You have reached this page because of your interest in the Sump Oil Aircraft Gas Turbine En NSN parts we have available on NSN Domain. Here, you can submit a quote request for Kerns Manufacturing Corp part number 6003T87G01, a component that can be located by searching for NSN 2840-00-855-5799 in our database. Apart from part number 6003T87G01, we also have an array of others, including military, defense, and aerospace parts that have been sourced from a wide range of trusted manufacturers on our Approved Vendor List (AVL). With this in mind, we invite you to explore our ever-expanding catalogs for in-demand items according to manufacturer, NSN, NIIN, and more.
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NSN Domain works with numerous government and defense agencies, so we take advantage of CAGE Codes like 93596 to uniquely identify items in a standardized manner. Moreover, we organize our stock according to various Federal Supply Classes (FSC), ensuring customers can find Kerns Manufacturing Corp part number 6003T87G01, which can be found under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease. On that note, please complete the form below for NSN 2840-00-855-5799 and/or any others so we can see how we can find a solution to your needs. For a hands-on approach, call or email us at any time; our experts are on standby 24/7x365!
| 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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