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Land Rover Defender 1999 2002my Workshop Supplement Body Repair 2nd 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................................................................................. 
    						
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