Thank you for considering General Electric Company part number 4007T78G07, an item we carry that is listed with the NSN 2840-01-268-2008 and product description “Frame Compressor Aircraft Gas Tu.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 4007T78G07 was specifically produced by General Electric Company under CAGE Code 99207, and with the NSN 2840-01-268-2008, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 4007T78G07 today, knowing we will be in touch shortly after reviewing your information.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-268-2008 Item PartTypeName: FRAME,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 012682008 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4007T78G08 | 3 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 4.427 INCHES MINIMUM AND 4.431 INCHES MAXIMUM |
| ABKV | OUTSIDE DIAMETER | 16.995 INCHES MINIMUM AND 17.005 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | J85-GE-21B AIRCRAFT GAS TURBINE ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABKV |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | MAINFRAME AND BRACKET ASSY |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-J85-94 FIG 11 IND 1 OR FIG 3 IND 13 |
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