC) Control

47
DK GRN/WHT
459
A/C Compressor Clutch Control

48
BLK/WHT
1423
HO2S Bank 1 Sensor 2 Heater Control Circuit Low

49
GRY
2704
5 Volt Reference A - MAP Sensor Feed

50
GRY
2702
5 Volt Reference A - EGR Pintle Position Sensor Feed

51
GRY
2701
5 Volt Reference A - TP Sensor Feed

52
BRN
1456
EGR Pintle Position Sensor Signal

53
--
--
Not Used

54
BRN
436
Air Pump 2 Relay Control

55
DK BLU
473
High Speed Cooling Fans Control

56
WHT
121
Tachometer Input

57
GRY
2700
5 Volt Reference B - A/C Pressure Sensor Feed

58
--
--
Not Used

59
DK GRN/WHT
2124
Cylinder #4 IC Control

60
LT BLU/WHT
2126
Cylinder #6 IC Control

61
PPL/WHT
2128
Cylinder #8 IC Control

62
DK GRN
2125
Cylinder #5 IC Control

63-64
--
--
Not Used

65
LT GRN
1867
Crankshaft Position Sensor A Ignition Feed

66
YEL/BLK
1868
Crankshaft Position Sensor A Ground

67
PNK/BLK
632
Camshaft Position Sensor Ground

68
BLK
2761
Engine Coolant Temperature (ECT) Sensor Ground

69
BLK
2752
Throttle Position (TP) Sensor Ground

70
GRY
435
EGR Valve Control Ground

71
GRY
2175
Reference Low (Rear/Odd Bank Ignition Assembly)

72
PPL
1589
Fuel Level Sensor Signal

73
PNK
1224
Transaxle Pressure Manifold Switch A Input

74
RED/BLK
380
A/C Pressure Sensor Signal

75-78
--
--
Not Used

79
GRY
23
Generator F Terminal Feedback

80
PPL
420
Torque Converter Clutch (TCC) Brake Switch Input



--------------------------------------------------------------------------------
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AJxtcman
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Report this Post02-26-2007 07:39 AM Click Here to See the Profile for AJxtcmanSend a Private Message to AJxtcmanDirect Link to This Post

AJxtcman

1098 posts
Member since Nov 2006
This PCM I have no info on yet, but it may be tunable.
.
.
2004 - 2005 Cadillac DeVille
--------------------------------------------------------------------------------

Powertrain Control Module Connector End Views
Table 1: PCM Connector C1
Table 2: PCM Connector C2
Table 3: PCM Connector C3


PCM Connector C1



Connector Part Information
• 15357147

• 56-Way F Micro 64 (BLU)

Pin
Wire Color
Circuit No.
Function

1-2
--
--
Not Used

3
BRN
436
AIR Pump Relay Control

4
DK BLU
473
High Speed Cooling Fan Relay Control

5-7
--
--
Not Used

8
DK GRN/ WHT
817
Vehicle Speed Signal

9-10
--
--
Not Used

11
RED/BLK
380
A/C Refrigerant Pressure Sensor Signal

12
PPL
1589
Fuel Level Sensor Signal - Primary

13-14
--
--
Not Used

15-16
PPL
1807
Class 2 Serial Data (Primary)

17
--
--
Not Used

18
WHT
1310
EVAP Canister Vent Solenoid Control

19
PNK
39
Ignition 1 Voltage

20
ORN
240
Battery Positive Voltage

21
--
--
Not Used

22
DK GRN
83
Cruise Control Inhibit Signal

23
WHT
121
Engine Speed Signal

24-30
--
--
Not Used

31
GRY
2709
5-Volt Reference

32
BLK
2751
Low Reference

33-34
--
--
Not Used

35
BLK
2759
Low Reference

36-37
--
--
Not Used

38
WHT
1390
Off/Run/Crank Voltage

39
GRY
847
Extended Travel Brake Switch Signal

40
--
--
Not Used

41
DK GRN
890
Fuel Tank Pressure Sensor Signal

42
--
--
Not Used

43
GRY
2700
5-Volt Reference

44
DK GRN/ WHT
465
Fuel Pump Relay Control - Primary

45
YEL
447
Starter Relay Coil Control

46
DK GRN
335
Low Speed Cooling Fan Relay Control

47
--
--
Not Used

48
LT BLU/BLK
396
Cruise Control Engaged Signal

49-50
--
--
Not Used

51
PPL
420
TCC Brake Switch/Cruise Control Release Signal

52
YEL
5
Crank Voltage

53
PNK/ WHT
1101
Damping Lift/Dive Signal

54
--
--
Not Used

55
BRN/ WHT
419
MIL Control

56
DK GRN/ WHT
459
A/C Compressor Clutch Relay Control



PCM Connector C2



Connector Part Information
• 15357131

• 73-Way F Micro 64 (BLK)

