If your operations demand dependable items that fall under the NSN 5306-00-097-9405, look no further than the expansive product list featured on this page. For your convenience, all NSN 5306-00-097-9405 part numbers that we have in stock like 597872, and others are listed below with their respective manufacturer. Should any of these products match your requirements, you may click on the “RFQ” button presented next to each listing to access our online quote request service. By providing our team with information like your desired part quantity, pricing, and fulfillment speed on the form you are directed to, we can offer a procurement solution that best accommodates your needs within 15 minutes of our receipt and review.
You never have to compromise any of your needs when you shop with us, as we always aim to offer competitive pricing and delivery times for every order. Furthermore, quality is a fundamental cornerstone of our operations, and we carry out various practices to guarantee the fit, form, and function of our NSN 5306-00-097-9405 products, starting with strictly sourcing from trustworthy NSN parts suppliers and manufacturers. To learn more about our diverse commitments and see why so many customers steadily depend on our services, connect with us by form, phone, or email at your earliest convenience.
| Item Name | Bolt Shoulder |
| Federal Supply Group (FSG) | Hardware and Abrasives |
| Federal Supply Class (FSC) | 5306 Bolts |
| National Item Identification Number (NIIN) | 00-097-9405 (000979405) |
| NCB Code | USA (00) |
| Manufacturer | Turbo Power And Marine System Inc, United Technologies Corporation, Sps Technologies Inc, Alcoa Global Fasteners Inc, Aerojet Rocketdyne Inc |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 597872 | turbo power and marine system inc | bolt shoulder | RFQ |
| 597872 | united technologies corporation | bolt shoulder | RFQ |
| 597872 | sps technologies inc | bolt shoulder | RFQ |
| 597872 | alcoa global fasteners inc | bolt shoulder | RFQ |
| 597872 | aerojet rocketdyne inc | bolt shoulder | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASA | THREAD LENGTH | 0.465 INCHES MINIMUM AND 0.495 INCHES MAXIMUM |
| AASB | FASTENER LENGTH | 0.950 INCHES MINIMUM AND 0.970 INCHES MAXIMUM |
| AASK | HEAD STYLE | DOUBLE HEXAGON W/HOLE |
| AASU | HEAD HEIGHT | 0.365 INCHES MINIMUM AND 0.385 INCHES MAXIMUM |
| AATB | WIDTH BETWEEN FLATS | 0.367 INCHES MINIMUM AND 0.376 INCHES MAXIMUM |
| AATC | EXTENDED WASHER DIAMETER | 0.490 INCHES MINIMUM AND 0.510 INCHES MAXIMUM |
| AATD | EXTENDED WASHER THICKNESS | 0.070 INCHES MINIMUM AND 0.080 INCHES MAXIMUM |
| AATN | SHOULDER DIAMETER | 0.335 INCHES MINIMUM FIRST SHOULDER AND 0.337 INCHES MAXIMUM FIRST SHOULDER |
| AATX | SHOULDER LENGTH | 0.475 INCHES MINIMUM FIRST SHOULDER AND 0.485 INCHES MAXIMUM FIRST SHOULDER |
| AHYM | NOMINAL THREAD DIAMETER | 0.250 INCHES |
| CMLP | THREAD QUANTITY PER INCH | 28 |
| CWYB | SHOULDER SHAPE | ROUND FIRST SHOULDER |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5754 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | PASSIVATE OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PWA586-1,FSCM 77445 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| THSD | THREAD SERIES DESIGNATOR | UNJF |
| Relevant Components for NSN - 5306-00-097-9405, 5306000979405 | ||||
| 5320-01-698-6474 (5320016986474) | 5340-01-449-6964 (5340014496964) | 5365-01-305-8613 (5365013058613) | 5310-01-623-8974 (5310016238974) | |
| 5320-01-540-4126 (5320015404126) | 5340-00-589-5330 (5340005895330) | 5330-01-519-6558 (5330015196558) | 5340-01-699-9823 (5340016999823) | |
| 5330-01-702-9229 (5330017029229) | 5330-01-182-5228 (5330011825228) | 5365-00-488-3930 (5365004883930) | 5340-01-297-4136 (5340012974136) | |
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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