ARMY *TM 9-6115-464-34 AIR FORCE TO-35C2-3 ... - Igor Chudov

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ARMY TM 9-6115 464 34AIR FORCE TO 35C2-3-445-2NAVY NAVFAC P-8-624-34Table 1-1. FITS AND TOLERANCESMfg’s Tolerances Desired Clearance Maximum MaximumComponent Allowable AllowableMinimum Maximum Minimum Maximum Wear ClearanceCYLINDER BLOCK: 3.7490 3.7510Cylinder bore dia. 3.7505 3.7515 0.0050Cylinder bore dia.(Bohn) 0.0005Cylinder bore out of round 0.0005 0.0030Cylinder bore taper 3.0665 3.0670 0.0020Main brg. bore - less brgs. 2.1870 2.1880Camshaft brg. bore - less brgs. 2.0000 2.0005Oil pump bore 0.7494 0.7500Valve tappet bore 0.003Warpage 0.0005MillingCRANKSHAFT: 2.8734 2.8744Main brg. journal dia. 0.0003 0.0030Main brg. journal out of round 0.0003 0.0020Main brg. journal taper 0.0020 0.0015Main brg. run-out at center 2.3730 2.3740 0.0030Conn. rod journal dia. 0.0003 0.0020Conn. rod journal out of round 0.0003 0.0020Conn. rod journal taper 0.1400 0.1700 0.0015Fillet radii 0.0009 0.0034Crankshaft main brg. clearance 0.0050 0.0100 0.0070Crankshaft thrust clearance 4.3100 4.3150 0.0150Seal surface dia.- rear 1.8740 1.8750 0.0150Seal surface dia. - front 0.0150CONN.ECTING ROD: 7.9980 8.0020Length - c to c 2.5260 2.5270Bearing bore - less bearings 0.0010 0.0030Br to crankshaft clearance 0.0050 0.0120 0.0050Conn. rod side clearance 0.0200Piston pin bushing bore - less 1.4370 1.4380bushing 1.2503 1.2508Piston pin bushing bore 0.0015CAMSHAFT: 2.0530 2.0540Bearing journal dia. 1.6890 1.7250 0.0020Lobe dia. meter - base to tip 0.0010 0.0100Journal run-out in vee blocks 0.0015 0.0035 0.0040Bearing clearance 0.0015 0.0055 0.0060End thrust 0.0120Back lash camshaft to crank 0.001 0.003gearPISTON:Clearance in cyl. bore (pull on 5 lb. 8 lb.1/2 x 0.0050 ribbon) -Clearance in cyl. bore (pull 3.7445 3.7455on1/2 x 0.005 ribbon bore)Piston pin bore 1.2500 1.2502 0.0010Width of ring groove - top -Keystone1/8 nom.Width of ring groove - 2nd &3rd comp 0.0975 0.0990 0.0050Width of ring groove - top -oil control 0.1880 0.1895 0.0050Width of ring groove - loweroil control 0.1880 0.1890 0.0050PISTON PIN:Length 3.0350 3.0400 ’Diameter 1.2498 1.2499 0.0020Clearance in piston 0.0000 0.0005 0.0020Clearance in connecting rod 0.0005 0.0012 0.00501-14 Change 1
Table 1-1. FITS AND TOLERANCES (CONTINUED)ARMY TM 9-6115-464-34AIR FORCE TO 35C2-3-445-2NAVY NAVFAC P-8-624-34Mfg’s. Tolerances Desired Clearance Maximum MaximumComponent Allowable AllowableMinimum Maximum Minimum Maximum Wear ClearancePISTON RING:Clearance in groove – top Keystone TaperClearance in groove – 2nd &3rd comp. 0.0040 0.0060 0.0080Clearance in groove – oilcontrol 0.0015 0.0030 0.0080Gap 0.0100 0.0200 0.0400VALVE, INTAKE:Head diameter 1.6825 1.6925Stem diameter 0.3725 0.3735Stem to guide clearance0.00250.0005 0.0025 0.0050Stem to rocker arm clearance– hot 0.0150Seat diameter in head 1.6470 1.6530Seat width in head 7/64 1/8Top of valve recessed belowcyl. hd deck 0.0210Valve seat angle 30°VALVE, EXHAUST:Head diameter 1.4950 1.5050Stem diameter 0.3725 0.3732 0.0025Stem to guide clearance 0.0015 0.0035 0.0060Stem to rocker arm clearance- hot 0.0150Seat diameter in head 1.4510 1.4560Seat width in head 7/64 1/8Top of valve recessed belowcyl. hd deck 0.0210Valve seat angle 45°VALVE GUIDE:Length 2.0325 2.9524Outside diameter 0.6265 0.6270Bore diameter - intake -ream 0.3740 0.3750 0.0030Bore diameter – exhaust –ream 0.3750 0.3760 0.0030Depth below cyl. head deck 1.3700 1.3800TAPPET, VALVE LIFTER(PUSH ROD):Body diameter 0.7485 0.74900.0030Overall length 2.2450 2.2550Clearance m bore (block) 0.0005 0.0015 0.0050VALVE SPRINGS - INTAKE& EXHAUST:Free Iength 1.7960 1.8360Total coils 6-1/4Diameter wire 0.1770Outside diameter 1.2920 1.3020Test load at 1.4920 inches(Ibs) 72 82Test load at 1.0820 inches(lb) 163 1801-15
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(c)(d)(e)Pull all slack from the le
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REPAIR INSTRUCTIONSARMY TM 9-6115-4
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ARMY *TM 9-6115-464-34 AIR FORCE TO-35C2-3 ... - Igor Chudov

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