| Mfg Part Number: 9184M63G05 | Manufacturer: General Electric Company |
| NSN : 2840-01-434-7020 | NIIN : 014347020 |
| Item Name : frame turbine aircr | CAGE Code : 07482 |
| FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your interest in our available 9184M63G05 NSN part. This part number 9184M63G05 is a Frame Turbine Aircr listed under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, and it is manufactured by General Electric Company. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
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Internet of Components is a premier supplier of 9184M63G05 NSN component, and we carry recently requested NSN components such as 2840014347020. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as General Electric Company. If you are interested in this particular item, we invite you to begin the purchasing process for 9184M63G05 today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-434-7020 Item Description: FRAME,TURBINE,AIRCRAFT GAS TURBINE ENGINE | 2840 | 014347020 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9184M63G05 | 2 | 2 | 5 |
| 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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