Thank you for taking interest in the Boeing Company The part number 3D0206-1, a Pushonnut product that we stock that is presented alongside the NSN 5310-01-534-6813 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 3D0206-1 specifically traces back to Boeing Company The through the CAGE Code 88277, a distinct identifier for one of their physical locations. Moreover, with the NSN 5310-01-534-6813, this listing falls within Federal Supply Code (FSC) 5310 Nuts and Washers, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 3D0206-1 here on Aero OEM Parts at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5310-01-534-6813 Item PartTypeName: PUSH ON NUT | 5310 | 015346813 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 15S11-1AF | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASTM A109 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ACSZ | MATING MEMBER DIAMETER ACCOMMODATED | 0.295 INCHES MINIMUM AND 0.305 INCHES MAXIMUM |
| ACTA | NUT STYLE | PUSH ON |
| ACTD | NUT DIAMETER | 0.500 INCHES MINIMUM AND 0.520 INCHES MAXIMUM |
| MATT | MATERIAL | STEEL COMP 1137 OVERALL |
| AGAV | III END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| ABPX | MATERIAL THICKNESS | 0.007 INCHES MINIMUM AND 0.013 INCHES MAXIMUM |
| SFTT | SURFACE TREATMENT | CADMIUM OVERALL |
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