| Part Number: 4075608-02 | Manufacturer: United Technologies Corp |
| NSN : 2840-01-318-4791 (2840013184791) | 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 : 407560802 | INC Code: 50531 |
| NIIN : 01-318-4791 (013184791) | FSG : 28 Engines Turbines and Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-318-4791 Item Description: Blade Compressor Aircraft Gas Turbine Engine | 2840 | 013184791 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4075608-02 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | OVERALL WIDTH | 1.095 INCHES NOMINAL |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZCJ | STAGE NUMBER | 8 |
| MATT | III MATERIAL | NICKEL ALLOY BLADE |
| ABHP | OVERALL LENGTH | 2.176 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F100PW0229 ENGINE/CORE MOD |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| MATT | MATERIAL | NICKEL ALLOY BLADE |
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