Thank you for taking interest in the General Electric Company part number 9184M63G06, a Frame Turbine Aircraft Gas Turbi product that we stock that is presented alongside the NSN 2840-01-445-0387 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 9184M63G06 specifically traces back to General Electric Company through the CAGE Code 07482, a distinct identifier for one of their physical locations. Moreover, with the NSN 2840-01-445-0387, this listing falls within Federal Supply Code (FSC) 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 9184M63G06 here on Aero OEM Parts at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-445-0387 Item PartTypeName: FRAME,TURBINE,AIRCRAFT GAS TURBI | 2840 | 014450387 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
9138M62 | 2 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 13.165 INCHES MINIMUM AND 13.205 INCHES MAXIMUM |
ABKV | OUTSIDE DIAMETER | 16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABKV AND FEAT |
FEAT | SPECIAL FEATURES | DCN 97-4, CID 407635; ITEM INTRODUCES A NEW TURBINE MID FRAME ASSEMBLY INCORPORATING A TBC MID FRAME AND WASPALOY BOLTS; REPLACES P/N 9138M62G10 |
MATT | MATERIAL | NICKEL ALLOY |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF39-4, FIG 63, IND 1 |
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