Part Details | HEADLESS STRAIGHT PIN
5315-00-238-1171 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.
Alternate Parts: 669864021, 66986-402-1, 5315-00-238-1171, 00-238-1171, 5315002381171, 002381171
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | SEP 08, 1972 | 00-238-1171 | 02390 ( PIN, STRAIGHT, HEADLESS ) |
REFERENCE DRAWINGS & PICTURES
CHAMFERED
CHAMFERED
DRILLED THRU CENTER
Cross Reference | NSN 5315-00-238-1171
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 66986-402-1 | 94756 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 5315-00-238-1171
| Characteristic | Specifications |
|---|---|
| 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 |