Helicopter Rotor Blades, Drive Mechanisms and Components: S14-35-4440, S14-35-5026, S1510-24425

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
S14-35-4440
S14354440
1615-00-520-6298Plug, Main Shaft, TransmissionIII End Item Identification: 1615-00-098-1523
General Characteristics Item Description: Pressed cork per HH-C-561 or HH-C-576, cl 4;BAKED VARNISH;2.000 in. lg by 2.969 in. dia tapered to 2.781 in. dia
Sikorsky Aircraft Corporation (78286)

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S14-35-4500
S14354500
1615-00-632-6932Transmission AssembSikorsky Aircraft Corporation (78286)

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S14-35-5026
S14355026
1615-00-694-7334Bearing Ring, halfGeneral Characteristics Item Description: Alum alloy per AN-A-13;ANODIZE per MIL-A-8625;4.000 in. od by 3.031 in.id by 0.091 in. thk;four 0.193 in. diaholes on 3.500 in. dia bolt circle
Sikorsky Aircraft Corporation (78286)

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S14-35-5062
S14355062
1615-00-388-8729Duct, TransmissionGeneral Characteristics Item Description: C/O weld assy, alum alloy comp 6061 T6, anodize per AN-QQ-A-696;3 DOUBLERS;12 NUTPLATE;41 rivets
Sikorsky Aircraft Corporation (78286)

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S14-35-5081-1
S143550811
1615-00-694-4734Coupling, Female SplSikorsky Aircraft Corporation (78286)

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S14-35-5081-2
S143550812
1615-00-694-4735Coupling, Female SplSikorsky Aircraft Corporation (78286)

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S14-35-7000
S14357000
1615-00-348-9936Gear box Assy, InterSikorsky Aircraft Corporation (78286)

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S1505-2469
S15052469
1615-00-974-6482Tank Cover AssemblySikorsky Aircraft Corporation (78286)

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S1510-21332
S151021332
1615-00-570-1557Bracket Assembly, Main Rotor TorqGeneral Characteristics Item Description: Magnesium alloy QQ-M-40 comp ZK60A, surface treatment MIL-M-3171 type 3 bracket, steel, MIL-S-5000 comp 4140 cond C, cadmium-plated QQ-P-416 liner, dim., 7.940 in. nom ht, 3.245 in. min, 3.255 in. max base lg, 0.625 in. nom base thk, 0.934 in. nom center upright thk, four mounting holes 0.377 in. dia drilled in. base W/1.874 in. C to C distance in. lg and 1.750 in. C to C distance on W, one central aperture 3.312 in. min, 3.313 in. max dia on upright 5.500 in. from bottom, right side of aperture counterbored to 3.700 in. dia by 0.064 in. deep, three equally spaced mounting holes 0.157 in. dia on upright on 4.124 in. bolt circle dia, liner dim., 3.625 in. nom flange od, 0.061 in. nom flange thk, 0.934 in. O/a lg, 3.3145 in. od, 3.125 in. nom id, four equally spaced slots on id 0.375 in. W by 0.078 in. deep
Sikorsky Aircraft Corporation (78286)

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S1510-21336
S151021336
1615-00-509-0881Torque Tube, Subassembly, Main RotGeneral Characteristics Item Description: Steel, MIL-S-5000, composition 4340, condition D
Sikorsky Aircraft Corporation (78286)

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S1510-21428-4
S1510214284
1615-00-707-6863Boot Assembly, MainSikorsky Aircraft Corporation (78286)

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S1510-23003-1
S1510230031
1615-00-968-6346Lock, Main Rotor hubGeneral Characteristics Item Description: Steel, MIL-S-18729, alloy 4130, condition N, protective finish cadmiumplate QQ-P-416, 1.500 in. lg, 0.500 in. W, 0.156 in. thk, 2 holes 0.2055 in. dia, 0.995 in. min 1.005 in. max cto C distance between holes
Sikorsky Aircraft Corporation (78286)

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S1510-23008-1
S1510230081
1615-00-603-8213Inner Spacer, Main RotorGeneral Characteristics Item Description: Steel, MIL-S-5000 comp 4340 cond C, shape, cylinder, flanged, dim., 5.500 in. min, 5.501 in. max O/a lg, 3.500 in. nom flange od, 0.685 in. min, 0.688 in. max flange W, 2.1255 in. min, 2.1260 in. max id, 2.4995 in. min, 2.5000 in. max od, 2.4375-16 class 3A threads on left end od by 0.750 in. lg, four equally spaced keyways on left end threads 0.3125 in. W by 0.0887 in. deep, twelve 0.437 in. dia holes drilled in flange face 0.450 in. deep on 2.825 in. dia bolt circle, item used on main rotor hinge assembly
Sikorsky Aircraft Corporation (78286)

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S1510-23047
S151023047
1615-00-341-0774Retainer, Main RotorIII End Item Identification: CH-54A aircraft
Sikorsky Aircraft Corporation (78286)

