| Part Number: 183089 | Manufacturer: American Aircraft Parts Mfg Co | NSN: 5310-00-208-6344 (5310002086344) |
| Item Name : nut plain round | CAGE Code: 99106 | FSC : 5310 Nuts and Washers |
We currently have Part Number 183089 with NSN 5310002086344 in stock. This component is manufactured by American Aircraft Parts Mfg Co under CAGE Code 99106 and described as Nut Plain Round..
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With over 100 million parts sold, we are among the reputed independent distributors within the United States. Sourcingstreamlined.com has over 26 different distinct federal supply code categories, with more than 10 million national stock numbers from 5,000 leading manufacturers.
A national stock number, also known as an NSN, part bears an official label indicating its procurement, storage, and stocking within the Federal supply system. NSN parts are an essential part of the military and defense logistics supply chain and can have multiple part numbers under it depending on whether it has multiple manufacturers for the same part. Part number 183089 belongs to the Federal Supply Group 5310 Nuts And Washers.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5310-00-208-6344 Item Description: Nut Plain Round | 5310 | 002086344 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 183089 | 6 | 2 | 5 |
| 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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