Helicopter Rotor Blades, Drive Mechanisms and Components: 114R3490-1, 114R3650-9, 114R6001-20
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114R3490-1 114R34901 | 1615-01-476-0755 | Swashplate, Controllable | Special Features: Ring assembly for swashplate End Item Identification: Chinook helicopter, CH-47 | The Boeing Company (77272) | |
| 114R3505-12 114R350512 | 1615-00-106-7911 | Swashplate, Controllable | The Boeing Company (77272) | ||
| 114R3505-15 114R350515 | 1615-00-179-5908 | Swashplate, Controllable | The Boeing Company (77272) | ||
| 114R3505-18 114R350518 | 1615-01-112-5910 | Swashplate, Control | The Boeing Company (77272) | ||
| 114R3505-20 114R350520 | 1615-01-112-2993 | Swashplate, Control | The Boeing Company (77272) | ||
| 114R3505-7 114R35057 | 1615-00-179-5938 | Swashplate, Controllable | The Boeing Company (77272) | ||
| 114R3505-8 114R35058 | 1615-00-771-1634 | Swashplate, Controllable | The Boeing Company (77272) | ||
| 114R3625-2 114R36252 | 1615-01-438-8726 | Rod End Assembly | III End Item Identification: CH-47 series helicopter General Characteristics Item Description: Rod end upper, pitch varying link, rotary wing hd controls to rotary winghd Special Features: Flight safety critical aircraft part | The Boeing Company (77272) | |
| 114R3625-3 114R36253 | 1615-01-115-3662 | Rod End Assembly | III End Item Identification: CH-47, rotary wing aircraft | The Boeing Company (77272) | |
| 114R3625-4 114R36254 | 1615-01-438-3962 | Rod End Assembly | III End Item Identification: CH-47 series helicopter General Characteristics Item Description: Rod end upper, pitch varying link, rotary wing hd controls to rotary winghd Special Features: Flight safety critical aircraft part | The Boeing Company (77272) | |
| 114R3650-11 114R365011 | 1615-00-003-1153 | Bolt Assembly, Rotary Wing Head | General Characteristics Item Description: Item C/O one bolt, self-retaining and one bushing, sleeve, boltmaterial, alloy steel and cres, 6.984 in. min, 7.029 in. max O/a lg, 0.5608 in. min, 0.5615 in. max largest od, 0.865 in. min, 0.877 in.max W across flats of bolt hex. head, thd designation, 0.5625-18 UNFJ-3A, bushing material, cres, 0.854 in. min, 0.864 in. max O/a lg, 0.5607 in. min, 0.5612 in. max id, 0.756 in. min, 0.759 in. max od of body, 1.000 in. nom odof flange Criticality Code Justification: TEXT | Avibank Mfg. Inc. (84256) The Boeing Company (77272) | |
| 114R3650-3 114R36503 | 1615-00-003-1146 | Bolt Assembly, Rotary Wing Head | III End Item Identification: CH-47 | Avibank Mfg. Inc. (84256) SPS Technologies LLC (56878) The Boeing Company (77272) U S Army Aviation and Missile (81996) | |
| 114R3650-4 114R36504 | 1615-00-004-1010 | Bolt Assembly, Rotary Wing Head | General Characteristics Item Description: Item C/O one bolt, self-retaining and one bushing, sleeve, bolt material, alloy steel and cres, 4.354 in. min, 4.384 in. max O/a lg, 0.6233 in. min, 0.6240 in. max largest od, 0.928 in. min, 0.940 in. max W across flats of bolt hex. head, thd designation, 0.6250-18 UNJF-3A, bushing material, cres, 1.465 in. min, 1.475 in. max O/a lg, 0.6227 in. min, 0.6232 in. max id, 0.880 in. min, 0.883 in. max od of body, 1.188 in. nom od of flange Criticality Code Justification: TEXT | Avibank Mfg. Inc. (84256) The Boeing Company (77272) | |
| 114R3650-6 114R36506 | 1615-00-003-1148 | Bolt Assembly, Rotary Wing Head | III End Item Identification: CH-47 | Avibank Mfg. Inc. (84256) SPS Technologies LLC (56878) The Boeing Company (77272) | |
| 114R3650-6B 114R36506B | 1615-00-003-1148 | Bolt Assembly, Rotary Wing Head | III End Item Identification: CH-47 | The Boeing Company (77272) | |
| 114R3650-7 114R36507 | 1615-00-003-1156 | Bolt Assembly, Rotary Wing Head | General Characteristics Item Description: Item C/O one bolt, self-retaining and one bushing, sleeve, boltmaterial, alloy steel and cres, 3.416 in. min, 3.461 in. max O/a lg, 0.6233 in. min, 0.6240 in. max largest od, 0.928 in. min, 0.940 in. max wacross flats of bolt hex. head, thd designation, 0.6250-18 UNJF-3A, bushingmaterial, cress, 0.803 in. min, 0.813 in. max 0/A lg, 0.6227 in. min, 0.6232 in. max id, 0.786 in. min, 0.789 in. max od of body, 1.062 in. nom odof flange Criticality Code Justification: TEXT | Avibank Mfg. Inc. (84256) SPS Technologies LLC (56878) The Boeing Company (77272) | |
| 114R3650-8 114R36508 | 1615-00-003-1157 | Bolt Assembly, Rotary Wing Head | General Characteristics Item Description: Item C/O one bolt, self-retaining and one bushing, sleeve, boltmaterial, alloy steel and cres, 8.787 in. min, 8.832 in. max O/a lg, 0.4988 in. min, 0.4995 in. max largest od, 0.741 in. min, 0.752 in. max wacross flats of bolt hex. head, thd designation, 0.5000-20 UNJF-3A, bushingmaterial, cres, 0.934 in. min, 0.944 in. max O/a lg, 0.4982 in. min, 0.4987IN. max id, 0.631 in. min, 0.634 in. max od of body, 1.000 in. nom od offlange Criticality Code Justification: TEXT | The Boeing Company (77272) | |
| 114R3650-9 114R36509 | 1615-00-003-1154 | Bolt Assembly, Rotary Wing Head | III End Item Identification: CH-47 | Avibank Mfg. Inc. (84256) SPS Technologies LLC (56878) The Boeing Company (77272) U S Army Aviation and Missile (81996) | |
| 114R6001-19 114R600119 | 1615-00-082-0392 | Cover Assembly, Head | The Boeing Company (77272) | ||
| 114R6001-20 114R600120 | 1615-00-862-3682 | Cover Assembly, Aft | The Boeing Company (77272) |