Part Details | SHOULDERED SHAFT
3040-01-125-8362 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: D0134481, D013448-1, D0134481, D013448-1, 1534AS427, 1534AS427, 1534AS427, 1534AS427, 10106824, 1534AS427, 1534AS427, 3040-01-125-8362, 01-125-8362, 3040011258362, 011258362
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | FEB 01, 1982 | 01-125-8362 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
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Cross Reference | NSN 3040-01-125-8362
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| D013448-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
| D013448-1 | 8V613 | BOEING COMPANY, THEDBA BOEING |
| 1534AS427 | 31645 | GOODRICH CORPORATIONDBA GOODRICH INTERIORS CARGO SYSTEMS |
| 1534AS427 | 05DN8 | KLUNE INDUSTRIES, INC.DIV KLUNE INDUSTRIES |
| 1534AS427 | 32067 | MARVIN ENGINEERING CO., INC.DBA MARVIN GROUP, THE |
| 1534AS427 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
| 10106824 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| 1534AS427 | 072E5 | RAYTHEON COMPANYDBA RAYTHEON |
| 1534AS427 | 09245 | SOLO ENTERPRISE CORP.DBA SOLO GOLF |
Technical Data | NSN 3040-01-125-8362
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | 7 PLAIN |
| MATERIAL | STEEL CORROSION RESISTING |
| SURFACE FINISH | 125.0 MICROINCHES |
| FIRST END DIAMETER | 0.4950 INCHES MINIMUM AND 0.4980 INCHES MAXIMUM |
| FIRST END WIDTH ACROSS FLATS | 0.432 INCHES MINIMUM AND 0.437 INCHES MAXIMUM |
| FIRST END STEP LENGTH | 0.963 INCHES NOMINAL |
| END SIMILARITY | IDENTICAL |
| LARGEST STEP DIAMETER | 0.495 INCHES MINIMUM AND 0.498 INCHES MAXIMUM |
| OVERALL LENGTH | 3.401 INCHES NOMINAL |
| STEP QUANTITY | 3 |
| SPECIAL FEATURES | FLIGHT SAFETY CRITICAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FSC APPLICATION DATA | RACK,BOMB,EJECTOR AIRCRAFT,BRU-32A |