Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 9138M62G10, which you have taken interest in. This Frame Turbine Aircraft Gas Turbine Engine item is listed alongside the NSN 2840-01-434-7020 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 9138M62G10 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from General Electric Company under CAGE Code 07482, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-434-7020 part number 9138M62G10 today, knowing we will support all your operational needs with care.
| 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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