Part Details | HEADED STRAIGHT PIN
5315-00-367-8789 A headed, cylindrically-shaped item having a solid shank for fitting into corresponding holes, used for aligning or fastening. It may have welding projections. It also may contain holes drilled perpendicular to axial centerline. Excludes PIN, ECCENTRIC.
Alternate Parts: 4036610, 4036610, 5315-00-367-8789, 00-367-8789, 5315003678789, 003678789
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | FEB 27, 1974 | 00-367-8789 | 02384 ( PIN, STRAIGHT, HEADED ) |
REFERENCE DRAWINGS & PICTURES
DEE
STRAIGHT
Cross Reference | NSN 5315-00-367-8789
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4036610 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4036610 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5315-00-367-8789
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | STRAIGHT |
| CHAMFER LENGTH | 0.030 INCHES MINIMUM AND 0.040 INCHES MAXIMUM |
| DIAMETER | 0.248 INCHES MINIMUM AND 0.249 INCHES MAXIMUM |
| UNDER HEAD LENGTH | 0.705 INCHES MINIMUM AND 0.725 INCHES MAXIMUM |
| PIN CHAMFER ANGLE | 40.0 DEGREES MINIMUM AND 50.0 DEGREES MAXIMUM |
| HEAD STYLE | 9 DEE |
| HEAD LENGTH | 0.625 INCHES NOMINAL |
| HEAD WIDTH | 0.390 INCHES MINIMUM AND 0.410 INCHES MAXIMUM |
| HEIGHT | 0.040 INCHES MINIMUM AND 0.045 INCHES MAXIMUM |
| SPECIAL FEATURES | HEAD-TWO CORNERS AT SAME END CHAMFERED,45.0 DEG,0.060 TO 0.080 IN.,OPPOSITE FACE (WIDTH) CURVED |
| END ITEM IDENTIFICATION | W/S: AIRCRAFT, EAGLE F-15; AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); SUPPORT EQUIPMENT, C-5 AIRCRAFT; ENGINE, AIRCRAFT, F100-PW-220 (F-15C/D/E); AIRCRAFT, F-111; ADVANCED AIR TRAFFIC CONTR. & LAND. SYS (ATCALS) 404L |