Part Details | SHOULDERED SHAFT
3040-01-532-6540 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: 68A4509782001, 68A450978-2001, 68A450978, 3040-01-532-6540, 01-532-6540, 3040015326540, 015326540
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | AUG 15, 2005 | 01-532-6540 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
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Cross Reference | NSN 3040-01-532-6540
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68A450978-2001 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 68A450978 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 3040-01-532-6540
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL CORROSION RESISTING |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5643, COND A. MIL SPEC SINGLE MATERIAL RESPONSE |
| SECOND END STYLE | PLAIN |
| SECOND END DIAMETER | 0.2845 INCHES NOMINAL |
| LARGEST STEP DIAMETER | 0.562 INCHES NOMINAL |
| OVERALL LENGTH | 5.285 INCHES NOMINAL |
| STEP QUANTITY | 9 |
| SPECIAL FEATURES | MANUFACTOR'S NAME IS SHAFTINPUT- -NOSE WHEEL STEERING; SHAFT IS 1.115 IN. WIDE AND 0.5624 INCHES HIGH; T.O. 9H2-3-83-3, FIGURE 9-2, INDEX 9; SHAFT HEAD HAS HOLE 0.245 IN. DIA. AROUND INSIDE OF HEAD WHICH IS A CRITICAL SAFETY FEATURE; SHAFT IS COUNTERBORED FROM HEAD 0.375 IN. DIA 1.880 IN. LENGTH THEN 0.250 IN. DIA AN ADDITIONAL 1.120 IN. LENGTH |
| CRITICALITY CODE JUSTIFICATION | AAMFZ$$AFEAT |
| END ITEM IDENTIFICATION | F-15 AIRCRAFT SHIMMY DAMPER - NSN 1620-00-267-1046 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHAFT, INPUT |