NSN 1560-00-305-4185 00-305-4185, 003054185
Product Details | BELL CRANK
1560-00-305-4185 An item in the form of two arms at an angle, having its fulcrum at the apex of the angle, and used to provide a means of changing the direction or varying the intensity of a pushing or pulling force. See also ARM (as modified); and LEVER (as modified).20411900057Specialized Test and Handling Equipment, Nuclear Ordnance11950030Miscellaneous Nuclear Ordnance16800049Miscellaneous Aircraft Accessories and Components30400042Miscellaneous Power Transmission Equipment
Part Alternates: 1560-00-305-4185, 00-305-4185, 1560003054185, 003054185
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 00-305-4185 | 22321 ( BELL CRANK ) |
Cross Reference | NSN 1560-00-305-4185
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| S1640-61305-3 | 78286 | SIKORSKY AIRCRAFT CORPORATION |
Request a Quote
What Our Customers Say
Compare
NSNs for Compare ( up to 4 ): Add 1560-00-305-4185
Related Products | NSN 1560-00-305-4185
Technical Data | NSN 1560-00-305-4185
| Characteristic | Specifications |
|---|---|
| MATERIAL | MAGNESIUM ALLOY |
| BORE LENGTH | 2.375 INCHES MINIMUM AND 2.380 INCHES MAXIMUM |
| BORE DIAMETER | 2.062 INCHES NOMINAL |
| COUNTERBORE DIAMETER | 2.187 INCHES MINIMUM AND 2.188 INCHES MAXIMUM |
| COUNTERBORE DEPTH | 0.375 INCHES MINIMUM AND 0.380 INCHES MAXIMUM |
| MANUFACTURERS CODE | 78286 |
| DESIGN CONTROL REFERENCE | S1640-61305 |
Restrictions/Controls & Freight Information | NSN 1560-00-305-4185
| Category | Code | Description |
|---|---|---|
| Hazardous Material Indicator Code | P | There is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||



