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Land Rover Defender 1999 2002my Workshop Supplement Body Repair 3rd Edition Rover Manual
Land Rover Defender 1999 2002my Workshop Supplement Body Repair 3rd Edition Rover Manual
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12ENGINE 32 OVERHAUL 8.Carefully move connecting rod to one side of journal and using feeler gauges, measure end-float of connecting rod on journal: Connecting rod end-float =0.2 to 0.5 mm (0.008 to 0.021 in). CAUTION: If end-float exceeds limits given, replace connecting rod and repeat end-float check - See pistons, connecting rods and cylinder bores. 9.Repeat above procedures for remaining big-end bearings. 10.Fit oil pump.See this Section.PISTONS, CONNECTING RODS AND CYLINDER BORES Service repair no - 12.17.02.01 Remove 1.Remove cylinder head gasket.See this Section. 2.Remove connecting rod bearings.See this Section. 3.Remove ridge of carbon from top of cylinder bore. 4.Suitably identify each piston and connecting rod assembly to its respective cylinder bore. 5.Carefully push connecting rod to top of cylinder bore taking care that connecting rod does not contact oil squirt jet or cylinder wall, remove each piston and connecting rod assembly in turn. 6.Using a suitable expander, remove and discard piston rings from pistons. 7.Using a squared off end of an old piston ring, clean carbon from ring grooves. 8.Clean carbon from piston crown and skirt. CAUTION: Do not use abrasives on graphited area of piston skirt, do not use a wire brush or scraper on any part of the pistons. 9.Secure connecting rod in a soft jawed vice. 10.Suitably identify each piston to its connecting rod and fitted position of piston on rod. 11.Using suitable circlip pliers, remove and discard 2 circlips securing gudgeon pin. 12.Push gudgeon pin out of piston and connecting rod; remove piston. 13.Suitably identify each gudgeon pin to its respective piston. 14.Repeat above procedures for each piston.
ENGINE 33 OVERHAUL Cylinder bores - Inspection 1.Check cylinder bores for scoring. 2.Measure cylinder bore wear and ovality at a point 70 mm (2.75 in) from top of each cylinder bore: Cylinder bore diameter =84.460 to 84.442 mm (3.325 to 3.324 in) CAUTION: Measurement must be taken from side to side and front to rear of bore: CAUTION: Cylinder bore diameter and ovality must be within limits given above, no reboring, honing or glaze busting of cylinder bores is permissible; cylinder block must be replaced if bores are worn or excessively scored. Pistons and connecting rods - Inspection 1.Check each piston for cracks, burning and damage. 2.Check connecting rods for alignment. CAUTION: Do not attempt to straighten misaligned connecting rods. 3.Ensure small-end oil feed holes in connecting rods are clear. 4.Measure and record diameter of each piston at right angles to gudgeon pin axis and 46 mm (1.81 in) from bottom of skirt: Piston diameter =84.262 mm±0.009 mm (3.317 in±0.0003 in) CAUTION: Measurement point must be on the graphited area of the piston.
12ENGINE 34 OVERHAUL 5.Starting with No. 1 piston, invert piston and with arrow on piston crown pointing towards REAR of cylinder block, insert piston into No. 1 cylinder bore. 6.Position piston with bottom of skirt 25 mm (1.0 in) from top of cylinder bore. 7.Using feeler gauges, measure and record clearance between piston skirt and LEFT HAND side of cylinder bore 60 mm (2.4 in) from top of bore: Piston to cylinder bore clearance =0.171 to 0.207 mm (0.007 to 0.008 in) 8.Repeat above procedures for remaining pistons. CAUTION: Oversize pistons are not available, if piston to cylinder bore clearance exceeds limits given, repeat check using a new piston; if clearances are still excessive, replace cylinder block. Piston and 1st compression rings fitted to Engine Serial No. Prefixes 15P to 19P may be fitted to Engine Serial No. Prefixes 10P to 14P in engine sets only. Oil control and 2nd compression rings are interchangeable between all engines. 9.Check fit of each gudgeon pin in its piston. Pin must be a tight, sliding fit with no perceptible side play. 10.Measure gudgeon pin diameter at each end and centre of pin. Renew gudgeon pin and piston as an assembly if diameters are less than specified or if excessive pin to piston side play is evident. Gudgeon pin diameter =29.995 to 30.000 mm (1.180 to 1.181 in) 11.Check connecting rod small-end bushes for wear, check that gudgeon pin is a sliding fit in the bush with no perceptible side play. CAUTION: Small-end bushes cannot be replaced, a new connecting rod must be fitted.
