Helicopter Rotor Blades, Drive Mechanisms and Components: 114D3204-3, 114D3250-1, 114D5109-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114D3204-3 114D32043 | 1615-01-094-8469 | Adapter, Shaft, Engin | The Boeing Company (77272) | ||
| 114D3207-3 114D32073 | 1615-00-066-0285 | Retainer Assembly, Bearing | General Characteristics Item Description: Steel, MIL-S-5000 comp 4340 cond F, cadmium-plated QQ-P-416 class 2, type 1 body, plastic, polycap inserts, dim., 1.000 in. nom O/a lg, 2.495 in. min, 2.496 in. max flange od, 0.380 in. nom flange W, 1.8125-16 unf class 3A external threads on body od by 0.620 in. lg, 0.515 in. square id, 1.520 in. nom id counterbore by 0.250 in. deep on left side, 8 slots equally spaced on flange face 0.125 in. W, two long lok inserts installed on od threads 90.0 deg apart, item used on engine and sync drive shafts | The Boeing Company (77272,81205) | |
| 114D3241-1 114D32411 | 1615-00-074-9932 | Shaft, Transmission | The Boeing Company (77272) | ||
| 114D3243-1 114D32431 | 1615-00-021-2701 | Adapter, Shaft, Trans | The Boeing Company (77272) | ||
| 114D3245-5 114D32455 | 1615-01-094-8470 | Adapter, Shaft, Trans | The Boeing Company (77272) | ||
| 114D3246-2 114D32462 | 1615-00-016-0999 | Driveshaft Subassem | The Boeing Company (77272) | ||
| 114D3250-1 114D32501 | 1615-00-019-5174 | Shaft Assembly, Rota | The Boeing Company (77272) | ||
| 114D3250-3 114D32503 | 1615-01-096-1025 | Drive Shaft Assembly, Rotary Wing | The Boeing Company (77272) | ||
| 114D3250-5 114D32505 | 1615-01-547-7780 | Drive Shaft Assembly, Rotary Wing | Special Features: Shaft assembly, aft vertical | The Boeing Company (77272) | |
| 114D3251-1 114D32511 | 1615-01-561-7147 | Drive Shaft Assembly, Tail Rotor | III End Item Identification: CH47 chinook Special Features: Threaded, engine to combineer drive shaft | The Boeing Company (77272) | |
| 114D3303-4 114D33034 | 1615-00-472-7292 | Shaft Assembly, fan | The Boeing Company (77272,81205) | ||
| 114D3401-1 114D34011 | 1615-00-021-2723 | Adapter Assembly, Transmission | General Characteristics Item Description: Steel, 114D3040-F2 adapter, steel corrosion resisting laminated plate, dim., 4.800 in. nom O/a lg, 2.842 in. body od, id involute spline data, fillet root side fit, 34 teeth 2.250 in. lg, 16DIAMETRAL pitch, 2.1250 in. pitch dia, 2.3000 in. major dia, 2.0200 in. minor dia, 20.0 deg pressure angle, left end flange 0.562 in. from end, 4.500 in. od by 0.250 in. thk, six holes 0.250 in. dia equally spaced drilled thru on 3.750 in. dia bolt circle, right end triangular flange 4.220 in. arm lg by 1.000 in. arm end W, 0.680 in. flange thk, onehole 0.6250 in. dia drilled thru each arm center on 6.500 in. dia bolt circle, no. 114DS344-1 laminated plate 8.500IN. od, 0.300 in. thk, 4.500 in. id bolted to triangular flange by no. 114D3053-1 bolt, no. MS20365-918 nut and no. 114D3044-1 washer, item used on rotor brake synchronous drive shaft | The Boeing Company (77272) | |
| 114D4042-1 114D40421 | 1615-00-919-4632 | Support, Lubrication | The Boeing Company (77272) | ||
| 114D4043-1 114D40431 | 1615-00-960-3971 | Housing Assembly, dr | The Boeing Company (77272,81205) | ||
| 114D5074-5 114D50745 | 1615-01-317-2309 | Coupling, Drive Shaft | III End Item Identification: Chinook aircraft | The Boeing Company (77272) | |
| 114D5085-1 114D50851 | 1615-00-830-7960 | Yoke, Dephasing Mechanism | General Characteristics Item Description: Steel MIL-S-5000 comp 4340 cond E, surface treatment black oxide coated MIL-F-13924 class 1 grade a, horseshoe shaped, dim., 6.250 in. nom W, 5.780 in. O/a ht, 4.560 in. arm ht, 1.000 in. arm end W, 0.250 in. arm end thk, 1.040 in. min, 1.100 in. max shaft end od, 5.410 in. nom inner distance between arms, arm ends slotted 0.440 in. W by 0.606 in. deep W/slot rounded by 0.220 in. radius, 8.7500 in. min, 8.7510 in. max shaft hole dia by 6.250 in. lg | The Boeing Company (77272,81205) | |
| 114D5087-1 114D50871 | 1615-00-830-7961 | Arm Assembly, Dephas | The Boeing Company (77272,81205) | ||
| 114D5094-3 114D50943 | 1615-00-755-6694 | Cover, Oil Tank, Combining Transmi | General Characteristics Item Description: Magnesium alloy QQ-M-44 comp AZ31-H24, dichromate per MIL-M-3171 type 3, dim., shape, flat topped pyramid, 15.300 in. nom lg, 19.000 in. nom base width, 9.200 in. nom top width, 0.125 in. nom material thk, 24 holes 0.281 in. nom dia drilled thru cover, five along each lg 0.700 in. from edge, three across top, seven across bottom, four equally spaced holes 3.030 in. above and below horizontal centerline and beginning 3.687 in. from base, one center hole 2.250 in. nom dia located 3.687 in. from base on horizontal centerline, six equallyspaced holes 0.281 in. dia on 3.250 in. dia bolt circle around center hole, cover corners rounded by 0.700 in. radius at top and 0.940 in. radius at base | The Boeing Company (77272,81205) | |
| 114D5109-1 114D51091 | 1615-00-957-6676 | Strainer Body, Sediment | Material: Aluminum alloy 2024 body Style Designator: Steam jacketed diverted flow basket strainer W/bolted cover Surface Treatment: Anodize body | The Boeing Company (77272,81205) | |
| 114D5109-2 114D51092 | 1615-00-957-6674 | Strainer Element, Sediment | Material: Copper alloy Style Designator: Cylindrical Filtering Media Design: MESH | The Boeing Company (77272,81205) |