Thank you for taking an interest in the top-caliber NSN products we feature here on AI NSN Parts. On this page, you can submit a quote request for part number 6003T87G01, a Sump Oil Aircraft Gas Turbine En item that is manufactured by Kerns Manufacturing Corp. Listed alongside the NSN 2840008555799 within our database, part number 6003T87G01 is conveniently ready for purchase at any time.
To ensure listings like part number 6003T87G01 are ready for swift installation, we have a rigorous quality assurance program in place. As such, we make it easy for you to inquire about popular NSNs like 2840-00-855-5799, as well as the many other Kerns Manufacturing Corp products produced under CAGE Code 93596 that interest you. For the benefit of our customers, we carefully vet every entity that we source from, guaranteeing that you only receive superior-caliber offerings in every order. With these dedications, you can always purchase from us with confidence. Furthermore, we also organize our stock based on Federal Supply Classes, so you can find popular items under FSCs like 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Do not hesitate to submit the RFQ form below, and within 15 minutes or less of submission, one of our experts will reach out with a customized solution. Get started today and see why so many customers steadily depend on AI NSN Parts for their operational needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-855-5799 Item PartTypeName: SUMP,OIL,AIRCRAFT GAS TURBINE EN | 2840 | 008555799 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
6003T87G01 | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 2.868 INCHES MINIMUM AND 2.872 INCHES MAXIMUM |
ABMZ | DIAMETER | 6.300 INCHES NOMINAL |
CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABPX AND ABMZ AND FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SUMP,FRONT FRAME |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
ABPX | MATERIAL THICKNESS | 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | J85-GE-21/21A/21B AIRCRAFT GAS TURBINE ENGINE |
FEAT | SPECIAL FEATURES | T.O. 2J-J85-94,FIG 7,IND 28; 2ND END DIA. 5.560 |
MATT | MATERIAL | ALUMINUM OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4117 ASSN STD 1ST MATERIAL RESPONSE OVERALL OR AMS4065 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
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