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| 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) | 01-444-7012 (014447012) |
| NCB Code | USA (01) |
| Manufacturer | General Electric Company |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 1807M26G01 | general electric company | blade turbine rotor aircraft gas | RFQ |
| 1807M26 | general electric company | blade turbine rotor aircraft gas | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| CZCJ | Stage Number | 2 |
| MRC | Decoded Requirement | Clear Text Reply |
| CRTL | Criticality Code Justification | AGAV |
| ABHP | Overall Length | 4.891 INCHES NOMINAL |
| AGAV | End Item Identification | ACFT ENG TF39 |
| CZBJ | Engine Section Location | HIGH PRESSURE TURBINE |
| APGF | Design Type | AXIAL COMPRESSOR |
| MATT | Material | ALUMINUM BLADE |
| BGLW | Blade Attachment Method | FIR TREE |
| ABMK | Overall Width | 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM |
| FEAT | Special Features | MATERIAL EXTERNAL PLATINUM ALUMINIDE COATING, THIS IS PART OF THE HT90 MOD FOR THE TF39, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, TRAIL |
| Relevant Components for NSN - 2840-01-444-7012, 2840014447012 | ||||
| 2825-00-790-8901 (2825007908901) | 2825-01-010-8535 (2825010108535) | 2825-00-371-7811 (2825003717811) | 2805-01-264-5598 (2805012645598) | |
| 2840-01-375-6452 (2840013756452) | 2805-01-130-2594 (2805011302594) | 2835-01-234-6845 (2835012346845) | 2805-01-714-1073 (2805017141073) | |
| 2840-00-837-2120 (2840008372120) | 2840-01-708-1715 (2840017081715) | 2840-01-200-9553 (2840012009553) | 2805-00-710-5355 (2805007105355) | |
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