Item Name | Bolt Internally Relieved Body |
Federal Supply Group (FSG) | Hardware and Abrasives |
Federal Supply Class (FSC) | 5306 Bolts |
National Item Identification Number (NIIN) | 01-286-6388 (012866388) |
NCB Code | USA (01) |
Manufacturer | Kitco Inc, Sps Technologies Inc, Nassau Tool Works Inc, Transaero Pty Ltd, Triumph Structures Los Angeles Inc, International Precision Inc, Hdi Landing Gear Usa Inc, Heroux Devtek Inc, Quality Socket Screw Corporation, Apex Manufacturing Company Inc, Honeywell International Inc, C And H Manufacturing Inc, Goodrich Corporation, Eagle Tool And Machine Co Inc, Boeing Company The, Es3 Prime Logistics Group Inc, Western Precision Industries, Triumph Actuation Systems Llc, Alcoa Global Fasteners Inc, Fitz Aerospace Llc, Ace Precision Inc, Magellan Aerospace Limited, Cm Manufacturing Inc |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
68A410615-2003 | kitco inc | bolt internally relieved body | RFQ |
68A410615-2003 | sps technologies inc | bolt internally relieved body | RFQ |
68A410615-2003 | nassau tool works inc | bolt internally relieved body | RFQ |
68A410615-2003 | transaero pty ltd | bolt internally relieved body | RFQ |
68A410615-2003 | triumph structures los angeles inc | bolt internally relieved body | RFQ |
68A410615-2003 | international precision inc | bolt internally relieved body | RFQ |
68A410615-2003 | hdi landing gear usa inc | bolt internally relieved body | RFQ |
68A410615-2003 | heroux devtek inc | bolt internally relieved body | RFQ |
68A410615-2003 | quality socket screw corporation | bolt internally relieved body | RFQ |
68A410615-2003 | apex manufacturing company inc | bolt internally relieved body | RFQ |
68A410615-2003 | honeywell international inc | bolt internally relieved body | RFQ |
68A410615-2003 | c and h manufacturing inc | bolt internally relieved body | RFQ |
68A410615-2003 | goodrich corporation | bolt internally relieved body | RFQ |
68A410615-2003 | eagle tool and machine co inc | bolt internally relieved body | RFQ |
68A410615-2003 | boeing company the | bolt internally relieved body | RFQ |
68A410615-2003 | es3 prime logistics group inc | bolt internally relieved body | RFQ |
68A410615-2003 | western precision industries | bolt internally relieved body | RFQ |
68A410615-2003 | triumph actuation systems llc | bolt internally relieved body | RFQ |
68A410615-2003 | alcoa global fasteners inc | bolt internally relieved body | RFQ |
68A410615-2003 | fitz aerospace llc | bolt internally relieved body | RFQ |
68A410615-2003 | ace precision inc | bolt internally relieved body | RFQ |
68A410615-2003 | magellan aerospace limited | bolt internally relieved body | RFQ |
68A410615-2003 | cm manufacturing inc | bolt internally relieved body | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 3A |
AAJF | THREAD DIRECTION | RIGHT-HAND |
AASA | THREAD LENGTH | 0.343 INCHES NOMINAL |
AASB | FASTENER LENGTH | 1.573 INCHES NOMINAL |
AASK | HEAD STYLE | DEE CHAMFER |
AASL | HEAD DIAMETER | 0.690 INCHES NOMINAL |
AASU | HEAD HEIGHT | 0.100 INCHES NOMINAL |
AASY | DISTANCE FROM CENTERLINE TO FLAT | 0.290 INCHES MINIMUM AND 0.295 INCHES MAXIMUM |
AAWB | SHANK UNTHREADED HOLE DIAMETER | 0.105 INCHES MINIMUM FIRST HOLE AND 0.108 INCHES MAXIMUM FIRST HOLE |
AAWX | CONCENTRIC HOLE DEPTH | 1.160 INCHES NOMINAL |
AAXC | CONCENTRIC HOLE DIAMETER | 0.205 INCHES MINIMUM AND 0.215 INCHES MAXIMUM |
AHYM | NOMINAL THREAD DIAMETER | 0.375 INCHES |
CMLP | THREAD QUANTITY PER INCH | 24 |
CQBC | MINIMUM TENSILE STRENGTH | 180000 POUNDS PER SQUARE INCH |
CRZS | DISTANCE FROM HEAD LARGEST BEARING SURFACE TO SHANK HOLE CENTER | 1.470 INCHES NOMINAL FIRST HOLE |
FEAT | SPECIAL FEATURES | EGRIP CLOSE TOLERANCE 0.373 MIN. IN. DIAMETER AND 0.374 MAX. IN. DIAMETER,LENGTH OF GRIP 1.225 MIN. IN. AND 1.235 MAX. IN.; PAINT WHITE ENAMEL,FIRST UNDER CUT,FLAT SIDE OF HEAD,INTERNAL HOLE,CHAMPER |
HUES | COLOR | WHITE POINT |
HUES | COLOR | WHITE TOP OF HEAD |
MATT | MATERIAL | STEEL COMP E4340 OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5000 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL |
SFTT | SURFACE TREATMENT | CADMIUM GRIP AND CHROMATE GRIP |
SFTT | SURFACE TREATMENT | CADMIUM SIDES OF HEAD AND CHROMATE SIDES OF HEAD |
SFTT | SURFACE TREATMENT | CADMIUM THREADS AND CHROMATE THREADS |
SFTT | SURFACE TREATMENT | ENAMEL POINT |
SFTT | SURFACE TREATMENT | ENAMEL TOP OF HEAD |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MMS-420,CAGEC 76301 MFR REF SINGLE TREATMENT RESPONSE POINT |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MMS-420,CAGEC 76301 MFR REF SINGLE TREATMENT RESPONSE TOP OF HEAD |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PS13145,CAGEC 76301 MFR REF SINGLE TREATMENT RESPONSE GRIP |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PS13145,CAGEC 76301 MFR REF SINGLE TREATMENT RESPONSE SIDES OF HEAD |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PS13145,CAGEC 76301 MFR REF SINGLE TREATMENT RESPONSE THREADS |
STYL | STYLE DESIGNATOR | CONCENTRIC HOLE UNTHREADED |
THSD | THREAD SERIES DESIGNATOR | UNJF |
Relevant Components for NSN - 5306-01-286-6388, 5306012866388 | ||||
5320-01-311-2514 (5320013112514) | 5365-01-606-7886 (5365016067886) | 5310-01-687-5946 (5310016875946) | 5331-01-345-2325 (5331013452325) | |
5331-01-137-6352 (5331011376352) | 5340-01-677-5187 (5340016775187) | 5310-01-215-1121 (5310012151121) | 5330-01-558-9303 (5330015589303) | |
5320-01-007-1870 (5320010071870) | 5365-00-542-0989 (5365005420989) | 5305-01-279-0723 (5305012790723) | 5315-01-181-8363 (5315011818363) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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