Land Rover Defender 90 110 Workshop 1984 Rover Manual
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V8 CYLINDER ENGINE 1121 -- Reclaiming cylinder head threads Damaged or stripped threads in the cylinder head can be salvaged by fitting Helicoils as follows: I~Ioles A -These threc holes may be drilled 0.3906 in. dia. x 0.937 + 0.040 in. deep. Tapped with Helicoil Tap No. 6 CPB or 6CS x 0.875 in. (min.) deep (g UNC 1%D insert). Holes B - These eight holes may be drilled 0.3906 in. dia. x 0.812 + 0.040 in. deep. Tapped with Helicoil Tap No. 6 CBB 0.749 in. (min.) deep (a UNC 1MD insert). Holes C - These four holes may be drilled 0.3906 in. dia. x 0.937 + 0.040 in. deep. Tapped with Helicoil Tap No. 6 CPB or 6CS x 0.875 in. (min.) deep ($ UNC 1 %D insert). Holes D - These four holes may be drilled 0.261 in. dia. x 0.675 + 0.040 in. deep. Tapped with Helicoil Tap No. 4CPB or 4CS x 0.625 in. (min.) deep (% UNC 1 KD insert). Holes E - These six holes may be drilled 0.3906 in. dia. x 0.937 + 0.040 in. deep. Tapped with Hclicoil Tap No. 6 CPR or 6CS x 0.875 in. (min.) deep (i UNC lW3 insert). - NOTE: Right-hand cylinder head illustrated. American projection. F Exhaust manifold face G Inlet manifold face H Front face I Rear face J Front of engine F A I I / I ST 799M G 99
El V8 CYLINDER ENGINE REMOVE AND OVERHAUL FLYWHEEL 6. Place a chisel immediately above the drilled hole and strike it sharply to split the starter ring gear. 1. Remove the retaining bolts and withdraw the flywheel from the crankshaft. 2. Examine the flywheel clutch face for cracks, scores and overheating. If the overall thickness of the flywheel is in excess of the minimum thickness i.e. 39,93 mm (1.572 in) it can be refaced provided that after machining it will not be below the minimum thickness. Remove the three dowels before machining. 3. Examine the ring gear and if worn or the teeth are chipped and broken it can be renewed as follows: 3 7. Heat the new ring gear uniformly to between 170 degrees and 175 degrees C (338 degrees to 347 degrees F) but do not exceed the higher temperature. 8. Place the flywheel, clutch side down, on a flat surface. 9. Locate the heated starter ring gear in position on the flywheel, with the chamfered inner diameter towards the flywheel flange. If the starter ring gear is chamfered both sides, it can be fitted either way round. 10. Press the starter ring gear firmly against the flange until the ring contracts sufficiently to grip the flywheel. 11. Allow the flywheel to cool gradually. Do NOT hasten cooling in any way or distorting may occur. 12. Fit new clutch assembly location dowels to the flywheel. I ST803M 2 4. Drill a 10 mm (.375 in) diameter hole axially between the diameter of the starter ring sufficiently deep to weaken the ring. Do NOT allow the drill to enter the flywheel. and piace a cioth over the fiywheei to protect rhe operator from flying fragments. root of any tooth and the inner 7 5. Secure the flywheel in a vice fittcd with soft jaws 9 WARNING: Take adequate precautions against flying fragments when splitting the ring gear. I ST804M f-3 :.v 100
V8 CYLINDER ENGINE REMOVE TIMING GEAR COVER AND WATER PUMP 1. Place an oil drip-tray beneath the timing cover and 2. Remove the crankshaft pulley bolt and special 3. Remove the two bolts securing the sump to the remove the oil filter element. washer and withdraw the pulley. bottom of the timing cover. ST805M 1 Renewing timing cover oil seal S. Remove the seven drive screws and withdraw the mud shield and the oil seal. 6. Position the gear cover with the front face uppermost and the underside supported across the oil seal housing bore on a suitable wooden block. 7. Enter the oil seal, lip side leading, into the housing bore. 8. Press in the oil seal until the plain face is 1,s mm (0.062 in) approximately below thc gear cover face. 9. Fit the mud shield and secure with the screws. 4. Remove the remaining timing cover retaining bolts and withdraw the cover complete with oil pump. REMOVE AND OVERHAUL THE OIL PUMP 1. Remove the bolts from the oil pump cover. 2. Withdraw the oil pump cover. 3. Lift off the cover gasket. 4. Withdraw the oil pump gears. 101
