NSN 5310-00-208-6344 of Nut Plain Round - Parts Details
| Alternative NSN: 5310002086344 |
| 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 Co Inc , United Technologies Corporation |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers 183089 under NSN 5310-00-208-6344 of Nut Plain Round manufactured by American Aircraft Co Inc, United Technologies Corporation.
Federal Supply Class of NSN 5310-00-208-6344 is FSC 5310 contains part details of Nuts and Washers. Quote for your desired part numbers.
Part Number's List for NSN 5310-00-208-6344, 5310002086344
Characteristics Data of NSN 5310002086344MRC 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
| 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 |