Part Details | SHOULDERED SHAFT
3040-01-073-5891 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: 11508040, 11508040, 3040-01-073-5891, 01-073-5891, 3040010735891, 010735891
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | MAR 17, 1979 | 01-073-5891 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
PLAIN
PLAIN
Cross Reference | NSN 3040-01-073-5891
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11508040 | 82577 | RAYTHEON COMPANYDBA RAYTHEON |
| 11508040 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 3040-01-073-5891
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | PLAIN |
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 6,T4 OR T351 FED SPEC SINGLE MATERIAL RESPONSE |
| FIRST END DIAMETER | 0.0920 INCHES MINIMUM AND 0.0930 INCHES MAXIMUM |
| END SIMILARITY | IDENTICAL |
| LARGEST STEP DIAMETER | 0.155 INCHES NOMINAL |
| OVERALL LENGTH | 1.420 INCHES NOMINAL |
| STEP QUANTITY | 3 |