Using the Request for Quote (RFQ) form provided on this page, you can request competitive procurement options on part number 209-040-110-3 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 209-040-110-3 It is listed as Stud Plain. component manufactured by Bell Helicopter Textron Inc, specifically under CAGE Code 97499. It is also accompanied by the NSN 5307010523572 for ease of organization, the first digits of the NSN indicating that the part belongs to FSC 5307 Studs.
NSN Information for Part Number 209-040-110-3 with NSN 5307-01-052-3572, 5307010523572
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5307-01-052-3572 Item Description: Stud Plain | 5307 | 010523572 | 0 | N | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
209-040-110-3 | 5 | 2 | 3 |
Characteristics Data of NSN 5307-01-052-3572, 5307010523572
MRC | Criteria | Characteristic |
---|---|---|
AAJF | THREAD DIRECTION | RIGHT-HAND NUT THREAD |
AASA | THREAD LENGTH | 0.875 INCHES MINIMUM AND 1.018 INCHES MAXIMUM STUD THREAD |
ADDU | DISTANCE FROM COTTER PIN HOLE CENTERLINE TO NUT END | 0.186 INCHES NOMINAL FIRST HOLE |
ADDV | COTTER PIN HOLE DIAMETER | 0.106 INCHES MINIMUM AND 0.116 INCHES MAXIMUM FIRST HOLE |
CQFM | HARDNESS RATING | 36.0 ROCKWELL C MINIMUM AND 40.0 ROCKWELL C MAXIMUM |
CQJX | NOMINAL THREAD SIZE | 0.438 INCHES STUD THREAD |
CSYM | SURFACE FINISH | 63.0 MICROINCHES STUD THD |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVY SPECIAL PROJECT |
THSD | THREAD SERIES DESIGNATOR | UNC STUD THREAD |
AAJD | THREAD CLASS | 3A NUT THREAD |
ABHP | OVERALL LENGTH | 1.990 INCHES MINIMUM AND 2.010 INCHES MAXIMUM |
CMLP | THREAD QUANTITY PER INCH | 14 STUD THREAD |
MATT | MATERIAL | STEEL COMP E4340 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5000 MIL SPEC SINGLE MATERIAL RESPONSE |