Part Details | SHOULDERED SHAFT
3040-01-015-1256 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: 6638521, 66-3852-1, 6638521, 66-3852-1, 3040-01-015-1256, 01-015-1256, 3040010151256, 010151256
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | JAN 15, 1976 | 01-015-1256 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 3040-01-015-1256
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 66-3852-1 | 8L185 | STL ENTERPRISES INC.DBA INTERNATIONAL AIRCRAFT SUPPLY |
| 66-3852-1 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 3040-01-015-1256
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL CORROSION RESISTING |
| SURFACE FINISH | 63.0 MICROINCHES |
| FIRST END DIAMETER | 2.2500 INCHES NOMINAL |
| FIRST END HOLE DIAMETER | 0.1260 INCHES NOMINAL |
| FIRST END DISTANCE FROM HOLE CENTER TO END | 0.1800 INCHES NOMINAL |
| END SIMILARITY | NOT IDENTICAL |
| LARGEST STEP DIAMETER | 2.870 INCHES NOMINAL |
| OVERALL LENGTH | 5.150 INCHES NOMINAL |
| STEP QUANTITY | 3 |
| SPECIAL FEATURES | FLANGED SECOND END |
| END ITEM IDENTIFICATION | KC-135, EC-135, RC-135 AND C-135 AIRCRAFT |