Helicopter Rotor Blades, Drive Mechanisms and Components: S6110-26100-001, S6110-26103-101, S6110-26410-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| S6110-26100-001 S611026100001 | 1615-00-826-5514 | Valve Assembly, Main | Bridgestone Americas Tire Operations (22337) | ||
| S6110-26100-1 S6110261001 | 1615-00-826-5514 | Valve Assembly, Main | Sikorsky Aircraft Corporation (78286) | ||
| S6110-26101 S611026101 | 1615-00-948-0472 | Valve, Rotary Wing | Sikorsky Aircraft Corporation (78286) | ||
| S6110-26101 S611026101 | 1615-01-502-4921 | Valve Assembly, Damper | III End Item Identification: EH-60A Special Features: Material spec for valves AMS5355 III Part Name Assigned By Controlling Agency: Valve assembly, diff.check damper-rotary wing head | Sikorsky Aircraft Corporation (78286) | |
| S6110-26101-000 S611026101000 | 1615-01-078-5719 | Valve Assy, Damper | Sikorsky Aircraft Corporation (78286) | ||
| S6110-26101-041 S611026101041 | 1615-01-502-4921 | Valve Assembly, Damper | III End Item Identification: EH-60A Special Features: Material spec for valves AMS5355 III Part Name Assigned By Controlling Agency: Valve assembly, diff.check damper-rotary wing head | Sikorsky Aircraft Corporation (78286) | |
| S6110-26103-101 S611026103101 | 1615-01-100-2870 | Valve-Stemmed, Yoke | General Characteristics Item Description: Steel AMS5355, passivated, 1.163 in. lg, 0.344 in. W, 0.344 in. H | Sikorsky Aircraft Corporation (78286) | |
| S6110-26104-101 S611026104101 | 1615-01-100-2871 | Valve, Yoke Assembly | III End Item Identification: Aircraft model CH-53D General Characteristics Item Description: Cres, AMS5355, 17-4PH; alt AMS5643, 17-4PH | Sikorsky Aircraft Corporation (78286) | |
| S6110-26400-010 S611026400010 | 1615-00-124-4790 | Damper Assembly, Rot | Sikorsky Aircraft Corporation (78286) | ||
| S6110-26400-042 S611026400042 | 1615-01-282-3541 | Damper Assembly Rotor | III End Item Identification: Acft model SH-3H | Sikorsky Aircraft Corporation (78286) | |
| S6110-26400-043 S611026400043 | 1615-01-260-9195 | Damper Assembly, Rotor | III End Item Identification: H-3H helicopter | Sikorsky Aircraft Corporation (78286) | |
| S6110-26400-044 S611026400044 | 1615-01-258-2505 | Damper Assembly, Rot | III End Item Identification: Aircraft model SH-3H | Sikorsky Aircraft Corporation (78286) | |
| S6110-26401-2 S6110264012 | 1615-01-039-3254 | Cylinder Assembly | End Item Identification: Helicopter, H-3, damper assembly | Sikorsky Aircraft Corporation (78286) | |
| S6110-26402-2 S6110264022 | 1615-00-124-4771 | Head, Rotary Wing | III End Item Identification: 1615-00-124-4787 General Characteristics Item Description: Al alloy;anodize per MIL-A-8625;90 aa microinches surface ROUGH;4.750 in. dia by 1.500 in. thk O/a;seven 0.328 in. dia holes on the basis of eight equally spaced spotface 0.750 in. dia by 0.062 radius on a 4.188 in. dia bc;one 0.328 in. dia hole 0.970 in. from CENTER;2.150 in. dia minor bore by 2.440 in. dia major bore | Sikorsky Aircraft Corporation (78286) | |
| S6110-26403-041 S611026403041 | 1615-01-309-1910 | Cylinder and Head Assembly | III End Item Identification: Aircraft model H-3 | Sikorsky Aircraft Corporation (78286) | |
| S6110-26403-2 S6110264032 | 1615-00-124-4787 | Cylinder and Head Assembly, Dampe | General Characteristics Item Description: C/O 1 CYLINDER;1 HEAD;3 BUSHING;1PLUG;1 STUDS;1 hyd STUD;4 LOCKRINGS;1 packing PREFORM;2 INSERT;4 ea screw, nut, washer | Sikorsky Aircraft Corporation (78286) | |
| S6110-26405-001 S611026405001 | 1615-00-124-4779 | Lug, Mounting, Upper Damper | General Characteristics Item Description: Steel ty 4340 per MIL-S-5000;CADMIUM cl 2, ty 3 per QQ-P-416;SURFACE rough 90AA microinches;heat treat RC34 minto RC38 MAX.;2.500 in. lg approx by 1.470 in. hgt O/A;0.470 in. hgt head W/0.090 in. lg by 45.0 deg chamfer, four 0.391 in. dia holes and two 0.380 in. dia holes, one 0.213 in. dia hole by 0.250-28 UNF-3B thd by 0.300 in. deep in CENTER;1.000 in. hgt body by 1.492 in.wd W/0.750 in. hgt by 0.750 in. wd bore | Sikorsky Aircraft Corporation (78286) | |
| S6110-26407-7 S6110264077 | 1615-00-124-4770 | Shaft, Guide, Damper | General Characteristics Item Description: Steel per MIL-S-5000, cond c;before finish machining heat treat to 150, 000 psi min. T.s. rockwell C 34-38 per MIL-H-6875;O/A dim 8.250 in. LG;1.436 in. dia. one end;other end 1 125-12 UNF-3A thd. per MIL-S-7742 | Sikorsky Aircraft Corporation (78286) | |
| S6110-26409-102 S611026409102 | 1615-01-010-3749 | Spacer, Damper Mounting Rotary Wi | III End Item Identification: Acft model HH3F General Characteristics Item Description: Make iaw spec QQ-A-250-4, material 2024-T351, 0.475 thk, make iaw sikorsky dwg S6110-26409 | Sikorsky Aircraft Corporation (78286) | |
| S6110-26410-001 S611026410001 | 1615-00-124-4777 | Dowel Plate, Mounting | General Characteristics Item Description: Steel ty 4130 per MIL-S-6758;CADMIUM plate per QQ-P-416;HEAT treat to rockwell C34 min to C38 max.;machine surface 90 microinches AA;4.794 in. lg BY0.125 in. thk plate W/two 0.453 in. dia holes located on ea end and one 0.213 in. dia by 0.380 in. deep, tap | Bell Helicopter Textron Inc. (97499) | |
| S6110-26410-1 S6110264101 | 1615-00-124-4777 | Dowel Plate, Mounting | General Characteristics Item Description: Steel ty 4130 per MIL-S-6758;CADMIUM plate per QQ-P-416;HEAT treat to rockwell C34 min to C38 max.;machine surface 90 microinches AA;4.794 in. lg BY0.125 in. thk plate W/two 0.453 in. dia holes located on ea end and one 0.213 in. dia by 0.380 in. deep, tap | Sikorsky Aircraft Corporation (78286) |