NSN 3040-00-272-2411
Part Details | SHOULDERED SHAFT
3040-00-272-2411 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: 1202512101, 1202512-101, 3040-00-272-2411, 00-272-2411, 3040002722411, 002722411
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | JUL 22, 1973 | 00-272-2411 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
PLAIN
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Cross Reference | NSN 3040-00-272-2411
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1202512-101 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 3040-00-272-2411
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | PLAIN |
| MATERIAL | ALUMINUM |
| SURFACE FINISH | 125.0 MICROINCHES |
| FIRST END DIAMETER | 1.0615 INCHES NOMINAL |
| END SIMILARITY | NOT IDENTICAL |
| SECOND END STYLE | 8 PLAIN |
| SECOND END DIAMETER | 1.4955 INCHES NOMINAL |
| SECOND END SPLINE LENGTH | 1.350 INCHES NOMINAL |
| SECOND END SPLINE MINOR DIAMETER | 1.3070 INCHES NOMINAL |
| SECOND END SPLINE MAJOR DIAMETER | 1.4955 INCHES NOMINAL |
| SECOND END PITCH DIAMETER | 1.4012 INCHES NOMINAL |
| SECOND END PRESSURE ANGLE | 30.000 DEGREES NOMINAL |
| SECOND END SPLINE QUANTITY | 23 |
| LARGEST STEP DIAMETER | 1.500 INCHES NOMINAL |
| OVERALL LENGTH | 8.940 INCHES NOMINAL |
| STEP QUANTITY | 8 |
| FSC APPLICATION DATA | S-3A AIRCRAFT |