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 | ||||
| 2805-01-240-6126 (2805012406126) | 2805-00-262-7518 (2805002627518) | 2815-01-248-8775 (2815012488775) | 2840-01-596-5492 (2840015965492) | |
| 2805-01-066-5405 (2805010665405) | 2840-01-617-3491 (2840016173491) | 2815-01-127-3597 (2815011273597) | 2805-01-066-4028 (2805010664028) | |
| 2825-00-025-9691 (2825000259691) | 2825-00-992-0632 (2825009920632) | 2815-00-361-9922 (2815003619922) | 2840-01-653-5046 (2840016535046) | |
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