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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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