12 Dismantle pump Assemble pump 0 ,,-,-.. ..__ . ...
V8 CYLINDER ENGINE 112 /, ,d.%:h. 2. Withdraw the chaln wheels complete with timing 6. Measure the camshaft journals for overall wear, ovality and taper. The diameters of the five journals are as follows commencing from the front of the shaft. c. 3 chain. 3. Withdraw thc camshaft whilst taking particular carc not to daniagc thc bearings in the cylinder block. _. ... , .... ., . : “I. . Examine components 4. Visually examine all parts for wear. Check the camshaft bearing journals and cams for wcar, pits, scores and overheating. Should any of these conditions be present the shaft should be renewed. 5. Examine the links and pins of the timing chain for wcar and compare its condition with that of a I.ew chain. Similarly the teeth of the chain wheels should be inspected and if necessary the wheels should be renewed. Number 1 journal 1.786 to 1.785 ins Number 2 journal 1.750 to 1.755 ins Number 3 journal 1.726 to 1.725 ins Number 4 journal 1.696 to 1.695 ins Number 5 journal 1.666 to 1.665 ins 7. To check the camshaft for bow, rest the two end journals i.e. numbers 1 and 5 on ‘V’ blocks and mount a dial gauge on the centre journal. Rotate the shaft and note the reading. If the run out is more than 0,05 mm (0.002 in) it should be renewed. REMOVE AND OVERHAUL CONNECTING-RODS AND PISTONS 1. Withdraw the remaining bolts and remove [he 2. Remove the sump oil strainer. 3. Removc the connccting-rod caps and retain them in sequence for reassembly. 4. Screw the guide bolts 605351 onto the connecting- rods. sump. continued 103
V8 CYLINDER ENGINE 5. Push the connecting-rod and piston assembly up the cylinder bore and withdraw it from the top. Retain the connecting -rod and piston assemblies in sequence with their respective caps. 6. Remove the guide bolts 605351 from the connecting -rod. Overhaul NOTE: The connecting-rods, caps and bearing shells must be retained in sets, and in the correct sequence. Remove the piston rings over the crown of the piston. If the same piston is to be refitted, mark it relative to its connecting -rod to ensure that the original assembly is maintained. 7. Withdraw the gudgeon pin, using tool 18G 1150 as follows: a. Clamp the hexagon body of 18G 1150 in a vice. b. Position the large nut flush with the cnd of the c. Push the screw forward until the nut contacts the centre scrcw. thrust race. ST777M 104 d. Locate the piston adaptor 18G 1150 E with its e long spigot inside the bore of the hexagon body. e. Fit the remover/replacer bush of 18G 1150 on the centre screw with the flanged end away from the gudgeon pin. f. Screw the stop -nut about half-way onto the smaller threaded end of the centre screw, leaving a gap ‘A’ of 3 mm (B in) between this nut and the remover/replacer bush. ypJ g. Lock the stop-nut securely with the lock screw. h. Check that the remover -replacer bush is correctly positioned in the bore of the piston. i. Push the connecting-rod to the right to expose the end of the gudgeon pin, which must be located in the end of the adaptor ‘d’. j. Screw the large nut up to the thrust race. k. Hold the lock screw and turn the large nut until the gudgeon pin has been withdrawn from the piston. Dismantle the tool. continued d a c b!
