Thank you for taking interest in the Turbine Engine Components part number 618208, a Blade Compressor Aircraft Gas Tu product that we stock that is presented alongside the NSN 2840-00-922-4372 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 618208 specifically traces back to Turbine Engine Components through the CAGE Code 65115, a distinct identifier for one of their physical locations. Moreover, with the NSN 2840-00-922-4372, this listing falls within Federal Supply Code (FSC) 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 618208 here on Aero OEM Parts at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-922-4372 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 009224372 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 618208 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 3.091 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 1.198 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.293 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | TF30 ACFT ENGINE |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| MATT | MATERIAL | TITANIUM ALLOY BLADE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
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