| Part Number: 111R115P21 | Manufacturer: Blades Technology Ltd |
| NSN : 2840-01-106-2602 (2840011062602) | Item Name : blade compressor aircraft gas tu |
| CAGE Code: S0635 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NIIN : 01-106-2602 (011062602) | FSG : 28 Engines Turbines and Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-106-2602 Item Description: Blade Compressor Aircraft Gas Tu | 2840 | 011062602 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 111r115p21 | 2 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.843 INCHES MINIMUM AND 1.845 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 0.713 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 17 |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| MATT | III MATERIAL | STEEL BLADE |
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