Buy Mil Spares is your sourcing solution for top-quality military and defense parts, aerospace parts, and other similar products that are necessary for operational fulfillment. You have reached the RFQ page for part number 9184M63G05, a Frame Turbine Aircraft Gas Turbine Engine item that is listed with the NSN 2840-01-434-7020 for an ease of identification. Manufactured by General Electric Company and readily available for procurement today, you are always welcome to request a quote on this NSN part to receive tailored pricing information and fulfillment options from our team. Simply offer us important information like your desired quantity, price, and fulfillment timeframe, and our team will supply you with a tailored quote on part number 9184M63G05 in 15 minutes or less.
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To ensure that customers quickly identify and procure exact items, we list everything with as much relevant information as possible. For example, while part number 9184M63G05 is manufactured by General Electric Company, it is specifically done so under CAGE Code 07482, a unique identifier assigned to a specific facility by the DLA that supplies to various government or defense agencies. Furthermore, using the first digits of the NSN 2840-01-434-7020, one can also determine that this part falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. With this in mind, continue exploring our website today, and see how we can help you secure competitive pricing and rapid lead times on all desired NSN parts.
| 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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