Part Details | SHOULDERED SHAFT
3040-01-188-6521 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: 1534AS431, D014189501, D014189-501, D014189501, D014189-501, 1534AS431, 1534AS431, 1534AS431, 1534AS431, 10104454, 1534AS431, 1534AS431, D014189501, D014189-501, 3040-01-188-6521, 01-188-6521, 3040011886521, 011886521
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | SEP 07, 1984 | 01-188-6521 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
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Cross Reference | NSN 3040-01-188-6521
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1534AS431 | 7D752 | BENDON GEAR & MACHINE INC |
| D014189-501 | 88277 | BOEING COMPANY, THEDBA BOEING |
| D014189-501 | 8V613 | BOEING COMPANY, THEDBA BOEING |
| 1534AS431 | 31645 | GOODRICH CORPORATIONDBA GOODRICH INTERIORS CARGO SYSTEMS |
| 1534AS431 | 05DN8 | KLUNE INDUSTRIES, INC.DIV KLUNE INDUSTRIES |
| 1534AS431 | 32067 | MARVIN ENGINEERING CO., INC.DBA MARVIN GROUP, THE |
| 1534AS431 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
| 10104454 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| 1534AS431 | 072E5 | RAYTHEON COMPANYDBA RAYTHEON |
| 1534AS431 | 09245 | SOLO ENTERPRISE CORP.DBA SOLO GOLF |
| D014189-501 | 57928 | SONIC INDUSTRIES INC. |
Technical Data | NSN 3040-01-188-6521
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | 2 PLAIN |
| MATERIAL | NICKEL ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE |
| FIRST END DIAMETER | 0.1900 INCHES NOMINAL |
| FIRST END EXTERNAL THREAD LENGTH | 0.378 INCHES NOMINAL |
| END SIMILARITY | NOT IDENTICAL |
| SECOND END STYLE | 2 PLAIN |
| SECOND END DIAMETER | 0.3750 INCHES NOMINAL |
| SECOND END EXTERNAL THREAD LENGTH | 0.283 INCHES NOMINAL |
| LARGEST STEP DIAMETER | 0.781 INCHES NOMINAL |
| OVERALL LENGTH | 4.239 INCHES NOMINAL |
| STEP QUANTITY | 8 |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL. |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | F/A-18 HORNET AIRCRAFT. |
| FSC APPLICATION DATA | RACK,BOMB EJECTOR AIRCRAFT BRU-32A |