NSN 3040-00-106-6173
Part Details | SHOULDERED SHAFT
3040-00-106-6173 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: 8835951, 883595-1, 8835951, 883595-1, 3040-00-106-6173, 00-106-6173, 3040001066173, 001066173
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
30 | JUL 17, 1968 | 00-106-6173 | 22914 ( SHAFT, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
PLAIN

PLAIN

Cross Reference | NSN 3040-00-106-6173
Part Number | Cage Code | Manufacturer |
---|---|---|
883595-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
883595-1 | 59364 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 3040-00-106-6173
Characteristic | Specifications |
---|---|
FIRST END STYLE | PLAIN |
MATERIAL | STEEL |
SURFACE FINISH | 32.0 MICROINCHES |
FIRST END DIAMETER | 0.1900 INCHES NOMINAL |
FIRST END HOLE DIAMETER | 0.0900 INCHES NOMINAL |
FIRST END DISTANCE FROM HOLE CENTER TO END | 1.9400 INCHES NOMINAL |
FIRST END HOLE DEPTH | 0.1200 INCHES NOMINAL |
END SIMILARITY | NOT IDENTICAL |
SECOND END STYLE | 3 PLAIN |
SECOND END DIAMETER | 0.1900 INCHES NOMINAL |
SECOND END WIDTH ACROSS FLATS | 0.1870 INCHES NOMINAL |
SECOND END STEP LENGTH | 0.6050 INCHES NOMINAL |
LARGEST STEP DIAMETER | 0.314 INCHES NOMINAL |
OVERALL LENGTH | 4.360 INCHES NOMINAL |
STEP QUANTITY | 2 |
FSC APPLICATION DATA | TURBO-FAN HEAT EXCHANGE AIRCRAFT |