Thank you for taking interest in Lockheed Martin Corporation part number 4G13980-101A, which is listed with the NSN 5306-00-135-1376 and a product description of “Bolt Internally Rel.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
Note : We Will Not Share Your Information To Any Third Parties.
Alongside part number 4G13980-101A, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Bolt Internally Rel part with the NSN 5306-00-135-1376. For example, you can browse other Lockheed Martin Corporation components that were produced under CAGE Code 98897 or listings that belong to FSC 5306 Bolts with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 4G13980-101A and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5306-00-135-1376 Item PartTypeName: BOLT,INTERNALLY RELIEVED BODY | 5306 | 001351376 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4G13980-101A | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASA | THREAD LENGTH | 0.506 INCHES MINIMUM |
| AASB | FASTENER LENGTH | 3.160 INCHES NOMINAL |
| AASK | HEAD STYLE | ROUND W/WRENCH FLATS CHAMFERED |
| AASL | HEAD DIAMETER | 1.320 INCHES NOMINAL |
| AASU | HEAD HEIGHT | 0.160 INCHES NOMINAL |
| AATB | WIDTH BETWEEN FLATS | 1.125 INCHES NOMINAL |
| AAVH | SHOULDER DIAMETER | 0.870 INCHES MINIMUM AND 0.871 INCHES MAXIMUM |
| AAVK | SHOULDER LENGTH | 2.560 INCHES NOMINAL |
| AAWX | CONCENTRIC HOLE DEPTH | 2.500 INCHES NOMINAL |
| AAXC | CONCENTRIC HOLE DIAMETER | 0.625 INCHES NOMINAL |
| CQBC | MINIMUM TENSILE STRENGTH | 220000 POUNDS PER SQUARE INCH |
| MATT | MATERIAL | STEEL OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6427 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| STYL | STYLE DESIGNATOR | CONCENTRIC HOLE UNTHREADED |
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.
Request for Quote