V8 CYLINDER ENGINE . 8. As an alternative to tool 18G 1150, press the gudgeon pin from the piston using an hydraulic press and the components which comprise tool 605350 as follows: a. Place the base of tool 605350 on the bed of an hydraulic press which has a capacity of 8 tons (8 tonnes). b. Fit the guide tube into the bore of the base with its countersunk face uppermost. c. Push the piston to one side so as to expose one end of the gudgeon pin and locate this end in the guide tube. d. Fit the spigot end of the small diameter mandrel into the gudgeon pin. e. Press out the gudgeon pin, using the hydraulic press. _.. . ... . .: ...._-.. >.W .: .... _.., .. E -. New pistons Pistons are available in service standard sizc and in oversizes of 0,25 mm (0.010 in) and 0,50 mm (0.020 in). Service standard size pistons are supplied 0,0254 mm (0.001 in) oversize. When ..fitting new service standard size pistons to a cylinder block, check for correct piston to bore clearance, honing the bore if necessary. Bottom of piston skirt-bore clearance should be 0,018 to 0,033 mm (0.0007 to 0.0013 in). NOTE: The temperature of the piston and cylinder block must be the same to ensure accurate measurement. When reboring the cylinder block, the crankshaft main bearing caps must be fitted and tightened to the correct torque. 9. Check the cylinder bore dimension at right angles to the gudgeon pin, 40 to 50 mm (1/2 to 2 in) from the top. 10. Check the piston dimension at right angles to the gudgeon pin, at the bottom of the skirt. 11. The piston dimension must be 0,018 to 0,033 mm (0.0007 to 0.0013 in) smaller than the cylinder. 12. If new piston rings arc to be fitted without reboring, deglaze the cylinder walls with a hone, without incrcasing the bore diameter to provide a cross -hatch finish. Original pistons Remove the carbon deposits, particularly from the ring grooves. Examine the pistons for signs of damage or excessive wear; refer to new pistons for the pistons if necessary. -0thnA n$ he,- r; tha w..,r-;on ,- -.-Y~-,-- E:+ -a. IIILLLIVU I CIILAllt; LIIL 1 IIIIIIE) LILJLPIILL. I ,I IlLvv continued 105
lz[ V8 CYLINDER ENGINE 13. Check the compression ring gaps in the applicable cylinder, held square to thc bore with the piston. Gap limits: 0,44 to 0,56 mm (0.017 to 0.022 in). Use a fine-cut flat file to increase the gap if required. Select a new piston ring if the gap exceeds the limit. NOTE: Gapping does not apply to oil control rings. Fit piston rings 17. Fit the expander ring into the bottom groove making sure that the ends butt and do not overlap. 18. Fit two ring rails to the bottom groove, one above and one below the expander ring. 19. Fit the second compression ring with the marking ‘TOP’ uppermost and the chrome compression ring in the top groove, either way round. ST819M / 14. Temporarily fit the compression rings to the piston. 15. The ring marked ‘TOP’ must be fitted with the marking uppermost and into the second groove. The chrome ring is for the top groove and can be fitted either way round. 16. Check the compression ring clearance in the piston groove. Clearance limits: 0,Oj to O,~O mm (0.002 to 0.004 in). ST821M Examineconnec*ing-rods 20. Check the alignment of the connecting-rod. 21. Check the connecting-rod small end, the gudgeon pin must be a press fit. 106 cont inucd
V8 CYLINDER ENGINE 112 Check crankshaft bearings 22. Locate the bearing upper shell into the connecting- rod. 23. Locate the connecting-rod and bearing on to the applicable crankshaft journal, noting that the domed shape boss on the connecting-rod must face towards the front of the engine on the right -hand bank of cylinders and towards the rear on the left -hand bank. 24. When both connecting-rods are fitted, the bosses will face inwards towards each other. 25. Place a piece of Plastigauge across the centre of the lower half of the crankshaft journal. 