ASAP Semiconductor is an industry-leading distributor for shopping for parts by National Stock Number (NSN) data, the items featured within this catalog all falling under NSN 2840-01-434-7020 (2840014347020). Toward the top of this page, you will find several details that pertain to this NSN, allowing you to confirm various aspects of these offerings to ensure accurate procurement. Meanwhile, the part numbers that we have available for purchase can be found below, with Request for Quote (RFQ) links provided alongside each should you wish to make a purchase. Our team is also available by phone or email to support you during the procurement process, so never hesitate to take the first step with us.
| Alternative NSN: | 2840014347020 |
| Manufacturers | General Electric Company |
| Item Name | Frame Turbine Aircraft Gas Turbine Engine |
| INC Code | 52349 |
| Federal Supply Group (FSG) | 28 Engines Turbines and Components |
| Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| National Item Identification Number (NIIN) | 01-434-7020 (014347020) |
| NCB Code | USA (01) |
| Part No | Manufacturer | Item Name | CAGE Code | Type | Status | Availability | RFQ | |
|---|---|---|---|---|---|---|---|---|
| 9138M62G10 | general electric company | frame turbine aircraft gas turbine engine | 07482 | a | a | Avl | RFQ |
|
| 9184M63G05 | general electric company | frame turbine aircraft gas turbi | 07482 | a | a | Avl | RFQ |
|
| 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 |
| 2825-00-678-4380 (2825006784380) | 2810-00-165-5920 (2810001655920) | 2840-01-140-6738 (2840011406738) | 2840-00-881-4726 (2840008814726) |
| 2840-01-308-7038 (2840013087038) | 2835-01-546-0315 (2835015460315) | 2840-01-617-5330 (2840016175330) | 2825-00-086-8538 (2825000868538) |
| 2815-00-071-7953 (2815000717953) | 2840-01-589-1807 (2840015891807) | 2825-00-175-8805 (2825001758805) | 2810-00-310-5584 (2810003105584) |
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