Part Details | SHOULDERED SHAFT
3040-01-258-5456 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: 9340M55P02, 9340M55P02, 9340M55P02, 9340M55P02, 9340M55P02 REV J, 9340M55P02, 42411165, 42411-165, 3040-01-258-5456, 01-258-5456, 3040012585456, 012585456
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | JUL 03, 1987 | 01-258-5456 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
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Cross Reference | NSN 3040-01-258-5456
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9340M55P02 | 91514 | AIRCRAFT GEAR CORP |
| 9340M55P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9340M55P02 | 03350 | GENERAL ELECTRIC COMPANYDBA GE STRUCTURED SERVICES DIV |
| 9340M55P02 | 57152 | TRIUMPH GEAR SYSTEMS - MACOMB, INC. |
| 9340M55P02 REV J | 82402 | TRIUMPH GEAR SYSTEMS, INC.DBA TRIUMPH GEAR SYSTEMS- PARK CITY |
| 9340M55P02 | 82402 | TRIUMPH GEAR SYSTEMS, INC.DBA TRIUMPH GEAR SYSTEMS- PARK CITY |
| 42411-165 | 82402 | TRIUMPH GEAR SYSTEMS, INC.DBA TRIUMPH GEAR SYSTEMS- PARK CITY |
Technical Data | NSN 3040-01-258-5456
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | FLATTED |
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS6265 ASSN STD ALL MATERIAL RESPONSES |
| FIRST END DIAMETER | 0.2500 INCHES NOMINAL |
| FIRST END EXTERNAL THREAD LENGTH | 0.5000 INCHES NOMINAL |
| FIRST END INTERNAL THREAD LENGTH | 0.1800 INCHES NOMINAL |
| END SIMILARITY | NOT IDENTICAL |
| SECOND END STYLE | PLAIN |
| SECOND END DIAMETER | 1.1819 INCHES NOMINAL |
| STEP QUANTITY | 18 |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | USED ON ACC. GEARBOX FOR F110 ENG; AIRCRAFT F-16 |