Part Details | SHOULDERED SHAFT
3040-01-127-1446 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: 13040268, 13040268, 3040-01-127-1446, 01-127-1446, 3040011271446, 011271446
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | FEB 24, 1982 | 01-127-1446 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
PLAIN
TAPERED WITH FLAT
PLAIN
TAPERED WITH FLAT
Cross Reference | NSN 3040-01-127-1446
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 13040268 | 1L007 | SPECIAL PROJECTS INC |
| 13040268 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 3040-01-127-1446
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | PLAIN |
| MATERIAL | ALUMINUM ALLOY 6061 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 8 TEM T6 FED SPEC SINGLE MATERIAL RESPONSE |
| FIRST END DIAMETER | 0.1750 INCHES MAXIMUM |
| END SIMILARITY | NOT IDENTICAL |
| SECOND END STYLE | 0 TAPERED WITH FLAT |
| SECOND END DIAMETER | 0.1871 INCHES MAXIMUM |
| SECOND END BEARING SEAT LENGTH | 2.970 INCHES MAXIMUM |
| SECOND END BEARING SEAT DIAMETER | 0.2500 INCHES MAXIMUM |
| SECOND END DISTANCE FROM BEARING SEAT TO END | 0.200 INCHES MAXIMUM |
| LARGEST STEP DIAMETER | 0.187 INCHES NOMINAL |
| OVERALL LENGTH | 4.235 INCHES MAXIMUM |
| STEP QUANTITY | 4 |