ASAP Aviation Procurement is pleased to announce that part number 339459 of NSN 5306-00-208-0261 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number 339459 is a Bolt Internally Rel manufactured by Lockheed Martin Corporation under CAGE Code 98897. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote. In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5306-00-208-0261 Item PartTypeName: BOLT,INTERNALLY RELIEVED BODY | 5306 | 002080261 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | ||||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 339459 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASA | THREAD LENGTH | 0.365 INCHES MINIMUM AND 0.395 INCHES MAXIMUM |
| AASB | FASTENER LENGTH | 8.780 INCHES NOMINAL |
| AASK | HEAD STYLE | ROUND W/WRENCH FLATS |
| AASL | HEAD DIAMETER | 3.000 INCHES NOMINAL |
| AASU | HEAD HEIGHT | 0.250 INCHES NOMINAL |
| AATB | WIDTH BETWEEN FLATS | 2.478 INCHES MINIMUM AND 2.488 INCHES MAXIMUM |
| AAXC | CONCENTRIC HOLE DIAMETER | 1.375 INCHES NOMINAL |
| AHYM | NOMINAL THREAD DIAMETER | 2.000 INCHES |
| CMLP | THREAD QUANTITY PER INCH | 16 |
| CQBC | MINIMUM TENSILE STRENGTH | 150000 POUNDS PER SQUARE INCH |
| FEAT | SPECIAL FEATURES | 1SLOT IN THREAD END 0.250 IN. WIDE BY 0.500 IN. DEEP AND UNDERCUT BETWEEN HEAD AND GRIP 1.975 IN. MIN 1.985 IN. MAX DIA BY 0.170 IN. WIDE AND UNDERCUT BETWEEN GRIP AND THREADS 1.896 IN.MIN 1.906 IN. MAX DIA BY 0.190 IN. MIN 0.220 IN. MAX WI |
| MATT | MATERIAL | STEEL COMP 8630 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-6050 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | CHROMIUM OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | TY 2.FSCM 98897 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| STYL | STYLE DESIGNATOR | CONCENTRIC HOLE UNTHREADED |
| THSD | THREAD SERIES DESIGNATOR | UN |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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