Using the Request for Quote (RFQ) form provided on this page, you can request competitive procurement options on part number 183089 with rapid responses always offered by our staff. To ensure that you locate and procure exactly what you need with ease, we list parts with as much information as we can. For example, part number 183089 It is listed as Nut Plain Round. component manufactured by American Aircraft Co Inc, specifically under CAGE Code 99106. It is also accompanied by the NSN 5310002086344 for ease of organization, the first digits of the NSN indicating that the part belongs to FSC 5310 Nuts and Washers.
NSN Information for Part Number 183089 with NSN 5310-00-208-6344, 5310002086344
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 |
Characteristics Data of NSN 5310-00-208-6344, 5310002086344
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 2B |
ABQU | DRIVE POINT DEPTH | 0.105 INCHES NOMINAL |
ACTD | NUT DIAMETER | 4.532 INCHES NOMINAL |
ADBH | DRIVE POINT WIDTH | 0.562 INCHES NOMINAL |
ADBM | DRIVE POINT QUANTITY | 16 |
BZRR | THREAD SERIES | UNS |
CMLP | THREAD QUANTITY PER INCH | 16 |
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 |
AAJF | THREAD DIRECTION | RIGHT-HAND |
ACTA | NUT STYLE | ROUND |
ADBG | NUT THICKNESS | 0.440 INCHES NOMINAL |
AGGP | DRILLED HOLE DIAMETER | 0.156 INCHES NOMINAL |
ALET | HOLE TYPE AND QUANTITY | 16 DRILLED |
CQJX | NOMINAL THREAD SIZE | 4.188 INCHES |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6322 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |