Part Details | INTERNALLY RELIEVED BODY BOLT
5306-00-316-5557 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: 1283171101, 1283171-101, 1283171101, 1283171-101, 1283171101, 1283171-101, 1283171101, 1283171-101, 1283171101, 1283171-101, 1283171101, 1283171-101, 1283171101, 1283171-101, ASE5032225, ASE50322-25, 5306-00-316-5557, 00-316-5557, 5306003165557, 003165557
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | NOV 11, 1973 | 00-316-5557 | 06676 ( BOLT, INTERNALLY RELIEVED BODY ) |
REFERENCE DRAWINGS & PICTURES
HEXAGON
CONCENTRIC HOLE UNTHREADED
Cross Reference | NSN 5306-00-316-5557
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1283171-101 | 17772 | AERO ENGINEERING & MANUFACTURINGCOMPANY OF CALIFORNIA |
| 1283171-101 | 29214 | BARCO ENGINEERING CO INC |
| 1283171-101 | 4H229 | KAYGOR INC |
| 1283171-101 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 1283171-101 | 30205 | MERCER PRODUCTS & MANUFACTURINGCOMPANY |
| 1283171-101 | 50945 | MERCURY AEROSPACE FASTENERS INC |
| 1283171-101 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
| ASE50322-25 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5306-00-316-5557
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNJF |
| NOMINAL THREAD DIAMETER | 0.375 INCHES |
| THREAD QUANTITY PER INCH | 24 |
| THREAD CLASS | 3A |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD LENGTH | 1.150 INCHES MINIMUM |
| FASTENER LENGTH | 4.500 INCHES NOMINAL |
| MINIMUM TENSILE STRENGTH | 180000 POUNDS PER SQUARE INCH |
| STYLE DESIGNATOR | A CONCENTRIC HOLE UNTHREADED |
| SHOULDER DIAMETER | 0.6243 INCHES MINIMUM AND 0.6248 INCHES MAXIMUM |
| SHOULDER LENGTH | 2.870 INCHES NOMINAL |
| CONCENTRIC HOLE DEPTH | 0.810 INCHES NOMINAL |
| CONCENTRIC HOLE DIAMETER | 0.375 INCHES NOMINAL |
| HEAD STYLE | HEXAGON |
| HEAD HEIGHT | 0.312 INCHES MINIMUM AND 0.327 INCHES MAXIMUM |
| WIDTH BETWEEN FLATS | 0.928 INCHES MINIMUM AND 0.940 INCHES MAXIMUM |
| TEST DATA DOCUMENT | 36659-ALP72-2014 DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) |
| CRITICALITY CODE JUSTIFICATION | AAVH |