Helicopter Rotor Blades, Drive Mechanisms and Components: S10-10-4300, S10-15-2120-1, S10-15-3002
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| S10-10-4300 S10104300 | 1615-00-187-6947 | Star Assembly, Main | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-4300-1 S101043001 | 1615-00-304-4589 | Star Assembly, Azimuth | General Characteristics Item Description: Assembly of star assembly 1, retainer 2, shield 1 and misc hardware | Sikorsky Aircraft Corporation (78286) | |
| S10-10-4345 S10104345 | 1615-00-187-6950 | Link, Main Rotor Sta | Special Features: Assembly of link lower 1, spacer 3, bearing 4, lubricator 1 | Sikorsky Aircraft Corporation (78286) | |
| S10-10-4349 S10104349 | 1615-00-234-5489 | Link Assembly, Main Rotor | General Characteristics Item Description: Assembly of link lower 1, spacer 3, bearing 4, lubricator 1 | Sikorsky Aircraft Corporation (78286) | |
| S10-10-4351 S10104351 | 1615-00-187-6951 | Link Assembly, Main | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-4400 S10104400 | 1615-00-341-0764 | Star Assy, Main Roto | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-4401-3 S101044013 | 1615-00-693-6915 | Star Assy, Main Roto | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-4401-4 S101044014 | 1615-00-614-0627 | Star Assy, Main Roto | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-4412-1 S101044121 | 1615-00-524-8375 | Star Assembly, Main | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-4430 S10104430 | 1615-00-524-8314 | Retainer, Boot, Main Rotor | III End Item Identification: 1615-00-693-6915 General Characteristics Item Description: Al alloy per QQ-A-327;ANODIZE;7.375 in. lg by 0.875 in. thk by 4.375 in. minor id by 7.187 major id;eight 0.265 in. dia holes equally spaced on 5.000 in. dia bolt circle;four 0.125 in. dia holes 90 deg apart on 5.625 in. dia circle | Sikorsky Aircraft Corporation (78286) | |
| S10-10-5340 S10105340 | 1615-00-397-1379 | Pivot, Main Rotor Hinge | General Characteristics Item Description: Steel per AN-S-684, cond C, comp 4130;CADMIUM plate per AN-P-61 except 0.500 in. dia hole;heat treat rockwell C33 to C38;2.344 in. lg by 1.500 in. wd by 1.312 in. thk O/A;0.4687 in. dia pilot hole one end W/0.250 in. dia cross drill to pilot HOLE;0.500 in. dia hole other end W/cross drill to hole 0.250-28 nf 2B thd | Sikorsky Aircraft Corporation (78286) | |
| S10-10-5341 S10105341 | 1615-00-397-1380 | Plunger, Main Rotor | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-5380-1 S101053801 | 1615-00-563-2717 | Flap Assy | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-5380-2 S101053802 | 1615-00-073-7364 | Flap Assy | Sikorsky Aircraft Corporation (78286) | ||
| S10-10-6311 S10106311 | 1615-00-187-6959 | Yoke Assembly, Main Rotor | General Characteristics Item Description: Assembly of yoke 1, bushing 3, lubrication fitting 1, drive screw 1; 2.497 in. min and 2.507 in. max l | Sikorsky Aircraft Corporation (78286) | |
| S10-10-6442-4 S101064424 | 1615-00-301-8407 | Reservoir, Dampener | Sikorsky Aircraft Corporation (78286) | ||
| S10-15-2120-1 S101521201 | 1615-00-211-1146 | Blade, Rotary Wing | III End Item Identification: H-19 helicopter | Sikorsky Aircraft Corporation (78286) | |
| S10-15-2120-6 S101521206 | 1615-00-632-5805 | Blade, Rotary Wing | III End Item Identification: H-19 helicopter Special Features: Fsc application:helicopter drive component;reference data and literature:t.O. 3R1-3-2-3 | Sikorsky Aircraft Corporation (78286) | |
| S10-15-2134 S10152134 | 1615-00-184-9899 | Tip Assembly, Tail Rudder | General Characteristics Item Description: Aluminum alloy; 2.000 in. min AND2.500 in. max W, 6.371 in. l | Sikorsky Aircraft Corporation (78286) | |
| S10-15-3002 S10153002 | 1615-00-184-9901 | Sleeve, Tail Rotor H | Sikorsky Aircraft Corporation (78286) |