ENGINE 35 OVERHAUL Piston ring gaps - Checking 1.Insert new compression and oil control piston rings in turn into No. 1 cylinder bore 30 mm (1.25 in) from top of bore and check ring fitted gaps; ensure rings are kept square to bore when checking gaps. 1st compression ring fitted gap =0.30 to 0.40 mm (0.012 to 0.016 in) 2nd compression ring fitted gap =0.40 to 0.60 mm (0.016 to 0.024 in) Oil control ring fitted gap =0.25 to 0.50 mm (0.01 to 0.02 in) Repeat for each cylinder bore in turn. CAUTION: Ensure rings are suitably identified with the cylinder bore in which they were checked and are fitted to the piston for that bore. 2.Fit oil control expander and ring to piston. 3.Fit 2nd compression ring with’TOP’marking upwards. 4.Fit 1st compression ring with’TOP’marking upwards. 5.Check piston ring to groove clearance: 1st compression ring -Not measured 2nd compression ring =0.050 to 0.082 mm (0.02 to 0.003 in) Oil control ring =0.050 to 0.082 mm (0.02 to 0.003 in) Pistons and connecting rods - Assembling 1.Lubricate gudgeon pin, gudgeon pin holes in piston and small-end bush with engine oil. 2.Position piston to its respective connecting rod with arrow on piston crown on the same side as the cast boss on the connecting rod. 3.Fit gudgeon pin to its respective piston and connecting rod; secure with new circlips. CAUTION: Ensure circlips are fully seated in their grooves. 4.Repeat above procedures for remaining pistons. 5.Lubricate piston rings and cylinder bores with engine oil. 6.Check that rings are free to rotate, position ring gaps at 120°to each other and away from the thrust - LH side of piston - viewed from front of piston. 7.Using a suitable piston ring clamp, compress piston rings. 8.Insert connecting rod and piston into its respective cylinder bore, ensuring that the arrow on piston crown and the cast boss on connecting rod are facing towards the front of the cylinder block. CAUTION: Ensure that connecting rod does not contact cylinder bore or oil squirt jet. Do not pull connecting rod fully down cylinder bore at this stage.
12ENGINE 36 OVERHAUL 9.Check that the cut-out in piston skirt is positioned above the oil squirt jet. 10.Repeat for other pistons in turn ensuring that pistons and connecting rods are fitted in cylinder bores from which they were removed. 11.Fit connecting rod bearings.See this Section. CAUTION: If new pistons, connecting rods or crankshaft have been fitted, it will be necessary to select correct thickness of cylinder head gasket.See this Section.CRANKSHAFT Service repair no - 12.21.33.01 Remove 1.Remove timing chain and sprockets.See this Section. 2.Remove crankshaft rear oil seal.See this Section. 3.Remove connecting rod bearings.See this Section. 4.Check that cylinder reference number is on each main bearing cap. Make suitable alignment marks between each main bearing cap and cylinder block. 5.Starting at No. 3 main bearing cap and working outwards, progressively loosen, then remove 2 bolts securing each cap. Discard main bearing cap bolts.
