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National Stock Number:
3040-01-505-4119
Federal Supply Class:
3040
National Item Identification Number:
015054119
Description:
SHAFT,STRAIGHT
Detail:
A straight shaft having two or more of the following conditions: a specified surface finish designation in the range of 1 to 125 microinches (o.o25 to 3.2 micrometers), arithmetical average (aa), machined peripheral flat(s), circular groove (s), keyway(s), splines, threads, or holes. It is not designed for use in aligning by fitting into corresponding holes of another item. It may be drilled for jubricating holes. For items having an integral gear(s) or worm(s), see GEARSHAFT (as modified). For items designed to support rotating members see AXLE(1), STRAIGHT. For items not having the above conditions see PIN, STRAIGHT, HEADLESS. For items having machined ends which constitute steps see SHAFT(1), SHOULDERED; AXLE(1), SHOULDERED; and BOLT, FLUID PASSAGE.
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Manufacturer Information:
| 9-64880 | 82918 | THE BOEING COMPANY | | 9-64880-2 | 82918 | THE BOEING COMPANY |
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Techincal Specification:
| END SIMILARITY | NOT IDENTICAL | | FIRST END DIAMETER | 1.9940 INCHES NOMINAL | | FIRST END PITCH DIAMETER | 1.9500 INCHES NOMINAL | | FIRST END PRESSURE ANGLE | 30.0 DEGREES NOMINAL | | FIRST END SPLINE LENGTH | 0.750 INCHES NOMINAL | | FIRST END SPLINE MAJOR DIAMETER | 2.0000 INCHES NOMINAL | | FIRST END SPLINE MINOR DIAMETER | 1.8500 INCHES NOMINAL | | FIRST END SPLINE QUANTITY | 39 | | FIRST END STYLE | SPLINED (INVOLUTE) | | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-6732 MIL SPEC SINGLE MATERIAL RESPONSE OR MIL-T-6736 MIL SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | STEEL COMP 8630 OR STEEL COMP 4130 | | PART NAME ASSIGNED BY CONTROLLING AGENCY | SHAFT, CAM ROLLER | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 18.000 INCHES NOMINAL | | SECOND END DIAMETER | 1.9940 INCHES NOMINAL | | SECOND END STYLE | PLAIN | | SPECIAL FEATURES | MATT STEEL TUBE;STOCK 2.125 O.D. X .25 WALL X 18.0 LG;HEAT TREAT; SIX CROSS DRILLED HOLES; 1 ST. END I.D. 1.69;2ND. END I.D. 1.7812;T.O. 1C-135(K)A-4 FIG. 953 IND. 61 |
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