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-8-824-343-97. REPLACEMENT OF INTERFERENCE SUPPRESSION COMPONENTS.a. Refer to the Operator and Unit Maintenance Manual to replace fuel transfer pumps.b. To replace capacitors at load terminal:(1) Remove screws (1, figure 3–148) and disconnect and tag electrical leads.(2) Remove nuts (2), screws (3), capacitors (4) and Iockwashers (5) from bracket (6).(3) Reassemble in reverse order using new capacitors,c. Refer to figure 3-130 to replace capacitors in static exciter.Figure 3-148. Interference Suppression Components3-311
ARMY TM 9-6115 464 34AIR FORCE TO 35C2-3-445-2NAVY NAVFAC P-8-624-34c. Cleaning. Inspection. and RepairWARNINGSolvent, Dry Cleaning P-D-680, Type II is flammable and moderately toxic to skin, eyes and respiratorytract. Eye and skin protection required. Good general ventilation is normally adequate. Failure toobserver this warning could cause severe personal injury or death.WARNINGCompressed air used for cleaning and drying purposes can create airborne particles that may enter theeyes. Pressure shall not exceed 30 psig and use only with adequate chip guards and chipping goggles.Failure to observer this warning could cause severe personal injury or death.(1) Clean all parts in dry cleaning solvent (Federal Specification P-D-680) and dry thoroughly with filtered compressedair.(2) Scrape carbon deposits from valves and Cylinder head.(3) Visually inspect rocker arms for cracks, corrosion, and excessive wear. Check that oil holes are open.(4) Inspect rocker arm shafts for cracks, deep wear patterns, nicks, and burrs. Remove minor nicks and burrs with oilsoaked crocus cloth. Clean polished shaft in dry cleaning solvent to remove abrasive particles.(5) Inspect blocks for cracks, nicks, burrs, and excessive wear. Remove nicks and burrs from outer surfaces with fineabrasive paper or stone.(6) Inspect springs for cracks, breaks, chaffing and distortion.(7) Inspect push rods for cracks, bends, excessive wear, nicks and scratches. Polish push rods with crocus cloth toremove minor defects.(8) Inspect valve guides for excessive wear. Bore diameter of exhaust valve guide shall be 0.3750 to 0.3790 inch.Bore diameter of intake valve guide shall be 0.3740 to 0. 3780 inch.(9) Replace worn valve guides as follows:(a)(b)(c)(d)Use a 5/8 inch drift with a 3/8 inch pilot and drive out valve guides.Drive replacement valve guides to a depth of 1.3700 to 1.3800 inches blow Cylinder head deckReam bore diameter of intake valve guides to 0.3740 to 0.3750 inch.Ream bore diameter of exhaust valve guides to 0.3750 to 0.3760 inch.(10) Inspect valve springs for cracks, breaks, and distortion. Using a spring tester, compress spring to a length of1.0820 inches. Test load shall be 163 to 180 pounds.(11) Inspect Cylinder head for cracks, breaks, and broken studs. Remove broken studs by center punching, drilling,and using an easy out.(12) Check Cylinder head for warping using a straight edge and feeler gauge. Check lengthwise and between eachCylinder crosswise. Warpage shall not exceed 0.003 inch laterally and 0.005 inch longitudinally. Cylinder headmay be milled to remove minor warpage.3-112 Change 1
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ARMY *TM 9-6115-464-34 AIR FORCE TO-35C2-3 ... - Igor Chudov

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