Part Details | SHOULDERED SHAFT
3040-01-408-9983 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: 7883411, 788341-1, 7883411, 788341-1, 3040-01-408-9983, 01-408-9983, 3040014089983, 014089983
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | MAR 03, 1995 | 01-408-9983 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
TAPERED WITH FLAT
INTERNAL THREADED
TAPERED WITH FLAT
INTERNAL THREADED
Cross Reference | NSN 3040-01-408-9983
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 788341-1 | 73030 | HAMILTON SUNDSTRAND CORPORATION |
| 788341-1 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 3040-01-408-9983
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | INTERNAL THREADED |
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5643 PER HS178 MFR REF SINGLE MATERIAL RESPONSE |
| FIRST END DIAMETER | 0.4195 INCHES NOMINAL |
| FIRST END INTERNAL THREAD LENGTH | 0.520 INCHES NOMINAL |
| END SIMILARITY | NOT IDENTICAL |
| SECOND END STYLE | 3 TAPERED WITH FLAT |
| SECOND END DIAMETER | 0.1430 INCHES NOMINAL |
| SECOND END HOLE DIAMETER | 0.0350 INCHES NOMINAL |
| SECOND END DISTANCE FROM HOLE CENTER TO END | 0.0750 INCHES NOMINAL |
| LARGEST STEP DIAMETER | 0.4195 INCHES NOMINAL |
| OVERALL LENGTH | 2.245 INCHES NOMINAL |
| STEP QUANTITY | 7 |
| SPECIAL FEATURES | THREAD 190-32UNF-3B, HELICAL COIL INSERT DEPTH 32 MIN, HARDNESS 31-39 HRC, USED ON EEC FUEL CONTROL, F117 ENGINE |