Helicopter Rotor Blades, Drive Mechanisms and Components: 114D2181-3, 114D2200-8, 114D3204-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114D2181-3 114D21813 | 1615-00-420-7844 | Reflector, Oil Sight | The Boeing Company (77272) | ||
| 114D2200-11 114D220011 | 1615-00-621-1852 | Transmission, Helico | The Boeing Company (77272) | ||
| 114D2200-13 114D220013 | 1615-01-051-2665 | Transmission Assemb | The Boeing Company (77272) | ||
| 114D2200-17 114D220017 | 1615-01-138-2584 | Transmission, Rotor | The Boeing Company (77272) | ||
| 114D2200-18 114D220018 | 1615-01-244-4971 | Transmission, Rotor | The Boeing Company (77272) | ||
| 114D2200-8 114D22008 | 1615-00-006-7695 | Transmission, Helicopter | General Characteristics Item Description: Item C/O approx 1072 parts | The Boeing Company (77272) | |
| 114D2200-9 114D22009 | 1615-00-092-4666 | Transmission, Helico | The Boeing Company (77272) | ||
| 114D3046-1 114D30461 | 1615-00-739-2550 | Shaft Assembly, Sync | The Boeing Company (77272,81205) | ||
| 114D3047-3 114D30473 | 1615-01-094-8468 | Adapter, Shaft, Trans | The Boeing Company (77272) | ||
| 114D3048-7 114D30487 | 1615-00-872-1213 | Shaft Assembly, Sync | The Boeing Company (77272,81205) | ||
| 114D3049-6 114D30496 | 1615-01-094-8474 | Adapter, Splined, Sha | III End Item Identification: CH-47 | The Boeing Company (77272) | |
| 114D3058-1 114D30581 | 1615-00-830-9775 | Support Assembly, Shaft Bearing | General Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ91C-T6, surface treatment dichromate MIL-M-3171 type 3, dim., 1.468 in. nom thk, 4.915 in. nom od, 6.880 in. nom left and right mounting tab lg, 0.380 in. nom tab thk, one hole 0.191 in. dia drilledthru each tab 0.250 in. from end W/6.380 in. C to C distance along lg and 2.800 in. C to C distance along W, 2.890 in. min, 2.915 in. max body id, 3.669 in. min, 3.670 in. max id counterbore by 0.674 in. lg, 3.5433 in. min, 3.5441 in.max liner bore, six equally spaced threaded holes tapped thru W/0.375-16 unc class 3B threads on 4.250 in. dia boltcircle, six no. S246A2-3-1012 studs andsix no. KR6A5-1 key rings installed inthreaded holes, one lubrication fittingno. MS15001-1 installed on od at 15.0 deg | The Boeing Company (77272,81205) | |
| 114D3058-4 114D30584 | 1615-00-074-2142 | Support Assembly | The Boeing Company (77272,81205) | ||
| 114D3058-6 114D30586 | 1615-01-095-7245 | Support Assembly, Sh | The Boeing Company (77272) | ||
| 114D3058-8 114D30588 | 1615-01-208-0710 | Support Assembly, Sh | III End Item Identification: CH-47 rotary wing aircraft | The Boeing Company (77272) | |
| 114D3059-6 114D30596 | 1615-01-094-8466 | Adapter, Shaft, Trans | The Boeing Company (77272) | ||
| 114D3067-3 114D30673 | 1615-00-937-7666 | Adapter Assembly, Drive Shaft | III End Item Identification: Boeing-vertol CH-47 series helicopter | The Boeing Company (77272) | |
| 114D3070-6 114D30706 | 1615-00-872-1212 | Drive Shaft Assembly, Rotary Wing | III End Item Identification: CH47 helicopter, cargo-tr | The Boeing Company (77272,81205) | |
| 114D3200-1 114D32001 | 1615-00-738-8374 | Adapter, Splined | The Boeing Company (77272,81205) | ||
| 114D3204-1 114D32041 | 1615-00-916-2438 | Adapter, Shaft Assem | The Boeing Company (77272) |