NSN 3040-00-106-8405
Part Details | SHOULDERED SHAFT
3040-00-106-8405 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: 32140167, 32-14016-7, 3040-00-106-8405, 00-106-8405, 3040001068405, 001068405
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
30 | JUL 19, 1968 | 00-106-8405 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
PLAIN

PLAIN

Cross Reference | NSN 3040-00-106-8405
Part Number | Cage Code | Manufacturer |
---|---|---|
32-14016-7 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 3040-00-106-8405
Characteristic | Specifications |
---|---|
FIRST END STYLE | PLAIN |
MATERIAL | ALUMINUM ALLOY 2024 |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 6,COND T4 FED SPEC SINGLE MATERIAL RESPONSE |
SURFACE FINISH | 250.0 MICROINCHES |
FIRST END DIAMETER | 0.5600 INCHES NOMINAL |
END SIMILARITY | IDENTICAL |
LARGEST STEP DIAMETER | 0.747 INCHES NOMINAL |
OVERALL LENGTH | 2.950 INCHES NOMINAL |
STEP QUANTITY | 4 |
SPECIAL FEATURES | TWO HOLES DRILLED,ONE IN EACH END,0.250 IN DIA;KEYWAY NEAR CENTER OF SHAFT |
END ITEM IDENTIFICATION | F-4 AIRCRAFT |