Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number 305-415-804-0, a General Electric Company item that is listed alongside the description “Blade Turbine Rotor Aircraft Gas” and the NSN 2840013715782. To guarantee a swift procurement process for NSN part number 305-415-804-0, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number 305-415-804-0 is manufactured by General Electric Company, it is specifically done so under CAGE Code 07482, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 2840-01-371-5782, one can also determine that this part falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-371-5782 Item PartTypeName: BLADE,TURBINE ROTOR,AIRCRAFT GAS | 2840 | 013715782 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 305-415-804-0 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 4.000 INCHES NOMINAL |
| APGF | DESIGN TYPE | COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | LOCK |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE ASSY-LPT RTR STG 1 |
| CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
| AGAV | END ITEM IDENTIFICATION | F108 AIRCRAFT ENGINE |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14,FIG FIN 72-54-00-9 IND 525 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| FEAT | SPECIAL FEATURES | MATERIAL INCONEL 100 |
| CZCJ | STAGE NUMBER | 1 |
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