20550356 Volvo.Penta Flange screw


20550356 Flange screw Volvo.Penta TAD520GE; TAD720GE; TAD721GE, TAD520VE; TAD720VE; TAD721VE, TAD550GE; TAD551GE; TAD750GE, TAD560VE; TAD561VE; TAD761VE, TAD734GE, TD520GE; TAD530GE; TAD531GE Flange
20550356 Flange screw Volvo Penta
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Buy Flange screw 20550356 Volvo Penta genuine, new aftermarket parts with delivery
Number on catalog scheme: 20
 

Volvo Penta entire parts catalog list:

TAD520GE; TAD720GE; TAD721GE; TAD722GE
TAD520VE; TAD720VE; TAD721VE; TAD722VE
TAD550GE; TAD551GE; TAD750GE; TAD751GE; TAD752GE; TAD753GE; TAD754GE
TAD560VE; TAD561VE; TAD761VE; TAD762VE; TAD763VE; TAD764VE; TAD765VE
TAD734GE
TD520GE; TAD530GE; TAD531GE; TAD532GE; TD720GE; TAD720GE; TAD730GE; TAD731GE; TAD732GE; TAD733GE; TAD530GE MECH; TAD530GE EDC4; TAD531GE MEC

Information:


F14. Remove the big end caps, bearing shells and bolts (Fig. F.1). If the bearing shells removed are serviceable, refit them in their original positions.
F25. Push pistons and connecting rods out of the top of the cylinders (Fig. F.2). Keep each piston and connecting rod assembly separate, each to each as markedTo Remove Pistons and Rings from Connecting Rods
1. Remove the rings from each piston.2. Remove the circlips and withdraw the gudgeon pin. If the gudgeon pin is tight in the piston bore, warm the piston in clean liquid to a temperature of 100/120°F (38/49°C).Inspection
1. Examine the pistons for scoring and clean carbon from the ring grooves. Check the clearance of the new piston rings in their respective grooves and if, with a new ring fitted the vertical groove clearance exceeds 0.008 in (0,20 mm) fit new piston.2. Check the fitted gap of the rings in the unworn portion at top of cylinder bore. For details of ring gap dimensions see "Technical Data", Pages B.6 to B.7. Ring gaps for conformable rings are with spring fitted.3. Check the fit of the gudgeon pin in the piston bore and in the small end bush. For details of piston bore, gudgeon pin and small end bush bore diameters see "Technical Data", Page B.7. When renewing a small end bush, ensure that the oil hole in the bush aligns with the hole in the connecting rod. Ream out to suit the gudgeon pin and check the connecting rod for parallelism see "Technical Data", Page B.8. The small end of the connecting rod on T4.236 engines is wedge shaped and the small end bush should be machined to suit the contours of the wedge. The earlier T4.236 connecting rod is also drilled from the big end to the small end to provide piston cooling by a feed of lubricating oil. Later T4.236 engines have piston cooling jets fitted in the cylinder block wall.4. Examine the big end bearings for wear and scoring. Also examine the crankpins for wear and ovality. For crankshaft details see page B.8.
F3To Assemble the Pistons to the Connecting Rods
If the original pistons are being used they must be assembled to the original connecting rods. For markings of pistons and connecting rods see Figs. F.8 and F.9.1. The cavity in the piston crown is off-set towards one side of the piston. Place the piston on the connecting rod with the cavity towards the side of the rod which carries the rod and cap identification numbers. Insert the gudgeon pin and fit new circlips, warming the piston, if necessary.2. Fit the rings in the following order, ensuring that the ring gaps are equally spaced around the piston.(a) 4.2482 Engines (see Fig. F.4)
F4Chrome Faced Spring Loaded Conformable Scraper - above gudgeon pin.Internally Stepped Taper Faced Compression - second groove.Molybdenum Faced Internally Stepped Barrel Faced Compression - top groove.When fitting the spring loaded conformable scraper ring, ensure that the latch pin enters both ends of the spring. With the ring gap diametrically opposite to the latch pin, position the oil control ring over spring correctly located in annular groove of ring, i.e., between the oil control ring and the bottom of the ring groove in the piston.When fitting the internally stepped taper faced compression ring, ensure that the "step" is towards the piston crown.When fitting the top compression ring, ensure that the manufacturers mark is towards the piston crown.(b) 4.248 Engines (4 Ring)
**Spring Loaded Conformable Scraper - above gudgeon pin.Internally Stepped Compression - third groove.*Internally Stepped Compression - second groove.Chrome Insert Barrel Faced Compression - top groove.When fitting sealed power rings, ensure that the ends of the spring loaded segment butt together and do not overlap.**Some earlier A4.248 engines had a sealed power scraper ring fitted in the 4th groove. *On some earlier A4.248 engines rated up to 2,000 rev/min, the second compression ring is plain cast iron.Some later engines, rated up to 2,000 rev/min, have internally stepped chrome faced rings in both 2nd and 3rd grooves.When fitting internally stepped compression rings, ensure that the step is towards the piston crown.When fitting the spring loaded conformable scraper ring, ensure that the latch pin enters both ends of the spring. With the ring gap diametrically opposite to the latch pin, position the oil control ring over spring correctly located in annular groove of ring, i.e., between the oil control ring and the bottom of the ring groove in the piston.(c) 4.248 Engines (3 Ring)
Chrome Faced Spring Loaded ConformableScraper - above gudgeon pin.Internally Stepped Taper Faced Compression - second groove.Molybdenum Faced Internally Stepped Barrel Faced Compression - top groove.When fitting the spring loaded conformable scraper ring, ensure that the latch pin enters both ends of the spring. With the ring gap diametrically opposite to the latch pin, position the oil control ring over the spring correctly located in the annular groove of ring, i.e., between the oil control ring and the bottom of the ring groove in the piston.When fitting the internally stepped compression rings in the second and top grooves, ensure that the "step" is towards the piston crown.(d) T4.236 Engines (see Fig. F.6)
F6Chrome Faced Spring Loaded Conformable Scraper - above gudgeon pin.Cast Iron Taper Faced Compression - second groove.Molybdenum Faced Wedge Compression - top groove.When fitting the spring loaded conformable scraper ring, ensure that the latch pin enters both ends of the spring. With the ring gap diametrically opposite to the latch pin, position the oil control ring over spring correctly located in annular groove, i.e., between the oil control ring and the bottom of the ring groove in the piston.When fitting the compression rings, ensure that the manufacturers mark is towards the piston crown.(e) 4.236 Engines fitted with cast iron liners
Slotted Scraper - below gudgeon pin.Slotted Scraper - above gudgeon pin.Internally Stepped Compression - third groove.Internally Stepped Compression - second groove.*Chrome Faced Compression - top groove*With later combine engines, a plain cast iron ring is fitted in the top groove. This plain ring is completely interchangeable with the earlier chrome faced


