F88161-4 Force REED STOP


F88161-4 REED STOP Force H0257F88A, H0257F88B, H0352F90B, H0352F90C, H0353E91A, H0353E91B, H0355D89A, H0356F89B, H0357C86A, H0357C87A, H0357C88B, H0357F88A, H0357F89C, H0357G90A, H040312RD, H040312SD, H040312UD, H0407E92C, H0504H88C, H0504H88D, H0504P89B, H0505C89B, H0507A89 REED
F88161-4 REED STOP Force
Rating:
38

Buy REED STOP F88161-4 Force genuine, new aftermarket parts with delivery
Number on catalog scheme: 11
 

Force entire parts catalog list:

H0257F88A 1988,1989
H0257F88B 1988,1989,1991
H0352F90B 1990
H0352F90C 1990
H0353E91A 1991
H0353E91B 1991
H0355D89A 1989
H0356F89B 1989
H0357C86A 1986
H0357C87A 1987
H0357C88B 1988
H0357F88A 1988
H0357F89C 1989
H0357G90A 1990
H040312RD 1995
H040312SD 1996,1997
H040312UD 1998,1999
H0407E92C 1992,1993,1994
H0504H88C 1988
H0504H88D 1988
H0504P89B 1989
H0505C89B 1989
H0507A89C 1989
H0507A89D 1989
H0507A90A 1990
H0507A90B 1990
H0507A90C 1990
H0507A90D 1990
H0507A91A 1991
H0507A91C 1991
H0507A92A 1992
H0507C86A 1986
H0507C87A 1987
H0507C87C 1987
H0507C88B 1988
H0507E91B 1991
H0507F87B 1987
H0507F88A 1988
H0507Z89B 1989

Information:

(1) End play for shaft (new) ... 0.114 0.038 mm(.0045 .0015 in) Maximum permissible end play (worn) ... 0.20 mm (.008 in)(2) Thickness of thrust bearing (where thrust rings contact bearing) ... 5.36 0.03 mm (.211 .001 in)(3) Tighten both band clamps with procedure that follows: a. Tighten to ... 14 1.1 N m (125 10 lb in)b. Tap (hit) clamp lightly all around.c. Tighten again to ... 14 1.1 N m (125 10 lb in)
Do not overtighten the clamps.
(4) Diameter of shaft (new) ... 15.997 to 16.005 mm (.6298 to .6301 in) Bore in the bearing (new) ... 16.035 to 16.043 mm (.6313 to .6316 in)Maximum permissible clearance between bearing and shaft (worn) ... 0.05 mm (.002 in)(5) Maximum permissible gap of oil seal ring, measured in bore of housing ... 0.25 mm (.010 in)(6) Install the compressor wheel (at room temperature) as follows: a. See Compressor Wheel Clearance for the correct shim thickness to use.b. Put compressor wheel on the shaft.c. Put a small amount of clean engine oil on the threads.d. Tighten the nut to 14 to 17 N m (125 to 150 lb in).
Do not bend or add stress to the shaft when nut is loosened or tightened.
e. Remove nut from shaft and apply 6V1541 Quick Cure Primer on the threads of the shaft and nut followed by application of 9S3265 Retaining Compound.f. Tighten nut to 4 N m (30 lb in).g. Tighten nut more as follows: For 99.0 mm (3.90 in) diameter compressor wheels, tighten the nut an additional 90°.For 86.4 mm (3.40 in) diameter compressor wheels, tighten the nut an additional 60°.(7) Shims. See Compressor Wheel Clearance for the correct shim thickness to use.(8) Thickness of each thrust ring ... 2.553 0.013 mm (.1005 .0005 in)(9) Bore in housing (new) ... 24.994 to 25.006 mm (.9840 to .9845 in) Outside diameter of the bearing (new) ... 24.882 to 24.892 mm (.9796 to .9800 in)Maximum permissible clearance between bearing and bore in housing (worn) ... 0.15 mm (.006 in)Torque for four nuts (put 5P3931 Anti-Seize Compound on threads) and bolts that hold the turbocharger to the exhaust manifold ... 55 5 N m (40 4 lb ft) Put clean engine oil in the oil inlet of the turbocharger after assembly or before installation to provide start up lubrication and/or storage protection.Compressor Wheel Clearance
a. Remove the compressor wheel from the cartridge group and place the wheel in the compressor housing. Center the wheel in the housing.b. Measure the distance from the compressor housing mounting face to the compressor wheel seating face. Measure four places at approximately 90° increments. This is dimension "A" (Fig. 1).c. Assemble the cartridge group complete except for the compressor wheel and shims. Hold the turbine wheel-shaft assembly toward the compressor end against the thrust bearing. Measure the distance from the bearing housing end face to the flinger sleeve. This is dimension "B" (Fig. 2).d. Measure the distance from the bearing housing end face to the compressor housing mounting face of the bearing housing. This is dimension "C" (Fig. 2).e. Shim thickness is C-B-A +0.23 to 0.28 mm (C-B-A +.009 to .011 in). This is the thickness of the shims to be installed between the flinger sleeve and compressor wheel.f. Shims to be of uniform thickness and free of burrs or other imperfections. Shim thickness should total 0.13 to 0.41 mm (.005 to .016 in) and consist of one or two shims selected from those specified in Step g. All measurements to be taken with dry (no lubrication) turbocharger.g. Thickness of shims: 4W7362 Shim ... 0.076 mm (.003 in)4W7357 Shim ... 0.127 mm (.005 in)4W7358 Shim ... 0.152 mm (.006 in)4W7359 Shim ... 0.178 mm (.007 in)4W7360 Shim ... 0.203 mm (.008 in)4W7361 Shim ... 0.229 mm (.009 in)4W7363 Shim ... 0.254 mm (.010 in)


Parts reed Force:

F316160
 
F316160 REED
H0202B80L, H0202B81M, H0202H79K, H0202H82N, H0252B83G, H0252H77B, H0252H78C, H0252H78D, H0254H75A, H0257F88A, H0257F88B, H0306B80C, H0307H81D, H0350H78L, H0351H76K, H0352F90B, H0352F90C, H0353E91A, H0353E91B, H0355D89A, H0356F89B, H0357C86A, H0357C87
FA572158
 
FA572158 REED PLATE W/PLUG
H0202B81M, H0202H82N, H0252B83G, H0257F88A, H0257F88B, H0307H81D, H0352F90B, H0352F90C, H0353E91A, H0353E91B, H0356F89B, H0357C86A, H0357C87A, H0357C88B, H0357F88A, H0357F89C, H0357G90A, H0357H83N
F18160 3
 
F18160 3 REED
H005201RS, H005201SD, H005201TS, H005201UD, H0052C88A, H0091H84D, H009201RS, H009201SD, H009201UD, H009201US, H0092284D, H0092H84L, H0092S88A, H0092S91A, H0093S91A, H015201RS, H015201US, H015211SS, H0152C84K, H0152S89A, H0407E92C, H0504H88C, H0504H88
FA658158
 
FA658158 REED PLATE
H040312RD, H040312SD, H040312UD, H0407E92C, H0504H88C, H0504H88D, H0504P89B, H0505C89B, H0507A89C, H0507A89D, H0507A90A, H0507A90B, H0507A90C, H0507A90D, H0507A91A, H0507A91C, H0507A92A, H0507C86A, H0507C87A, H0507C87C, H0507C88B, H0507E91B, H0507F87
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