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NSN 3120-01-215-9842 (3120012159842) Bushing Sleeve Parts Catalog

The part belongs to NSN 3120-01-215-9842 is an Bushing Sleeve produced by Rbc Transport Dynamics, General Electric Company. This specific NSN is a numeric identifier assigned by the Defense Logistics Agency (DLA) to categorize all products distributed by the NATO federal supply chain. At ASAP AOG, a company owned and operated by ASAP Semiconductor, we possess parts that belong to the NSN 3120-01-215-9842 and these are readily available in our current inventory. Our on-hand inventory contains parts belonging to this particular NSN that you can easily access. So, if you need an Bushing Sleeve made by Rbc Transport Dynamics, General Electric Company that carries the NSN 3120-01-215-9842, you can rely on us to provide you with the necessary parts from our available inventory.


At ASAP AOG, we are dedicated to providing competitive quotes for premium NATO parts. We work hard to ensure all the national stock number 3120012159842 parts are fully certified and up to standard. Our supply chain is extensive and one of the fastest in the industry. Have a question or need a quote today? Simply fill out the RFQ below.


Alternative NSN: 3120-01-215-9842
Item Name: Bushing Sleeve
FSG: 31 Bearings
Federal Supply Class (FSC): 3120 Bearings Plain Unmounted
NCB Code: USA (01)
Manufacturers: General Electric Company, Rbc Transport Dynamics

Manufacturer’s List for NSN 3120-01-215-9842

general electric company rbc transport dynamics

Part Number's List for NSN 3120-01-215-9842

Part No.
Manufacturer
Item Name
Availability
RFQ

Technical Characteristics of NSN 3120012159842

MRCCriteriaCharacteristic
ABHPOVERALL LENGTH0.2180 INCHES MINIMUM AND 0.2620 INCHES MAXIMUM
ADARBODY OUTSIDE DIAMETER0.3720 INCHES MINIMUM AND 0.3730 INCHES MAXIMUM
ADASBODY INSIDE DIAMETER0.2640 INCHES MINIMUM AND 0.2660 INCHES MAXIMUM
AEPRFLANGE OUTSIDE DIAMETER0.4800 INCHES MINIMUM AND 0.5200 INCHES MAXIMUM
AGAVEND ITEM IDENTIFICATIONENGINE, AIRCRAFT, F110-GE-100/129 (F-16 C/D); ENGINE, F118-GE-100 (B-2 BOMBER); ENGINE, AIRCRAFT, F-108 (CFM-56, KC-135A)
AGFFFLANGE WIDTH0.0280 INCHES MINIMUM AND 0.0320 INCHES MAXIMUM
BZLXCORNER SHAPECHAMFERED INSIDE RIGHT CORNER
BZLXCORNER SHAPESQUARE INSIDE LEFT CORNER
BZLXCORNER SHAPESQUARE LEFT FLANGE BODY CORNER
BZLXCORNER SHAPESQUARE LEFT FLANGE OUTSIDE RIGHT CORNER
BZLXCORNER SHAPESQUARE OUTSIDE LEFT CORNER
BZLXCORNER SHAPESQUARE OUTSIDE RIGHT CORNER
CSYMSURFACE FINISH63.0 MICROINCHES INSIDE DIAMETER SURFACE OF BODY
CSYMSURFACE FINISH63.0 MICROINCHES LEFT END SURFACE OF BODY AND FLANGE
CSYMSURFACE FINISH63.0 MICROINCHES OUTSIDE DIAMETER SURFACE OF BODY
CSYMSURFACE FINISH63.0 MICROINCHES RIGHT END SURFACE OF LEFT FLANGE
MATTMATERIALPLASTIC POLYAMIDE INNER LAYER AND GLASS FIBER INNER LAYER AND RESIN SYNTHETIC INNER LAYER
MATTMATERIALSTEEL COMP 630 OUTER LAYER
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONAMS 5643 ASSN STD SINGLE MATERIAL RESPONSE OUTER LAYER
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONFABROID X,FSCM 09455 MFR REF SINGLE MATERIAL RESPONSE INNER LAYER
STYLSTYLE DESIGNATORSOLID, EXTERNAL FLANGE ONE END