Parts flange Volvo Penta:

948217
 
948217 Flange screw
251A, AD31D; AD31D-A; AD31XD, AD31L-A; AD31P-A; AD41L-A, AD41D; D41D; TAMD41D, D12D-A MG; D12D-E MG, D12D-A MH; D12D-B MH; D12D-C MH, D2-55; D2-55B; D2-55C, D3-110I-A; D3-110I-B; D3-110I-C, D4-180I-B; D4-180I-C; D4-180I-D, D4-180I-F; D4-225A-F; D4-22
967949
 
967949 Flange screw
251A, 3.0GLP-A; 3.0GLP-B; 3.0GLM-A, 4.3GL-A; 4.3GL-B; 4.3GL-C, 4.3GXi-A, 4.3GXi-B; 4.3GXi-BF; 4.3OSi-B, 5.0GXi-A; 5.7Gi-A; 5.7GXi-A, 5.0GXi-B; 5.0GXi-BF; 5.0OSi-B, 5.7GL-A; 5.7GL-B; 5.7GL-C, 8.1Gi-A; 8.1Gi-B; 8.1Gi-BF, 8.1Gi-E; 8.1Gi-EF; 8.1GXi-D, 8.
990940
Flange nut
990940 Flange nut
1372, D1-13; D1-13B; D1-20, D11A-A; D11A-B; D11A-C, D11B1-A MP; D11B2-A MP, D11B3-A MP; D11B4-A MP, D12D-A MG; D12D-E MG, D12D-A MH; D12D-B MH; D12D-C MH, D13B-A MP; D13B-B MP; D13B-C MP, D13B-E MH; D13B-E MH (FE); D13B-N MH, D13B-F MG; D13B-E MG; D1
984736
Flange screw
984736 Flange screw
1372, D11A-A; D11A-B; D11A-C, D11B1-A MP; D11B2-A MP, D11B3-A MP; D11B4-A MP, D13B-A MP; D13B-B MP; D13B-C MP, D13B-E MH; D13B-E MH (FE); D13B-N MH, D13B-F MG; D13B-E MG; D13B-E MG (FE), D13C1-A MP; D13C2-A MP; D13C3-A MP, D16C-A MG, D16C-A MH; D16C-
984752
Flange screw
984752 Flange screw
1372, D11A-A; D11A-B; D11A-C, D11B1-A MP; D11B2-A MP, D11B3-A MP; D11B4-A MP, D13B-A MP; D13B-B MP; D13B-C MP, D13B-E MH; D13B-E MH (FE); D13B-N MH, D13B-F MG; D13B-E MG; D13B-E MG (FE), D13B-J MP; D13B-M MP, D13C1-A MP; D13C2-A MP; D13C3-A MP, D16C-
984813
 
984813 Flange screw
1372, D11B1-A MP; D11B2-A MP, D11B3-A MP; D11B4-A MP, D16C-A MG, D16C-D MH, TAD1170VE; TAD1171VE; TAD1172VE, TAD1351VE; TAD1352VE; TAD1353VE, TAD1352VE, TAD1371VE; TAD1372VE; TAD1373VE, TAD1640GE; TAD1641GE; TAD1642GE, TAD1641VE; TAD1642VE; TAD1643VE
11700326
 
11700326 Flange screw
D5A-T; D5A-TA; D5A-B TA, D5A-T; D5A-TA; D5A-B TA, TAD520GE; TAD720GE; TAD721GE, TAD520VE; TAD720VE; TAD721VE, TAD550GE; TAD551GE; TAD750GE, TAD560VE; TAD561VE; TAD761VE, TAD734GE, TAD750VE; TAD760VE, TD520GE; TAD530GE; TAD531GE, TD520VE; TD720VE
966818
Flange nut
966818 Flange nut
D16C-A MG, D5A-T; D5A-TA; D5A-B TA, D9A2A; D9A2A D9-425; D9A2A D9-500, TAD1630P; TWD1630P; TWD1630PP, TAD1630V; TWD1630V, TAD1640GE; TAD1641GE; TAD1642GE, TAD1641VE; TAD1642VE; TAD1643VE, TAD520GE; TAD720GE; TAD721GE, TD520GE; TAD530GE; TAD531GE, TID
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