Part Details | HEADLESS SHOULDER PIN
5315-00-872-3277 A cylindrically-shaped headless item, having a shank at one or both ends. It is used for aligning, fastening, or transfer of torque and/or thrust by fitting into corresponding holes of another item. It may be threaded on one end.
Alternate Parts: 114S17571, 114S1757-1, 114S17571, 114S1757-1, 5315-00-872-3277, 00-872-3277, 5315008723277, 008723277
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1960 | 00-872-3277 | 16749 ( PIN, SHOULDER, HEADLESS ) |
REFERENCE DRAWINGS & PICTURES
CHAMFERED
SLOTTED
CHAMFERED
SLOTTED
BOTH END DRILLED
SHOULDER
Cross Reference | NSN 5315-00-872-3277
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 114S1757-1 | 81205 | THE BOEING COMPANYDBA BOEING |
| 114S1757-1 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 5315-00-872-3277
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | SHOULDER |
| SHANK LENGTH | 0.342 INCHES MINIMUM AND 0.362 INCHES MAXIMUM |
| SHOULDER DIAMETER | 0.371 INCHES MINIMUM AND 0.373 INCHES MAXIMUM |
| SHANK DIAMETER | 0.246 INCHES MINIMUM AND 0.248 INCHES MAXIMUM |
| OVERALL LENGTH | 2.302 INCHES MINIMUM AND 2.322 INCHES MAXIMUM |
| FIRST END STYLE | CHAMFERED |
| FIRST END TAPER LENGTH | 0.052 INCHES MINIMUM AND 0.072 INCHES MAXIMUM |
| FIRST END TAPER ANGLE | 15.0 DEGREES NOMINAL |
| SECOND END RELATIONSHIP WITH FIRST END | NOT IDENTICAL |
| SECOND END STYLE | SLOTTED |
| SECOND END SLOT DEPTH | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| SECOND END SLOT WIDTH | 0.084 INCHES MINIMUM AND 0.104 INCHES MAXIMUM |
| FIRST END LOCATION | SHANK END |
| HOLE ARRANGEMENT STYLE | BOTH END DRILLED |
| FIRST HOLE DIAMETER | 0.084 INCHES MINIMUM AND 0.104 INCHES MAXIMUM |
| SECOND HOLE DIAMETER | 0.084 INCHES MINIMUM AND 0.104 INCHES MAXIMUM |
| DISTANCE FROM CENTERLINE OF HOLE TO END OF PIN | 0.692 INCHES MINIMUM AND 0.732 INCHES MAXIMUM |
| CENTER TO CENTER DISTANCE BETWEEN HOLES | 0.850 INCHES MINIMUM AND 0.890 INCHES MAXIMUM |
