Helicopter Rotor Blades, Drive Mechanisms and Components: 114DS221-2, 114E5888-13, 114H6813-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114DS221-2 114DS2212 | 1615-01-247-8469 | Screen, Lubricator | The Boeing Company (77272) | ||
| 114DS221-3 114DS2213 | 1615-01-246-6787 | Screen, Lubricator | The Boeing Company (77272) | ||
| 114DS221-5 114DS2215 | 1615-01-247-8474 | Screen, Lubricator | The Boeing Company (77272) | ||
| 114DS221-8 114DS2218 | 1615-01-247-8470 | Screen, Lubricator | III End Item Identification: CH-47, screen information, "a"dia 4.824, "B".280, "C".070, "D".210, "E"4.834, lubricator part NO(REF)114D5265 & 114D6249 | The Boeing Company (77272) | |
| 114DS344-1 114DS3441 | 1615-01-567-7013 | Plate Assembly, Driv | The Boeing Company (77272) | ||
| 114DS345-3 114DS3453 | 1615-00-856-1793 | Plate, fan Drive Ass | The Boeing Company (77272,81205) | ||
| 114DS440-1 114DS4401 | 1615-00-866-5999 | Cooler, Fluid, Transm | The Boeing Company (77272) | ||
| 114DS441-1 114DS4411 | 1615-00-866-5997 | Cooler, Oil, Transmis | The Boeing Company (77272) | ||
| 114DS547-4 114DS5474 | 1615-00-996-3902 | Pump Assembly, Oil, C | The Boeing Company (77272,81205) | ||
| 114DS559-3 114DS5593 | 1615-00-849-4379 | Filter and Relief V | The Boeing Company (77272) | ||
| 114DS562-3 114DS5623 | 1615-00-691-6370 | Valve, Check, Oil Pre | The Boeing Company (77272,81205) | ||
| 114DS577-2 114DS5772 | 1615-01-005-2245 | Screen Assembly | The Boeing Company (77272) | ||
| 114DS672-1 114DS6721 | 1615-01-219-8665 | Clutch Assembly, Centrifugal, Airc | The Boeing Company (77272) | ||
| 114DS672-1 114DS6721 | 1615-01-330-4855 | Clutch Assembly, Centrifugal, Aircraft | The Boeing Company (77272) | ||
| 114DS672-2 114DS6722 | 1615-01-219-8666 | Clutch Assembly, Centrifugal, Airc | The Boeing Company (77272) | ||
| 114DS672-2 114DS6722 | 1615-01-346-0978 | Clutch Assembly, Centrifugal, Aircraft | The Boeing Company (77272) | ||
| 114E2052-14 114E205214 | 1615-00-955-9575 | Shroud Assembly, Lef | The Boeing Company (77272,81205) | ||
| 114E2052-15 114E205215 | 1615-00-955-9576 | Shroud Assembly, rig | The Boeing Company (77272,81205) | ||
| 114E5888-13 114E588813 | 1615-01-565-8693 | Transmission, Mechanical, Helicopt | End Item Identification: Chinook CH-47D helicopters | The Boeing Company (77272) | |
| 114G1018-20 114G101820 | 1615-01-045-7882 | Skid, Rotor Blade | General Characteristics Item Description: HARDWOOD;21.750 in. nom lg, 3.600 in. nom W, 3.620 in. nom H III Fsc Application Data: Shipping and storage, container, rotor blade | The Boeing Company (77272) | |
| 114H6800-7 114H68007 | 1615-01-301-3487 | Absorber | The Boeing Company (77272) | ||
| 114H6813-1 114H68131 | 1615-00-070-1137 | Baffle Assembly, Shock Absorber | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, comp 2024-T3 or T4, surface finish, anodized per MIL-A-8625 type 1, no. 16437 gray, rubber MIL-P-25732, gasket, aluminum alloy, QQ-A-225/6, comp 2024-T4, pin, dim., 3.110 in. dia, 0.032 in. nom material thk, one hole 0.082 in. dia drilled thru plate 1.437 in. left of vertical centerline on horizontal centerline, one hole 0.156 in. dia drilled thru plate 1.220 in. left of vertical centerline, 3.120 in. gasket od, 2.620 in. id, 0.060 in. material thk, one slot 0.140 in. nom width cut thru left of vertical centerline on the horizontal centerline, 0.160 in. nom pin lg O/a, 0.123 in. pin od by 0.115 in. lg, 0.081 in. nom od by 0.045 in. lg pin right end, gasket is bonded to plate, baffle assembly used on dampener flutter, direct action | The Boeing Company (77272) |