Part Details | SHOULDERED SHAFT
3040-01-149-7444 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: 202297611, 2022976-1-1, 16VM0030039, 16VM003003-9, 202297612, 2022976-1-2, 3040-01-149-7444, 01-149-7444, 3040011497444, 011497444
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | MAR 25, 1983 | 01-149-7444 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
TAPERED WITH FLAT
TAPERED WITH FLAT
Cross Reference | NSN 3040-01-149-7444
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2022976-1-1 | 70210 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 16VM003003-9 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 2022976-1-2 | 0ZWK8 | MOOG INC.DBA MOOG AIRCRAFT GROUP TORRANCE |
Technical Data | NSN 3040-01-149-7444
| Characteristic | Specifications |
|---|---|
| FIRST END STYLE | 3 TAPERED WITH FLAT |
| MATERIAL | STEEL CORROSION RESISTING |
| FIRST END DIAMETER | 1.1200 INCHES NOMINAL |
| FIRST END HOLE DIAMETER | 0.1900 INCHES NOMINAL |
| FIRST END DISTANCE FROM HOLE CENTER TO END | 0.7500 INCHES NOMINAL |
| END SIMILARITY | IDENTICAL |
| LARGEST STEP DIAMETER | 1.250 INCHES NOMINAL |
| OVERALL LENGTH | 27.605 INCHES NOMINAL |
| STEP QUANTITY | 3 |
| SPECIAL FEATURES | INTERNAL SPLINES SECOND END |
| END ITEM IDENTIFICATION | F-16 ACFT |
| SUPPLEMENTARY FEATURES | BARRIER FOR GREASE RETENTION |