Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 1476M11P02, a General Electric Company item with the NSN 2840013719462 that is listed alongside the description “Blade Fan Aircraft Gas Turbine E.” If you are interested in part number 1476M11P02 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 1476M11P02 is specifically listed with the NSN 2840-01-371-9462, and this code can be used to determine that it falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, while tracing back to General Electric Company, this NSN part was specifically produced under CAGE Code 07482. With our services and dedication to simple procurement in mind, get started with us today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-371-9462 Item PartTypeName: BLADE,FAN,AIRCRAFT GAS TURBINE E | 2840 | 013719462 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1476M11P02 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | OVERALL WIDTH | 3.098 INCHES MINIMUM AND 3.102 INCHES MAXIMUM |
| ABMZ | DIAMETER | 18.924 INCHES MAXIMUM |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | MATL TITANIUM; STAGE 1; SLOT BLADE ATTACHMENT METHOD |
| MATT | MATERIAL | TITANIUM ALLOY OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-F110-14 |
| ABHP | OVERALL LENGTH | 11.348 INCHES MINIMUM AND 11.358 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT ENGINE |
| CZBJ | ENGINE SECTION LOCATION | FAN |
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