Thank you for considering General Electric Company part number 9138M62G12, an item we carry that is listed with the NSN 2840-01-445-0387 and product description “Frame Turbine Aircraft Gas Turbi.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 9138M62G12 was specifically produced by General Electric Company under CAGE Code 07482, and with the NSN 2840-01-445-0387, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 9138M62G12 today, knowing we will be in touch shortly after reviewing your information.
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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