ENGINE 37 OVERHAUL 6.Fit 2 slave bolts into each main bearing cap in turn and ease bearing caps from cylinder block. 7.Remove and discard bearing shells from each cap. NOTE: These bearing shells are plain. 8.Using assistance, remove crankshaft. 9.Remove and discard main bearing shells and 2 thrust washers from cylinder block. NOTE: These bearing shells are grooved. 10.Remove Torx screw securing each oil squirt jet to cylinder block, remove squirt jets.Cylinder block - Inspection 1.Clean main bearing shell and thrust washer locations in cylinder block, ensure bolt holes are clean and dry. 2.Clean main bearing caps. 3.Clean crankshaft bearing journals, check oilways are clear. 4.Ensure drillings in oil squirt jets are clear. 5.Check core plugs in cylinder block for corrosion or signs of leakage, seal replacement plugs with Loctite 243. Crankshaft - Inspection 1.Check crankshaft main and big-end bearing journals for scoring, wear and ovality, make 3 checks at 120°intervals in centre of journals. Crankshaft bearing journal diameters: Main bearings = 62.000 mm±0.013 mm (2.441 in±0.001 in) Big-end bearings = 54.000±0.01 mm (2.125±0.0004in) CAUTION: Crankshafts may not be reground, only one size of main and big-end bearing shell is available and if journals are found to be scored, oval or worn, crankshaft must be replaced. Main and big-end bearing shells and thrust washers must be replaced whenever they are removed.
12ENGINE 38 OVERHAUL Crankshaft spigot bush 1.Check crankshaft spigot bush for wear, replace if necessary using the following procedures: 2.Secure crankshaft in a suitably padded vice. 3.Tap a thread in spigot bush to accommodate a suitable impulse extractor. 4.Fit impulse extractor to spigot bush. 5.Remove spigot bush. 6.Clean spigot bush recess in crankshaft. 7.Fit new spigot bush to crankshaft using a suitable mandrel. Crankshaft - Refit 1.Fit oil squirt jets, fit Torx screws and tighten to8 Nm (6 lbf.ft). 2.Lubricate new, grooved, main bearing shells with engine oil and fit to cylinder block. 3.Lubricate new thrust washers with engine oil and fit, grooved side facing outwards, to recess in each side of cylinder block No. 3 main bearing. 4.Lubricate crankshaft journals with engine oil and using assistance, position crankshaft in cylinder block. 5.Lubricate new, plain, main bearing shells with engine oil and fit to main bearing caps. 6.Fit main bearing caps in their original fitted positions ensuring that reference marks are aligned. 7.Fit and lightly tighten new main bearing cap bolts. CAUTION: Do not lubricate bolt threads. 8.Starting with No. 3 main bearing cap and working outwards, tighten main bearing cap bolts to: Stage 1 -33 Nm (24 lbf.ft) Stage 2 -Further 90 ° CAUTION: Do not carry out stages 1 and 2 in one operation. 9.Check that crankshaft rotates smoothly. 10.Assemble a magnetic base DTI to front of cylinder block with stylus of gauge on end of crankshaft. 11.Using suitably padded levers, move crankshaft rearwards and zero DTI. 12.Move crankshaft forwards and note crankshaft end-float reading on gauge. Crankshaft end-float =0.02 to 0.25 mm (0.001 to 0.011 in) CAUTION: Oversize thrust washers are not available, if end-float exceeds figure given, crankshaft must be replaced. 13.Remove DTI. 14.Fit connecting rod bearings.See this Section. 15.Fit timing chain and sprockets.See this Section. 16.Fit crankshaft rear oil seal.See this Section.
17 - EMISSION CONTROL CONTENTS Page DESCRIPTION AND OPERATION EGR SYSTEM COMPONENTS - TYPE 1 2............................................................ EGR SYSTEM COMPONENTS - TYPE 2 4............................................................ EMISSION CONTROL SYSTEMS 6....................................................................... CRANKCASE EMISSION CONTROL 7.................................................................. EXHAUST GAS RECIRCULATION 8..................................................................... EGR MODULATOR 9.............................................................................................. INLET THROTTLE (ILT) MODULATOR 10............................................................. EGR VALVE 11....................................................................................................... INLET THROTTLE (ILT) VALVE 12........................................................................ IN-LINE AIR FILTER - PRE EU´ u MODELS 13........................................................ EGR SYSTEMS 14................................................................................................. REPAIR VALVE - EGR - NON EU3 MODELS 1................................................................... VALVE - EGR - EU3 MODELS 2............................................................................ INLET THROTTLE (ILT) MODULATOR 3............................................................... SOLENOID - VALVE - EGR 3.................................................................................