NSN 5306-00-316-5557, (5306003165557) - Bolt Internally Rel Parts List
Bolt Internally Rel parts under NSN 5306-00-316-5557 manufactured by Aero Engineering And Manufacturing, Mercer Products And Manufacturing, Mercury Aerospace Fasteners Inc, Triumph Aerostructures Llc, United Technologies Corporation. All NSN items provided by NSN Parts Hub are compliant with fit, form, and functionality according to parameters set by the DLA. With over 3 billion new and obsolete parts in our searchable database, you can find your required part number of NSN 5306-00-316-5557 with ease when you use NSN Parts Hub as your purchasing partner. We maintain an unmatched supply-chain network with trusted MFRs and verified PMAs and are the only distributor with a No China Sourcing pledge. Do you require part numbers other than 1283171-101, ASE50322-25? Related NSN parts are listed below for your convenience.
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| Alternative NSN: 5306003165557 |
| Item Name: Bolt Internally Rel |
| Federal Supply Class (FSC): 5306 Bolts |
| NIIN: 003165557 |
| NCB Code: USA (00) |
| Manufacturers: Aero Engineering And Manufacturing , Mercer Products And Manufacturing , Mercury Aerospace Fasteners Inc , Triumph Aerostructures Llc , United Technologies Corporation |
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| 1283171-101 | aero engineering and manufacturing | bolt internally rel | Avl | RFQ |
| 1283171-101 | mercer products and manufacturing | bolt internally rel | Avl | RFQ |
| 1283171-101 | mercury aerospace fasteners inc | bolt internally rel | Avl | RFQ |
| 1283171-101 | triumph aerostructures llc | bolt internally rel | Avl | RFQ |
| ASE50322-25 | united technologies corporation | bolt internally rel | Avl | RFQ |
Characteristics Data of NSN 5306003165557
| MRC | Criteria | Characteristic |
|---|---|---|
| AAEL | THREADS PER INCH | 24 CONCENTRIC HOLE |
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASA | THREAD LENGTH | 1.150 INCHES MINIMUM |
| AASB | FASTENER LENGTH | 4.500 INCHES NOMINAL |
| AASK | HEAD STYLE | HEXAGON |
| AASU | HEAD HEIGHT | 0.312 INCHES MINIMUM AND 0.327 INCHES MAXIMUM |
| AATB | WIDTH BETWEEN FLATS | 0.928 INCHES MINIMUM AND 0.940 INCHES MAXIMUM |
| AAVH | SHOULDER DIAMETER | 0.6243 INCHES MINIMUM AND 0.6248 INCHES MAXIMUM |
| AAVK | SHOULDER LENGTH | 2.870 INCHES NOMINAL |
| AAWB | SHANK UNTHREADED HOLE DIAMETER | 0.106 INCHES MINIMUM FIRST HOLE AND 0.116 INCHES MAXIMUM FIRST HOLE |
| AAWX | CONCENTRIC HOLE DEPTH | 0.810 INCHES NOMINAL |
| AAXC | CONCENTRIC HOLE DIAMETER | 0.375 INCHES NOMINAL |
| ABXT | INTERNAL THREAD LENGTH | 0.560 INCHES NOMINAL CONCENTRIC HOLE |
| AHYM | NOMINAL THREAD DIAMETER | 0.375 INCHES |
| BZRR | THREAD SERIES | UNJF CONCENTRIC HOLE |
| CMLP | THREAD QUANTITY PER INCH | 24 |
| CQBC | MINIMUM TENSILE STRENGTH | 180000 POUNDS PER SQUARE INCH |
| CQJX | NOMINAL THREAD SIZE | 0.375 INCHES CONCENTRIC HOLE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AAVH |
| CRZS | DISTANCE FROM HEAD LARGEST BEARING SURFACE TO SHANK HOLE CENTER | 4.200 INCHES NOMINAL FIRST HOLE |
| MATT | MATERIAL | STEEL COMP E4340 OVERALL |
| SFTT | SURFACE TREATMENT | CADMIUM OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | LC+77-1061,CL 2,TY 2,36659 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| STYL | STYLE DESIGNATOR | CONCENTRIC HOLE THREADED |
| TEST | TEST DATA DOCUMENT | 36659-ALC+72-2014 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 |
| THSD | THREAD SERIES DESIGNATOR | UNJF |
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