Airframe Structural Components: 114C1142-2, 114C1161-1, 114C3317-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114C1142-2 114C11422 | 1560-00-830-4328 | Pedal Post, Right hand | General Characteristics Item Description: Magnesium alloy, QQ-M-40 | The Boeing Company (77272,81205) | |
| 114C1161-1 114C11611 | 1560-00-830-4336 | Bell Crank | Bore Diameter: 0.320 inches minimum and 0.360 inches maximum Bore Length: 2.340 inches minimum and 2.390 inches maximum Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 2.980 inches minimum 1ST end and 3.000 inches maximum 1ST end | The Boeing Company (77272,81205) | |
| 114C1183-1 114C11831 | 1560-00-886-3370 | Adapter, Control Stick | General Characteristics Item Description: Magnesium alloy, QQ-M-40, 3.480 in. lg | The Boeing Company (77272,81205) | |
| 114C1183-3 114C11833 | 1560-01-568-5096 | Adapter, Control Stick | III End Item Identification: 1520-01-457-5179 Overall Length: 2.000 inches nominal III Part Name Assigned BY Controlling Agency: End rod assembly | The Boeing Company (77272) | |
| 114C1224-23 114C122423 | 1560-00-919-9989 | Parts Kitxstiffener | The Boeing Company (77272,81205) | ||
| 114C1246-1 114C12461 | 1560-00-886-1357 | Piston | The Boeing Company (77272,81205) | ||
| 114C1267-1 114C12671 | 1560-00-794-2617 | Connector rod Assembly | III End Item Identification: Aircraft model H-47 General Characteristics Item Description: 12.580 in. lg | The Boeing Company (77272,81205) | |
| 114C1280-5 114C12805 | 1560-00-678-1186 | Bracket, Spring Supp | The Boeing Company (77272) | ||
| 114C2510-1 114C25101 | 1560-00-980-7326 | Bell Crank | The Boeing Company (77272,81205) | ||
| 114C2512-1 114C25121 | 1560-00-980-7322 | Bell Crank | The Boeing Company (77272,81205) | ||
| 114C2512-4 114C25124 | 1560-00-168-5996 | Bell Crank | Bore Diameter: 0.485 inches minimum and 0.515 inches maximum Bore Length: 1.960 inches nominal Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 6.000 inches nominal 1ST end | The Boeing Company (77272) | |
| 114C2513-4 114C25134 | 1560-00-168-5995 | Bell Crank | Bore Diameter: 0.377 inches minimum and 0.427 inches maximum Bore Length: 1.960 inches nominal Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 6.000 inches nominal 2ND end | The Boeing Company (77272) | |
| 114C2514-4 114C25144 | 1560-00-963-1075 | Bell Crank | The Boeing Company (77272,81205) | ||
| 114C2515-1 114C25151 | 1560-00-987-1410 | Bell Crank | The Boeing Company (77272,81205) | ||
| 114C3042-9 114C30429 | 1560-00-854-9060 | Yoke, Longitudinal Cyclic Support | General Characteristics Item Description: Magnesium alloy QQ-M-40 composition ZK60A condition T5 | The Boeing Company (77272) | |
| 114C3044-2 114C30442 | 1560-00-868-8468 | Shaft, Support | Ruscomb Tool & Machine Co. Inc. (07952) The Boeing Company (77272,81205) | ||
| 114C3310-21 114C331021 | 1560-00-834-2202 | Bell Crank | Bore Diameter: 1.812 inches minimum and 1.814 inches maximum Bore Length: 3.650 inches minimum and 3.670 inches maximum Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 10.990 inches minimum 2ND end and 11.010 inches maximum 2ND end | The Boeing Company (77272) | |
| 114C3312-1 114C33121 | 1560-00-789-4993 | Bell Crank | Counterbore Diameter: 1.623 inches minimum and 1.624 inches maximum Counterbore Depth: 0.380 inches nominal Bore Diameter: 1.450 inches nominal | The Boeing Company (77272,81205) | |
| 114C3314-1 114C33141 | 1560-00-010-5509 | Shaft, Mixing Linkag | Apex Manufacturing Company Inc. (2V343) The Boeing Company (77272) | ||
| 114C3317-1 114C33171 | 1560-00-789-7785 | Bell Crank | Bore Diameter: 2.373 inches nominal | The Boeing Company (77272,81205) |