| Part Number: 4077512-02 | Manufacturer: United Technologies Corp |
| NSN : 2840-01-323-4296 (2840013234296) | 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 : 407751202 | INC Code: 50531 |
| NIIN : 01-323-4296 (013234296) | FSG : 28 Engines Turbines and Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-323-4296 Item Description: BLADE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE | 2840 | 013234296 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4077512-02 | 3 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.467 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 0.811 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 12 |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-54 |
| MATT | III MATERIAL | NICKEL ALLOY BLADE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1005 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
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