Pin
Wire Color
Circuit No.
Function

1
BRN
1174
Oil Level Switch Signal

2
RED
1676
EGR Solenoid High Control

3
PPL/WHT
421
Rear AIR pump Relay Control

4
--
--
Not Used

5
TAN/ WHT
3111
HO2S Low Signal (Bank 1 Sensor 1)

6
GRY
2702
5-Volt Reference

7
--
--
Not Used

8
GRY
2701
5-Volt Reference

9
GRY
435
EGR Solenoid Low Control or EGR Solenoid Control

10
RED
225
Generator Turn On Signal

11
LT BLU
1876
Knock Sensor 2 Signal

12
GRY
23
Generator Field Duty Cycle Signal

13
GRY
1716
Knock Sensor 1 (KS1) Low Reference

14
--
--
Not Used

15
PPL
3120
HO2S High Signal (Bank 1 Sensor 2)

16
BRN
1456
EGR Valve Position Signal

17
LT GRN/ WHT
1749
IAC Coil B High Control

18
YEL
410
ECT Sensor Signal

19
DK BLU
496
Knock Sensor 1 Signal

20
TAN/ WHT
3121
HO2S Low Signal (Bank 1 Sensor 2)

21
PNK/BLK
632
Low Reference

22
DK BLU
417
TP Sensor Signal

23
PPL
2121
IC 1 Control

24
LT BLU/WHT
2126
IC 6 Control

25
ORN
1799
High Resolution Signal

26
--
--
Not Used

27
GRY
2303
Low Reference Knock Sensor 2 (KS2)

28
YEL/BLK
573
Crank Sensor B Signal

29
PPL/WHT
3110
HO2S High Signal (Bank 1 Sensor 1)

30
GRY
2704
5-Volt Reference (MAP)

31
LT BLU/WHT
1800
Crank Sensor A Signal

32
--
--
Not Used

33
BLK
2761
Low Reference (Coolant Sensor)

34
RED
2127
IC 7 Control

35
BLK
2753
Low Reference (EGR)

36
ORN/BLK
469
Low Reference (MAP)

37
BLK
2752
Low Reference (TPS)

38
--
--
Not Used

39
BRN
2129
Low Reference (EST Bank 1)

40
--
--
Not Used

41
YEL/BLK
1868
Low Reference

42
BRN/ WHT
2130
Low Reference (EST Bank 2)

43
LT BLU
2123
IC 3 Control

44-45
--
--
Not Used

46
YEL
2868
Low Reference (Crank Return)

47
TAN/BLK
231
Oil Pressure Switch Signal

48
--
--
Not Used

49
RED
631
12-Volt Reference

50
LT GRN
1867
12-Volt Reference

51
LT GRN
2867
12-Volt Reference

52
--
--
Not Used

53
LT BLU/BLK
1748
IAC Coil A Low Control

54
BLK/WHT
3113
HO2S Heater Low Control (Bank 1 Sensor 1)

55
BLK/WHT
845
Fuel Injector 5 Control

56
BRN
3122
HO2S Heater Low Control (Bank 1 Sensor 2)

57
DK BLU/WHT
878
Fuel Injector 8 Control

58
LT GRN/BLK
444
IAC Coil B Low Control

59
LT BLU/BLK
844
Fuel Injector 4 Control

60
YEL/BLK
846
Fuel Injector 6 Control

61
LT BLU/WHT
1747
IAC Coil A High Control

62
DK GRN/WHT
2124
IC 4 Control

63
PPL/WHT
2128
IC 8 Control

64
DK GRN
2125
IC 5 Control

65
RED/WHT
2122
IC 2 Control

66
PNK/BLK
1746
Fuel Injector 3 Control

67
LT GRN
432
MAP Sensor Signal

68
--
--
Not Used

69
RED/BLK
877
Fuel Injector 7 Control

70
DK GRN/WHT
428
EVAP Canister Purge Solenoid Control

71
BLK
1744
Fuel Injector 1 Control

72
LT GRN
1745
Fuel Injector 2 Control

73
BLK
451
Ground



PCM Connector C3



Connector Part Information
• 15357148

• 56-Way F Micro 64 (GRY)

Pin
Wire Color
Circuit No.
Function

1
PNK
1224
Transmission Fluid Pressure Switch Signal A

2
YEL/BLK
1223
2-3 Shift Solenoid or Shift Solenoid B Valve Control

3
LT BLU/WHT
1229
PC Solenoid Valve Low Control (Sol. A)

4
TAN/BLK
464
Delivered Torque Signal

5
YEL
772
Transmission Range Switch Signal B

6
GRY
773
Transmission Range Switch Signal C

7
WHT
776
Transmission Range Switch Signal P

8
--
--
Not Used

9
--
--
Not Used

10
YEL/BLK
1227
TFT Sensor Signal

11
YEL
492
MAF Sensor Signal

12-15
--
--
Not Used

16
LT GRN
3212
HO2S Heater Low Control (Bank 2 Sensor 1)

17-18
--
--
Not Used

19
TAN/ WHT
3211
HO2S Low Signal (Bank 2 Sensor 1)

20-21
--
--
Not Used

22
PPL
401
Signal Low - Front/VSS Low Signal/OSS Low Signal

23-26
--
--
Not Used

27
ORN/BLK
463
Requested Torque Signal

28-31
--
--
Not Used

32
BLK/WHT
771
Transmission Range Switch Signal A

33
DK BLU/WHT
1231
AT ISS Low Signal

34
BLK
2760
Low Reference (IAT)

35
BLK
2762
Low Reference (Trans Fluid Temp Sensor)

36-42
--
--
Not Used

43
PPL/WHT
3210
HO2S High Signal (Bank 2 Sensor 1)

44
LT GRN
1222
Valve Control (1-2 Shift Solenoid or Shift Solenoid A)

45
RED/BLK
1228
PC Solenoid Valve High Control (Sol. A)

46
--
--
Not Used

47
YEL
400
Signal High - Front/VSS High Signal/OSS High Signal

48
RED
1226
Transmission Fluid Pressure Switch Signal C

49-50
--
--
Not Used

51
TAN
472
IAT Sensor Signal

52-53
--
--
Not Used

54
RED/BLK
1230
AT ISS High Signal

55
TAN/BLK
422
TCC Solenoid Valve Control

56
--
--
Not Used

------------------
Cadillac Tech
ASE MASTER TECH since 1988

86 Northstar Fiero
85 RX7 former SCCA car
56 TR3 small mouth 6.0L
A.J. Whiteley

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