You have arrived on the Request for Quote (RFQ) page for part number 6003T87G01, a General Electric Company component that is listed with the product description “Sump Oil Aircraft Gas Turbine En” and NSN 2840-00-855-5799 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside General Electric Company part number 6003T87G01, you can seamlessly search for more items from this manufacturer or CAGECode 99207 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, which this component falls under having the NSN 2840-00-855-5799. Whether you desire part number 6003T87G01 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
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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