NSN 5306-01-513-8612
Part Details | INTERNALLY RELIEVED BODY BOLT
5306-01-513-8612 An externally threaded fastener whose external threaded portion is of one nominal diameter. It has a concentric hole along the longitudinal centerline which may extend a part or the full length of the bolt. The concentric hole along the centerline may be counterbored and/or internally threaded at the head end or the bolt end. The head is designed to be held or driven by an external and/or internal driver. For items having a hole(s) perpendicular to the axis which meet the concentric hole along the longitudinal centerline, see BOLT, FLUID PASSAGE.
Alternate Parts: 74A4251202013, 74A425120-2013, 74A4251202023, 74A425120-2023, 74A4251202013, 74A425120-2013, 74A4251202023, 74A425120-2023, 5306-01-513-8612, 01-513-8612, 5306015138612, 015138612
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | OCT 08, 2003 | 01-513-8612 | 06676 ( BOLT, INTERNALLY RELIEVED BODY ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5306-01-513-8612
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 74A425120-2013 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 74A425120-2023 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 74A425120-2013 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 74A425120-2023 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
Technical Data | NSN 5306-01-513-8612
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | F-18 E/F |