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National Stock Number:
5315-00-238-1171
Federal Supply Class:
5315
National Item Identification Number:
002381171
Description:
PIN,STRAIGHT,HEADLESS
Detail:
A headless, cylindrically-shaped item having a straight, smooth, solid body, with or without a drilled hole(s). It has an outside diameter equal to or less than its length. Its length must not exceed twelve inches (304 MM); for items whose length exceeds twelve inches (304 MM); see ROD, STRAIGHT, HEADLESS. It is used for aligning or transfer of torque and/or thrust, by fitting into corresponding holes of another item. See also PIN, STRAIGHT, THREADED.
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Manufacturer Information:
| 66986-402-1 | 94756 | THE BOEING COMPANY |
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Techincal Specification:
| MATERIAL | ALUMINUM ALLOY 2017 OVERALL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/5 ALLOY 2017 T4 FED SPEC SINGLE MATERIAL RESPONSE OVERALL | | SURFACE TREATMENT | ANODIZE OVERALL | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MA0109-009,94756 MFR REF SINGLE TREATMENT RESPONSE OVERALL | | FIRST END STYLE | CHAMFERED | | FIRST END TAPER LENGTH | 0.020 INCHES NOMINAL | | FIRST END TAPER ANGLE | 45.0 DEGREES NOMINAL | | SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL | | HOLE ARRANGEMENT STYLE | DRILLED THRU CENTER | | FIRST HOLE DIAMETER | 0.039 INCHES MINIMUM AND | | 0.041 INCHES MAXIMUM | | PIN OVERALL LENGTH | 0.200 INCHES NOMINAL | | PIN OVERALL DIAMETER | 0.1562 INCHES NOMINAL | | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED | | SPECIAL FEATURES | DESIGN ANALYSIS; NUCLEAR HARDNESS CRITICAL | | THE MANUFACTURERS DATA | | | MANUFACTURERS CODE | 94756 | | DESIGN CONTROL REFERENCE | 66986-402-1 |
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