Helicopter Rotor Blades, Drive Mechanisms and Components: 114D5118-1, 114D5200-14, 114D6200-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114D5118-1 114D51181 | 1615-00-084-8455 | Bracket Assembly, De | The Boeing Company (77272,81205) | ||
| 114D5124-1 114D51241 | 1615-00-966-9376 | Reflector, Oil Sight | The Boeing Company (77272,81205) | ||
| 114D5134-1 114D51341 | 1615-00-012-4597 | Cup Assembly, Oil dr | The Boeing Company (77272,81205) | ||
| 114D5200-11A 114D520011A | 1615-01-326-6133 | Transmission, Mechanical, Helicopt | End Item Identification: CH147 chinook | The Boeing Company (77272) | |
| 114D5200-12 114D520012 | 1615-01-106-5592 | Transmission, Helicopter | III End Item Identification: CH-47 series helicopters General Characteristics Item Description: Consists of 652 parts | The Boeing Company (77272) | |
| 114D5200-13 114D520013 | 1615-01-449-0858 | Transmission, Helicopter | III End Item Identification: CH-47 series helicopter General Characteristics Item Description: Spare parts | The Boeing Company (77272) | |
| 114D5200-14 114D520014 | 1615-01-212-1411 | Transmission, Helicopter | The Boeing Company (77272) | ||
| 114D5200-17 114D520017 | 1615-01-244-4969 | Transmission, Helicopter | III End Item Identification: CH-47 series helicopters General Characteristics Item Description: Consists of 651 parts | The Boeing Company (77272) | |
| 114D5200-2 114D52002 | 1615-00-176-2628 | Transmission, Helico | The Boeing Company (77272) | ||
| 114D5200-8 114D52008 | 1615-01-054-7272 | Transmission, Helicopter | III End Item Identification: CH-47 series helicopters General Characteristics Item Description: Consists of 668 parts | The Boeing Company (77272) | |
| 114D5248-1 114D52481 | 1615-00-050-6199 | Screen Assembly, Transmission | General Characteristics Item Description: Brass, QQ-B-613 comp 2 1/2 hard frame, brass screen 10 X 10 mesh 0.075 in. opening, no. 10 wire 0.028 in. dia, screen silver soldered MIL-B-7883 to frame or silver solder MIL-B-15395 class 7, dim., 5.923 in. nom O/a lg, 4.000 in. nom O/a W, 0.780 in. nom O/a ht, 0.063 in. nom material thk, 2.880 in. nom screen W, 4.188 in. nom screen lg, two mounting holes 0.257 in. nom dia on frame lg top and bottom, 2.500 in. distance between centers on lg, 4.000 in. distance between centers on W, one slot oncenter tab right end 0.380 in. lg by 0.260 in. W, one center guide slot on left end 0.180 in. lg by 0.256 in. W | The Boeing Company (77272) | |
| 114D5249-1 114D52491 | 1615-00-068-6606 | Baffle, Pinion Gear | General Characteristics Item Description: Aluminum alloy QQ-A-250/11 comp 6061-TO, surface treatment anodized per MIL-C-5541, shape, 270 deg conical collar, dim., 7.500 in. base od, 5.080 in. base id, 4.000 in. nom top id, 1.915 in. nom height, 0.063 in. material thickness, four mounting holes 0.218 in. min, 0.225 in. max dia drilled on 7.500 in. bolt circle dia, two holes on left side ofopening 50.0 deg above and below horizontal centerline, two holes adjacent to opening 60.0 deg above and below horizontal centerline, item used on combing transmission | The Boeing Company (77272) | |
| 114D5261-1 114D52611 | 1615-00-068-6618 | Tube, Oil Transfer | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, surface treatment anodized per MIL-C-5541, dim., 0.875 in. min, 0.880 in. max lg, 0.623 in. min, 0.624 in. max od, 0.312 in. min, 0.319 in. max id, 0.150 in. nom od groove W both ends, 0.080 in. nom groove depth, 0.093 in. groove distance from each end, tube used on engine and combingng transmissions | The Boeing Company (77272) | |
| 114D5265-3 114D52653 | 1615-01-095-7478 | Lubricator, Bearing | III End Item Identification: 1520-00-633-6836 General Characteristics Item Description: Part of helicopter transmission assy | The Boeing Company (77272) | |
| 114D5267-1 114D52671 | 1615-00-068-6607 | Deflector, Oil, Pinion Gear | General Characteristics Item Description: Steel, MIL-S-18729 comp 4130, surface treatment black oxide MIL-C-13924, shape, modified l, dim., 4.350 in. nom O/a lg, 1.660 in. nom O/a flat W, 1.050 in. nom O/a bent W, 0.063 in. nom thk, 0.810 in. nom base width, two holes in base 0.218 in. min, 0.224 in. max dia 0.500 in. from front and 0.380 in. from each end W/3.594 in. distance between centers, upright section upwardat 0.810 in. from plate front at 115.0DEG angle, sides of upright section tapered at 45.0 deg angle W/2.250 in. W across top, base front center cut by 3.000 in. radius to 0.250 in. depth | The Boeing Company (77272) | |
| 114D5267-2 114D52672 | 1615-01-114-2155 | Plate, Transmission | The Boeing Company (77272) | ||
| 114D5271-1 114D52711 | 1615-00-176-2624 | Fitting, Oil Transfe | The Boeing Company (77272) | ||
| 114D6071-1 114D60711 | 1615-00-895-9396 | Retainer, Lubricating Oil | General Characteristics Item Description: Aluminum alloy QQ-A-267 comp 2024-T4, anodized MIL-C-5541, dim., 0.560 in.nom O/a lg, 1.253 in. min, 1.254 in. maxod by 0.460 in. nom lg, 1.480 in. nom flange od by 0.100 in. thk, 0.750 in. nom id, 1.100 in. counterbore dia, 0.460IN. counterbore depth, flange side id countersunk 90.0 deg by 0.040 in. deep, right od corner chamfer 45.0 deg by 0.040 in. lg | The Boeing Company (77272,81205) | |
| 114D6200-3 114D62003 | 1615-00-168-5934 | Transmission, Helico | The Boeing Company (77272) | ||
| 114D6200-4 114D62004 | 1615-00-079-1007 | Transmission, Mechanical, Helicopt | End Item Identification: CH-47C, cargo, hel | The Boeing Company (77272) |