| Part Number: 4077509 02 | Manufacturer: United Technologies Corp |
| NSN : 2840-01-323-5914 (2840013235914) | Item Name : blade compressor aircraft gas turbine engine |
| CAGE Code: 77445 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| Alternate P/N : 407750902 | INC Code: 50531 |
| NIIN : 01-323-5914 (013235914) | FSG : 28 Engines Turbines and Components |
| Country: USA | NCB Code: 01 |
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| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.020 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 0.938 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | FIR TREE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 9 |
| MATT | III MATERIAL | NICKEL ALLOY BLADE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1010 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
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