26. Locate the bearing lower shell into the connecting - rod cap. 27. Locate the cap and shell on to the connecting-rod. Note that the rib on the edge of the cap must be the same side as the shape boss On the IR/IIORTANT: The connecting-rods, caps and bearing - - connecting-rod. 28. Secure the connecting -rod cap, and tighten to the shells must be retained in sets, and in the correct sequence, , correct torque. .... 29. Do not rotate the crankshaft or connecting-rod 30. Remove the connecting-rod cap and shell. 31. Using the scalc printed on the Plastigauge packet, measure the flattened Plastigauge at its widest point. 32. The graduation that most closely corresponds to the width of the Plastigauge indicates the bearing clearance. 33. The correct bearing clearance with new or overhauled components is 0,013 to 0,06 mm 34. If a bearing has been in service, it is advisable to fit a new bearing if the clearance exceeds 0,08 mm (0.003 in). 35. If a new bearing is being fitted, use selective assembly to obtain the correct clearance. 36. Wipe off the Plastigauge with an oily rag. DO NOT scrape it off. while the Plastigauge is in USC. (0.0006 !e 0.0022. in>. Assembling pistons to connecting-rods 37. If an hydraulic press and tool 605350 was used for dismantling, refit cach piston to its connccting-rod as follows: a. Check that the base of tool 605350 and the guide tube are fitted as follows: - Place the base of tool 605350 on the bed of an hydraulic press which has a capacity of 8 tons (8 tonnes). Fit the guide tube into the bore of the base with its countersunk face uppermost. b. Fit the long mandrel inside the guide tube. c. Fit the connccting-rod into the piston with the markings together if the original pair arc being used, then place the piston and connecting-rod assembly over the long mandrel until the gudgeon pin boss rests on thc guidc tube. d. Fit the gudgeon pin into the piston up to the connecting-rod, and the spigot end of the small diameter mandrel into the gudgeon pin. e. Press in the gudgeon pin until it abuts the shoulder of the long mandrel. continucd 107
V8 CYLINDER ENGINE c 37 D A 38. If tool 18G 1150 was used for dismantling, refit each piston to its connecting-rod as follows: a. Clamp the hexagon body of 18G 1150 in a vice, with the adaptor 18G 1150 E positioned as in 4d. b. Remove the large nut of 18G 1150 and push the centre screw approximately 50 mm (2 in) into the body until the shoulder is exposed. c. Slide the parallel guide sleeve, grooved end last, onto the centre screw and up to the shoulder. I 1 39. d. Lubricate the gudgeon pin and bores of the connecting -rod and piston with graphited oil (Acheson’s Colloids ‘Oildag’). Also lubricate the ball race and centre screw of 18G 1150. e. Fit the connecting-rod and the piston together onto the tool with the markings together if the original pair are being used and with the connecting -rod around the sleeve up to the groove. f. Fit the gudgeon pin into the piston bore up to the connecting -rod. g. Fit the removerheplacer bush 18G 115013 with its flanged end towards the gudgeon pin. h. Screw the stop-nut onto the centre screw and adjust this nut to obtain a 1 mm (& in) end-float ‘A’ on the whole assembly, and lock the nut securely with the screw. i. Slide the assembly back into the hexagon body and screw on the large nut up to the thrust race. represents the minimum load for an acceptable interference fit of the gudgeon pin in the con necti ng -rod. k. Using the torque wrench and socket 18G 587 on the large nut, and holding the lock screw, pull the gudgeon pin in until the flange of the remover-rcplacer bush is 4 mm (0.160 in) ‘B’ from the face of the piston. Under no circumstances must this flange be allowed to contact the piston. j. Set the torque wrench 18G 537 to 12 Ibf ft. This F~::, ,e:>; CAUTION: If the torque wrench has not broken throughout the pull, the fit of the gudgeon pin to the connecting -rod is not acceptable and necessitates the renewal of components. The large nut and centre screw of the tool must be kept well -oiled. e, e. :-. “-” Remove the tool and check that the piston moves freely on the gudgeon pin and that no damage has occurred during pressing. I’ I ST778M I08