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

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ARMY TM 9-6115-464-34AIR FORCE 35C2-3-445-2NAVY NAVFAC P-8-624-34(5)(6)(7)(8)(9)(lo)(11)(12)(13)(14)(16)(17)(18)(19)(20)(21)Remove nut (21) Iockwasher (22), and main contactor assemblies (23),Remove retaining ring (24), main contactor operator (31), shim (26), locating bushing (27), contactspring (28), shim (29) and shim (30) from bridge assembly (25).Remove nut (39), Iockwasher (40), terminal washer (41).Remove screw (42), Iockwasher (43), adjusting bushing (44), and actuator& connector assembly(45).Remove nut (35), Iockwasher (36), flatwasher (37), and connector assembly (38).Remove arc chute (32), grommet (33), and arc chute spacer (34) from main base (46)Remove screw (47), Iockwasher (48), auxiliary contact assembly (54) from connector& wireassembly (55).Remove screw (49), Iockwasher (50), Iockwasher (51), cable clamp (52) and auxiliary contactassemably (53 and 54).Remove nut (56), Iockwasher (57), flat washer (58), screw (59) to remove bracket assembly (60).Remove screws (61), Iockwashers (62) and economizing switch (63).Remove screws (64), Iockwasher (65), flat washer (66) and switch bracket (67).Remove nut (68), Iockwasher (69), guide rod (70), nut (71), Iockwasher (72), auxiliary operator (73),and return spring (74).Remove nut (75), Iockwasher (76) and terminal (77).Remove spacer (78), core and rod (79).Remove screw (80), Iockwasher (81) and flatwasher (82).Remove core and frame (83), coil washer (84), coil (85) and end plate (86).NOTEObserve the following precautions before disassembling type B contactor, figure3-101.1. Do not loosen or remove screws (51) or (74). Keeping the relationship of base (37), frame (76)and frames (80) and (81) intact facilitates re-assembly.2. When disassembling movable contact assemblies (items 39,40,41,49,48,45,43, 53), notearrangement of metallic washers (53) on each stud (70) and rod (68) (contacts A, B and C) sothat they can be reassembled in the same order.d. Disassembly Type B.(1) Remove identification plate (1, Figure 3-101).(2) Remove wiring diagram plate (2).(3) Remove screw (3), Iockwasher (4), flatwasher (5) and shield (6).(4) Remove contactor subassy (7).(5) Remove screw (8), Iockwasher (9).(6) Remove screw (10), Iockwasher (11) and screw (12).(7) Remove screws (13), lockwasher (14), from cover (15).(8) Remove Switch-Connector assy (16), Aux switch (17 and 18).3-212
ARMY TM 9-6115-464—34AIR FORCE TO 35C2-3-445-2NAVY NAVFAC P-8-624-34(9) Remove connector (19) and gasket (20).(10) Remove locking spacer (21), Iockwasher (22), flatwasher (23), Chamber (24), and gasket (25).(11) Remove nut (26), lockwasher (27), flatwasher (28), and base assembly (29).(12) Remove flatwasher (32 and 33), nut (34), insert (36) from base (37).(13) Remove nut (39), Iockwasher (40), flatwasher (41), spacer (42), bushings (43 and 44) and bridgeassembly (45).(14) Remove spring (48), bushing (49), arc-chute (50).(15) Remove screw (51), Iockwasher (52), metallic washer (53), insulation (54), and detent (55).(16) Remove solenoid assembly (64), moveable core-rod assembly (65), core assembly (69), frameassemby (73), and micro switch assembly (84).e. Cleaning Inspection and Repair (Type A.)(1)(2)(3)(4)(5)(6)(7)(8)(9)(10)(11)(12)(13)(14)(15)(16)Clean all parts with a clean lint-free cloth moistened with solvent P-D-680 Type Il.Check terminal covers (4) and housing (15) for cracks, breaks, and other damage.Inspect chamber base (19), main base (46), and main contact operator (31) for cracks, breaks, andother damage.Inspect bridge assembly (25) for pitting, corrosion, and other damage.Inspect contact assembly (38) for burns, corrosion, melting and other damage.Inspect auxiliary operator (73) for cracks.Check core and rod (79), core and frame (83), bracket assembly (60), and end plate (86) for cracks,breaks, and other damage.Check coil (85) for swelling of encapsulated materials, burns, and evidence of corrosion. Using anohmmeter, check coil for continuity.Check economizing switch (63) for cracks, corrosion, burns, and evidence of shorting.Check contacts of contact assemblies (53 and 54) for corrosion, pitting, burns, and other damage.Check connector and wire assembly for cracks, stripped or otherwise damaged threads, burned orchaffed insulation, bare wires and other damage. Refer to Appendix A references to solder or repairwire and connector damage.Check all threads for crossing, stripping, peening, and other damage.Discard gaskets (20, 14, and 13) and spacer (78).Repair minor threat damage to parts using thread chaser. Discard hardware with thread damage.Remove minor pitting from contact surfaces of bridge assemblies with fine grit abrasive paper or afine file. Replace bridge assemblies if deeply pitted.Replace any parts found defective or damaged beyond repair.3-213
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Table 1-1. FITS AND TOLERANCES (CON
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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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