| Item Name | Blade Turbine Rotor Aircraft Gas |
| Federal Supply Group (FSG) | Engines Turbines and Components |
| Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| National Item Identification Number (NIIN) | 01-444-7701 (014447701) |
| NCB Code | USA (01) |
| Manufacturer | General Electric Company |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 1807M24 | general electric company | blade turbine rotor aircraft gas | 07482 | RFQ |
| 1807M24G01 | general electric company | blade turbine rotor aircraft gas | 07482 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 5.388 INCHES MINIMUM AND 5.400 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF39 |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | FIR TREE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 2 |
| FEAT | SPECIAL FEATURES | THIS ITEM IS PART OF THE HT90 MODFOR THE TF39 ENGINE, EXTERNAL COATING PLATINUM ALUMINIDE, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, LEAD |
| MATT | III MATERIAL | ALUMINUM BLADE |
| Relevant Components for NSN - 2840-01-444-7701, 2840014447701 | ||||
| 2805-00-371-7568 (2805003717568) | 2835-00-626-9669 (2835006269669) | 2840-00-939-3493 (2840009393493) | 2840-01-321-1442 (2840013211442) | |
| 2825-00-309-1763 (2825003091763) | 2835-00-682-5353 (2835006825353) | 2815-00-139-3970 (2815001393970) | 2840-00-866-1571 (2840008661571) | |
| 2840-01-674-1631 (2840016741631) | 2840-01-310-6208 (2840013106208) | 2815-01-690-0888 (2815016900888) | 2835-01-177-9984 (2835011779984) | |
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