Part Details | SHOULDERED SHAFT
3040-01-218-2516 A shaft having two or more different diameters (greater than 0.031 inches (0.79 millimeter)) along its length. It must have one or more of the following conditions: a specified surface finish designation in the range 1 to 125 microinches (0.025 to 3.2 micrometers) arithmetical average (AA), machined peripheral flat(s), circular groove(s), keyway(s), splines, threads, or holes. The ends and/or shoulders may be machined to accommodate bearings, couplings, and the like. It is not designed for use in aligning by fitting into corresponding holes of another item. For items used to support rotating members see AXLE(1), SHOULDERED. For items not having any of the above conditions see PIN, SHOULDER, HEADLESS. Excludes SHAFT(1), STRAIGHT; and AXLE(1), STRAIGHT.
Alternate Parts: 5004006, 3040-01-218-2516, 01-218-2516, 3040012182516, 012182516
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | OCT 09, 1985 | 01-218-2516 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 3040-01-218-2516
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5004006 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
Technical Data | NSN 3040-01-218-2516
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP 17-4PH |
| LARGEST STEP DIAMETER | 3.1870 INCHES NOMINAL |
| OVERALL LENGTH | 2.0990 INCHES NOMINAL |
| STEP QUANTITY | 4 |
| SPECIAL FEATURES | SHAFT HOLLOW BOTH ENDS BUT NOT THRU,RELIEFS INTERNAL,ONE GROOVE ON SMALLER DIAMETER |
| END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| FSC APPLICATION DATA | AIRCRAFT ACCESSORY EQUIPMENT |