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 9184M63G05, a Frame Turbine Aircraft Gas Turbine Engine item that is manufactured by General Electric Company. Listed alongside the NSN 2840014347020 within our database, part number 9184M63G05 is conveniently ready for purchase at any time.
To ensure listings like part number 9184M63G05 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 2840-01-434-7020, as well as the many other General Electric Company products produced under CAGE Code 07482 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.
MRC | Criteria | Characteristic |
---|---|---|
FEAT | Special Features | 6TURBINE MID FRAME ASSY; NEW FRAME TO REDUCE NUMBER OF LINER SADDLE AND BLIPPER CRACKS; G10 FRAME HAS NEW LINER, 1820M83G01, WHICH INCORPORATES A REDESIGNED BLIPPER, HIGHER IN STRENGTH/TEMPERATURE; INTERGAL WITH THE LINER FOWARD OUT RING INSTEAD OF BEING WELDED TO THE RING AS OF NOW; TURBINE MID FRAME NOT AFFECTED IN PHYSICAL INTERCHANGEABILITY; NEW LINER AND CURRENT LINER ARE PHYSICALLY INTERCHANGEABLE; FUNCTIONAL INTERCHANGEABILITY IS AFFECTED IN THAT THE NEW LINER HAS HIGHER STRENGTH/TEMPERATURE |
RDAL | Reference Data And Literature | T.O. 2J-TF39-4, FIG 63 IND 1 |
ABHP | Overall Length | 13.165 INCHES MINIMUM AND 13.205 INCHES MAXIMUM |
CRTL | Criticality Code Justification | ABHP AND ABKV AND FEAT |
AGAV | End Item Identification | TF-39 AIRCRAFT GAS TURBINE ENGINE |
ABKV | Outside Diameter | 16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM |
MATT | Material | NICKEL ALLOY |
MRC | Decoded Requirement | Clear Text Reply |
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