Part Details | SHOULDERED SHAFT
3040-01-100-2729 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: 6510511505103, 65105-11505-103, 6510511505103, 65105-11505-103, 6510511505103, 65105-11505-103, 3040-01-100-2729, 01-100-2729, 3040011002729, 011002729
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | SEP 01, 1980 | 01-100-2729 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
PLAIN
TAPERED WITH FLAT
PLAIN
TAPERED WITH FLAT
Cross Reference | NSN 3040-01-100-2729
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 65105-11505-103 | 5K840 | AEREX MANUFACTURING INC. |
| 65105-11505-103 | 2A269 | MACOR INC |
| 65105-11505-103 | 78286 | SIKORSKY AIRCRAFT CORPORATIONDBA SIKORSKY |
Technical Data | NSN 3040-01-100-2729
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | 2 PLAIN |
| MATERIAL | STEEL CORROSION RESISTING |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5629 ASSN STD SINGLE MATERIAL RESPONSE |
| SURFACE FINISH | 8.0 MICROINCHES |
| FIRST END DIAMETER | 0.3750 INCHES NOMINAL |
| FIRST END EXTERNAL THREAD LENGTH | 0.640 INCHES NOMINAL |
| END SIMILARITY | NOT IDENTICAL |
| SECOND END STYLE | 5 TAPERED WITH FLAT |
| SECOND END DIAMETER | 0.1905 INCHES MINIMUM AND 0.1910 INCHES MAXIMUM |
| SECOND END HOLE DIAMETER | 0.0700 INCHES MINIMUM AND 0.0800 INCHES MAXIMUM |
| SECOND END DISTANCE FROM HOLE CENTER TO END | 0.290 INCHES NOMINAL |
| SECOND END EXTERNAL THREAD LENGTH | 0.480 INCHES MINIMUM AND 0.560 INCHES MAXIMUM |
| SECOND END HOLE DEPTH | 0.191 INCHES NOMINAL |
| LARGEST STEP DIAMETER | 0.750 INCHES NOMINAL |
| OVERALL LENGTH | 11.270 INCHES NOMINAL |
| STEP QUANTITY | 9 |
| SPECIAL FEATURES | FLIGHT SAFETY CRITICAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FSC APPLICATION DATA | HUB ASSEMBLY,MAIN ROTOR |