Thank you for your interest in NSN part number YTM238 under NSN 3120001681473 on Click Aerospace. Click Aerospace is a website owned and operated by ASAP Semiconductor, offering customers access to an unparalleled inventory of premium parts that cater to a variety of industries and applications. Bearing Plain Rod E is an item listed with the part number YTM238, and FSC 3120 Bearings Plain Unmounted and it is manufactured by Bell Helicopter Textron Inc having CAGE Code 97499. This item, alongside the rest of our listed NSN parts, is readily available for purchase through our website now. Get started on the purchasing process today by filling out and submitting an Instant RFQ as provided through our website. Once received, a member of our staff will reach out to you in 15 minutes or less to offer a personalized quote based on your individual needs.
Note : We will not share your information to any third parties.
Click Aerospace is a leading independent distributor of NSN part YTM238, and we can help you procure NSN components such as 3120001681473 and many more. The quality of our inventory is of the utmost importance to us, and thus we choose to only source our parts from global manufacturers like Bell Helicopter Textron Inc. Get started with a competitive quote today when you submit an Instant RFQ and experience how we are revolutionizing the parts procurement process.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
3120-00-168-1473 Item Description: Bearing Plain Rod E | 3120 | 001681473 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
Ytm238 | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 3A |
AAJF | THREAD DIRECTION | RIGHT-HAND |
AAZF | SHANK STYLE | EXTERNALLY THREADED |
ABHP | OVERALL LENGTH | 4.1970 INCHES MINIMUM AND 4.2270 INCHES MAXIMUM |
ABXV | BORE DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
AGGF | OUTER MEMBER OUTSIDE DIAMETER | 1.7900 INCHES MINIMUM AND 1.8100 INCHES MAXIMUM |
AGGG | BORE CENTER TO SHANK END DISTANCE | 3.3020 INCHES MINIMUM AND 3.3220 INCHES MAXIMUM |
AGGH | OUTER MEMBER WIDTH | 0.6250 INCHES MINIMUM AND 0.6350 INCHES MAXIMUM |
AGGJ | INNER MEMBER WIDTH | 0.9350 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
AGGY | SHANK THREAD LENGTH | 1.9900 INCHES MINIMUM AND 2.0300 INCHES MAXIMUM |
AWDP | THREAD DIAMETER | 0.562 INCHES NOMINAL |
CMLP | THREAD QUANTITY PER INCH | 18 |
CQFM | HARDNESS RATING | 36.0 ROCKWELL C MINIMUM ROD END BODY AND 39.0 ROCKWELL C MAXIMUM ROD END BODY |
FEAT | SPECIAL FEATURES | KEYWAY IN SHANK,0.125 IN. MIN 0.130 MAX W,0.0835 IN. MIN 0.0845 IN. MAX DEEP; 4 PUNCH LOCKS PER SIDE LOCATED ON 1.570 IN. DIA ON FACE OF ROD END BODY |
MATT | MATERIAL | PLASTIC TETRAFLUOROETHYLENE RACE LINER |
MATT | MATERIAL | STEEL COMP 416SE RACE INSERT |
MATT | MATERIAL | STEEL COMP 440C INNER LAYER |
MATT | MATERIAL | STEEL COMP 630 ROD END BODY |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5610 ASSN STD SINGLE MATERIAL RESPONSE RACE INSERT |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5643 ASSN STD SINGLE MATERIAL RESPONSE ROD END BODY |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-S-763 FED SPEC SINGLE MATERIAL RESPONSE INNER LAYER |
STYL | STYLE DESIGNATOR | BALL TYPE |
TEST | TEST DATA DOCUMENT | 81349-MIL-I-6866 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTIN |
THSD | THREAD SERIES DESIGNATOR | UNF |
Glad You Chose Click Aerospace as Your Parts Distributor Website today. We Hope that You Will Remember Us the Next Time You’re Looking for Required Parts.
Request for Quote
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”. |