Thank you for your interest in part number 9138M62G10, a component manufactured by General Electric Company that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 2840-01-434-7020 and features the description “Frame Turbine Aircraft Gas Turbine Engine.” To request a quote for part number 9138M62G10, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 2840-01-434-7020 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from General Electric Company, which is associated with the CAGECode 07482. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components part number 9138M62G10.
| 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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