If your operations demand dependable items that fall under the NSN 5306-00-693-6295, look no further than the expansive product list featured on this page. For your convenience, all NSN 5306-00-693-6295 part numbers that we have in stock like 2499199, 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 5306-00-693-6295 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 Eye |
| Federal Supply Group (FSG) | Hardware and Abrasives |
| Federal Supply Class (FSC) | 5306 Bolts |
| National Item Identification Number (NIIN) | 00-693-6295 (006936295) |
| NCB Code | USA (00) |
| Manufacturer | Boeing Company The |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASA | THREAD LENGTH | 0.312 INCHES MINIMUM AND 0.453 INCHES MAXIMUM |
| AATK | EYE INSIDE DIAMETER | 0.277 INCHES MINIMUM AND 0.290 INCHES MAXIMUM |
| AATP | SHOULDER THICKNESS | 0.062 INCHES NOMINAL |
| AATR | SHANK LENGTH | 1.015 INCHES MINIMUM AND 1.062 INCHES MAXIMUM |
| AATZ | EYE STOCK DIAMETER | 0.089 INCHES MINIMUM AND 0.099 INCHES MAXIMUM |
| AAUA | EYE STOCK THICKNESS | 0.094 INCHES NOMINAL |
| AAVH | SHOULDER DIAMETER | 0.438 INCHES NOMINAL |
| AAWB | SHANK UNTHREADED HOLE DIAMETER | 0.060 INCHES MINIMUM AND 0.080 INCHES MAXIMUM FIRST HOLE |
| ABHP | OVERALL LENGTH | 1.793 INCHES MINIMUM AND 1.816 INCHES MAXIMUM |
| AHYM | NOMINAL THREAD DIAMETER | 0.190 INCHES |
| CMLP | THREAD QUANTITY PER INCH | 32 |
| CQBC | MINIMUM TENSILE STRENGTH | 125000 POUNDS PER SQUARE INCH |
| CQFM | HARDNESS RATING | 26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| CRHT | DISTANCE FROM CENTER OF EYE TO SHANK END | 1.574 INCHES MINIMUM AND 1.597 INCHES MAXIMUM |
| CWXM | EYE OUTSIDE WIDTH | 0.438 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVY SPECIAL PROJECT |
| MATT | MATERIAL | STEEL COMP 4130 OR STEEL COMP 8630 OR STEEL COMP 8735 OR STEEL COMP 8740 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-6758 MIL SPEC 1ST MATERIAL RESPONSE OR MIL-S-6050 MIL SPEC 2ND MATERIAL RESPONSE OR MIL-S-6098 MIL SPEC 3RD MATERIAL RESPONSE OR MIL-S-6049 MIL SPEC 4TH MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | CADMIUM AND CHROMATE OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| STYL | STYLE DESIGNATOR | ROUND,CLOSED W/SHOULDER |
| THSD | THREAD SERIES DESIGNATOR | UNF |
| Relevant Components for NSN - 5306-00-693-6295, 5306006936295 | ||||
| 5315-01-193-2252 (5315011932252) | 5305-00-282-9451 (5305002829451) | 5340-01-151-8391 (5340011518391) | 5315-01-482-3431 (5315014823431) | |
| 5360-01-616-7828 (5360016167828) | 5340-00-680-3497 (5340006803497) | 5330-01-492-4379 (5330014924379) | 5310-01-705-5442 (5310017055442) | |
| 5365-01-648-1970 (5365016481970) | 5340-01-524-2523 (5340015242523) | 5340-01-265-3907 (5340012653907) | 5306-01-333-8059 (5306013338059) | |
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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