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S1510-23082
S151023082
1615-00-339-9580Cap, Main RotorGeneral Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ63 cond hta or comp AZ92 cond hta ORQQ-M-55 comp AZ92 cond hta, surface treatment, type 3 MIL-M-3171, wash PRIMERMIL-C-8514, epoxy polyamide primer MIL-P-23377, dim., 4.000 in. nom od, 4.625IN. min, 4.635 in. max flange od by 0.406 in. nom flange W, 1.125 in. nom O/alg, 4.000 in. nom id on flange side, 2.125 in. nom id left side, 2.249 in. min, 2.251 in. max dia counterbore id by 0.250 in. deep, 0.343 in. nom wallthickness, inside left and outside right corners chamfered 0.625 in. lg by 38DEG located from 2.750 to 4.000 in. dia on od and 2.500 to 4.000 in. dia onid, one hole 0.3281 in. dia drilled thru chamfered side 0.500 in. from topand tapped W/1/8-27 ampt threads, flange od center-grooved 0.1875 in. W BY4.253 in. dia, fluorescent penetrant inspected, MIL-I-6866
Sikorsky Aircraft Corporation (78286)

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S1510-23086
S151023086
1615-00-339-9581Cap, Sleeve and Spindle AssemblyGeneral Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ63-HTA or comp AZ92-HTA, surface treatment dichromate MIL-M-3171 type 3, dim., 6.250 in. N/m flange od, 0.125 in. nom flange W, 0.6875 in. nom O/a W, 6-16 N class 3 external od threads by 0.406 in. lg, one central external extension 0.880 in. dia by 0.500 in. lg W/0.625 in. distance across wrenching flats, fiveinternal webs 0.180 in. thk, item used on main rotor hub
Sikorsky Aircraft Corporation (78286)

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S1510-23212-1
S1510232121
1615-00-991-0309Lock, Main RotorGeneral Characteristics Item Description: Steel MIL-S-6758 comp 4130, cadmium-plated QQ-P-416, dim., shape 72.0 deg splined segment W/three mounting holes, 10.920 in. flange od, 0.253 in. nom flange thk, 2.003 in. nom O/a ht, 8.738 in. min, 8.742 in. max body od, 7.850 in. min, 7.855 in. max body id, internal involute spline data, 159 teeth 0.750 in. lg located 1.250 in. from top of lock, 14.5 deg pressure angle, 7.950 in. pitch dia, 7.835 in. min, 7.850 in. max minor dia, 8.100 in. nom major dia, 20 diametral pitch, three holes 0.298 in. dia drilled thru flange on 10.375 in. dia bolt circle
Sikorsky Aircraft Corporation (78286)

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S1510-23385
S151023385
1615-00-775-7766Eye Bolt AssemblyGeneral Characteristics Item Description: Steel, AMS6260 comp 9310, cadmium-plated QQ-P-416 bearing end, carburized shank, dim., 7.883 in. nom O/a lg, 4.319 in. min, 4.325 in. max shank lg, 1.1253 in. min, 1.1258 in. max shank right endod by 1.250 in. lg, 1.6255 in. min, 1.6258 in. max shank left end od by 1.250 in. lg, 2.187 in. flange od by 0.125 in. thk located 6.228 in. from right end, two flats on flange od W/1.990 in. distance across flats, 0.966-32 ns class 3 threads on right end od by 0.406 in.lg, 0.625 in. right end id by 6.687 in.lg counterbored to 0.6875 in. dia by 0.312 in. lg, eye bolt end 1.249 in. thk, bolt end rounded by 1.093 in. radius, eye drilled W/1.6241 in. dia hole W/one S1510-23389 inner race and one GR-18-RSS mcgill bearing installed in hole, 2.062 in. distance from right flange face to bearing center, one MS15002-1 lubricator installed on bolt end od, item used on main rotor
Sikorsky Aircraft Corporation (78286)

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S1510-24228-1
S1510242281
1615-00-135-2571Trunnion Assy, Main RotorGeneral Characteristics Item Description: Steel, MIL-S-6758 comp 4130 cond C, cadmium-plated QQ-P-416 O/a except threads, dim., 4.483 in. nom O/a lg, 2.124 in. nom center W, 0.881 in. nom left and right arm lg, 1.250 in. nom arm thickness, 1.250-18 nef class 3A external threads on arms by 0.412 in. lg, 1.6249 in. min, 1.6259 in. max trunnion center id, one inner ring no. M1-15 and one bearing no. GR-18RSS mcgill mfr co installed in trunnion center, one lub fitting installed on trunnion od, one keyway thru threads on right arm, 0.187 in. W, 0.144 in. deep, 0.437 in. lg made by 0.500 in. dia cutter, trunnion used on main rotor, rotating star assembly
Sikorsky Aircraft Corporation (78286)

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S1510-24425
S151024425
1615-00-604-2880Washer, Star AssemblSikorsky Aircraft Corporation (78286)

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  • We solve sourcing challenges for S14-35-4440, S14-35-7000, S1510-21336, S1510-21428-4, S1510-23003-1, S1510-23047, S1510-23082, S1510-23212-1, S1510-24228-1, S1510-24425 - NSN parts, hard to find, long lead time and obsolete components.