Thank you for taking interest in General Electric Company part number 9184M63G05, which is listed with the NSN 2840-01-434-7020 and a product description of “Frame Turbine Aircraft Gas Turbine Engine.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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| 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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