Part Details | SHOULDERED SHAFT
3040-01-215-9674 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: 3873577, 387-3577, 3873577, 387-3577, 3873577, 387-3577, 3040-01-215-9674, 01-215-9674, 3040012159674, 012159674
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | SEP 04, 1985 | 01-215-9674 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
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Cross Reference | NSN 3040-01-215-9674
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 387-3577 | 1YQE8 | ALLIANT TECHSYSTEMS OPERATIONS LLCDIV ARMAMENT SYSTEMS DIVISION |
| 387-3577 | 8V613 | BOEING COMPANY, THEDBA BOEING |
| 387-3577 | 02731 | MCDONNELL DOUGLAS HELICOPTER CO INC |
Technical Data | NSN 3040-01-215-9674
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | PLAIN |
| MATERIAL | STEEL COMP 4340 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5000 MIL SPEC SINGLE MATERIAL RESPONSE |
| FIRST END DIAMETER | 24.09 MILLIMETERS NOMINAL |
| END SIMILARITY | NOT IDENTICAL |
| SECOND END STYLE | 2 PLAIN |
| SECOND END DIAMETER | 24.09 MILLIMETERS NOMINAL |
| SECOND END EXTERNAL THREAD LENGTH | 7.0 MILLIMETERS NOMINAL |
| LARGEST STEP DIAMETER | 29.578 MILLIMETERS NOMINAL |
| OVERALL LENGTH | 72.0 MILLIMETERS NOMINAL |
| STEP QUANTITY | 3 |