| Part Number: 1476M11P02 | Manufacturer: General Electric Company |
| NSN : 2840-01-371-9462 (2840013719462) | Item Name : blade fan aircraft gas turbine e |
| CAGE Code: 07482 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-371-9462 Item Description: Blade Fan Aircraft Gas Turbine E | 2840 | 013719462 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1476m11p02 | 3 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 11.348 INCHES MINIMUM AND 11.358 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 3.098 INCHES MINIMUM AND 3.102 INCHES MAXIMUM |
| ABMZ | DIAMETER | 18.924 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CZBJ | ENGINE SECTION LOCATION | FAN |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | MATL TITANIUM; STAGE 1; SLOT BLADE ATTACHMENT METHOD |
| MATT | III MATERIAL | TITANIUM ALLOY OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-F110-14 |
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