| Alternative NSN: 5310-00-208-6344 |
| Item Name: Nut Plain Round |
| FSG: 53 Hardware and Abrasives |
| Federal Supply Class (FSC): 5310 Nuts and Washers |
| NIIN: 002086344 |
| NCB Code: USA (00) |
| Manufacturers: American Aircraft Parts Mfg Co , United Technologies Corp |
Veritable Aviation, owned and operated by ASAP Semiconductor, makes the parts procurement process for NSN 5310-00-208-6344 as streamlined as possible. Our easy to use search engine opens up our 6-billion-part inventory open to our loyal customers. Simply type in a part number such as 183089 or NSN 5310-00-208-6344 and receive a quote within fifteen minutes or less from one of our dedicated account managers. We work with well-known industry names American Aircraft Parts Mfg Co, United Technologies Corp.
We are dedicated to providing only the best products under NSN 5310-00-208-6344 through our quality assurance practices, earning us our FAA-AC 0056B accreditation and ISO 9001:2015 certification. To get your parts procurement process started, fill out the request for quote form below.
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| 183089 | American Aircraft Parts Mfg Co | nut plain round | Avl | RFQ |
| 183089 | United Technologies Corp | nut plain round | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 2B |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| ABQU | DRIVE POINT DEPTH | 0.105 INCHES NOMINAL |
| ACTA | NUT STYLE | ROUND |
| ACTD | NUT DIAMETER | 4.532 INCHES NOMINAL |
| ADBG | NUT THICKNESS | 0.440 INCHES NOMINAL |
| ADBH | DRIVE POINT WIDTH | 0.562 INCHES NOMINAL |
| ADBM | DRIVE POINT QUANTITY | 16 |
| AGGP | DRILLED HOLE DIAMETER | 0.156 INCHES NOMINAL |
| ALET | HOLE TYPE AND QUANTITY | 16 DRILLED |
| BZRR | THREAD SERIES | UNS |
| CMLP | THREAD QUANTITY PER INCH | 16 |
| CQJX | NOMINAL THREAD SIZE | 4.188 INCHES |
| CRHC | HOLE CONFIGURATION STYLE | CONFIGURATION F |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| FEAT | SPECIAL FEATURES | IAW TF33 ENGINEERING DIRECTIVE. AN INTERNAL PARTS FAILURE COULD CAUSE CATASTROPHIC OR CRITICAL FAILURE RESULTING IN LOSS OF AIRCRAFT OR ENGINE SHUTDOWN |
| MATT | MATERIAL | STEEL COMP 8740 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6322 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
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