NSN 5306-01-513-8611
Part Details | INTERNALLY RELIEVED BODY BOLT
5306-01-513-8611 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: 74A4251202009, 74A425120-2009, 74A4251202019, 74A425120-2019, 74A4251202009, 74A425120-2009, 74A4251202019, 74A425120-2019, 5306-01-513-8611, 01-513-8611, 5306015138611, 015138611
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | OCT 08, 2003 | 01-513-8611 | 06676 ( BOLT, INTERNALLY RELIEVED BODY ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5306-01-513-8611
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 74A425120-2009 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 74A425120-2019 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 74A425120-2009 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 74A425120-2019 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
Technical Data | NSN 5306-01-513-8611
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | F-18 E/F |