Thank you for your interest in Embraer Sa part number 2010233, a Bolt Machine product we carry that is featured with the NSN 5306-00-150-9105. This component is ready for purchase at any time, so you are encouraged to complete the Request for Quote (RFQ) form provided below if you would like to obtain pricing information for your consideration. All we ask is that you supply us with essential details like desired item quantities, target price, and when fulfillment is expected, as this will ensure our response caters to any distinct specifications.
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At ASAP Semiconductor, our goal is to make the process of finding and securing precise components simple, which is why we present vital listing details with each offering here on Boundless Aerospace. For instance, part number 2010233 was manufactured by Embraer Sa under the CAGECode 001JK, and with the NSN 5306-00-150-9105, it belongs to FSC 5306 Bolts. More than that, all our inventory is delivered with any pertinent qualifying certifications or manufacturer trace documentation for your further benefit. Bearing all of this in mind, be sure to request a quote for part number 2010233 today, and we will be in touch as soon as possible.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5306-00-150-9105 Item PartTypeName: BOLT,MACHINE | 5306 | 001509105 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 5306-00-150-9105 | 2 | 9 | 6 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASA | THREAD LENGTH | 0.438 INCHES MINIMUM AND 0.516 INCHES MAXIMUM |
| AASB | FASTENER LENGTH | 0.516 INCHES MINIMUM AND 0.562 INCHES MAXIMUM |
| AASK | HEAD STYLE | HEXAGON |
| AASU | HEAD HEIGHT | 0.140 INCHES MINIMUM AND 0.172 INCHES MAXIMUM |
| AATB | WIDTH BETWEEN FLATS | 0.428 INCHES MINIMUM AND 0.440 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | B-1 SUPPORT EQUIPMENT;SOF AIRCRAFT;TF-33 ENGINE;PHOENIX MISSILE;HARPOON MISSILE;TF-56 ENGINE;AIRCRAFT,C-2A (REPROCURED);ENGINE,AIRCRAFT,TF-33-P-7 |
| AHYM | NOMINAL THREAD DIAMETER | 0.250 INCHES |
| ANEE | GRIP LENGTH | 0.046 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
| CBBL | FEATURES PROVIDED | FINISHED HEAD |
| CMLP | THREAD QUANTITY PER INCH | 28 |
| CQBC | MINIMUM TENSILE STRENGTH | 125000 POUNDS PER SQUARE INCH |
| CQFM | HARDNESS RATING | 26.0 ROCKWELL C MINIMUM OVERALL AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| MATT | MATERIAL | STEEL COMP 4140 OVERALL OR STEEL COMP 8740 OVERALL OR STEEL COMP 8630 OVERALL OR STEEL COMP 8735 OVERALL OR STEEL COMP 4130 OVERALL OR STEEL COMP 4037 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5626 MIL SPEC 1ST MATERIAL RESPONSE OVERALL OR MIL-S-6049 MIL SPEC 2ND MATERIAL RESPONSE OVERALL OR MIL-S-6050 MIL SPEC 3RD MATERIAL RESPONSE OVERALL OR MIL-S-6098 MIL SPEC 4TH MATERIAL RESPONSE OVERALL OR MIL-S-6758 MIL SPEC 5TH MATE |
| SFTT | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMATE OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-16,TY2,CL3 FED SPEC ALL TREATMENT RESPONSES OVERALL |
| THSD | THREAD SERIES DESIGNATOR | UNF |
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