Part Details | SHOULDERED SHAFT
3040-01-245-9457 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: 5003902, 3040-01-245-9457, 01-245-9457, 3040012459457, 012459457
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | DEC 06, 1986 | 01-245-9457 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 3040-01-245-9457
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5003902 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
Technical Data | NSN 3040-01-245-9457
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6414 ASSN STD SINGLE MATERIAL RESPONSE |
| SURFACE FINISH | 250.0 MICROINCHES |
| FIRST END SPLINE MINOR DIAMETER | 1.1090 INCHES MINIMUM AND 1.1250 INCHES MAXIMUM |
| FIRST END SPLINE MAJOR DIAMETER | 1.3080 INCHES MINIMUM AND 1.3130 INCHES MAXIMUM |
| END SIMILARITY | IDENTICAL |
| LARGEST STEP DIAMETER | 1.235 INCHES MINIMUM AND 1.250 INCHES MAXIMUM |
| OVERALL LENGTH | 3.568 INCHES MINIMUM AND 3.588 INCHES MAXIMUM |
| STEP QUANTITY | 6 |
| SPECIAL FEATURES | HAS EXTERNAL INVOLUTE SPLINES; 20 TEETH,FILLET ROOT SIDE-TYPE,1.250 IN. PITCH DIA,16/32 PITCH DIA,30 DEG PRESSURE ANGLE,1.0825 IN. BASE CIRCLE DIA |
| END ITEM IDENTIFICATION | ACFT,TYPE B-1B |
| FSC APPLICATION DATA | FLIGHT CONTROL |