AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| Item Name | Blade Compressor Aircraft Gas Tu |
| 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) | 00-927-2618 (009272618) |
| NCB Code | USA (00) |
| Manufacturer | United Technologies Corporation, Turbine Engine Components, Airfoil Textron Inc |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.944 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 0.834 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.415 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| MATT | MATERIAL | NICKEL ALLOY BLADE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1003 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| Relevant Components for NSN - 2840-00-927-2618, 2840009272618 | ||||
| 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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