Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Blade Compressor Aircraft Gas Tu items. You have expressed particular interest in part number 576712, a United Technologies Corporation component we offer that is presented with the NSN 2840-00-927-2618 for straightforward identification and procurement. By completing and submitting the Request for Quote form provided on this page, you can obtain pricing details on this NSN part for your comparisons. Once our staff members receive and review your submitted information, a dedicated account manager will directly contact you with a response within 15 minutes or less.
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We strive to streamline the purchasing process and simplify it as much as possible, which includes providing detailed listings for all components to help customers pinpoint their exact needs. For instance, part number 576712 is manufactured by United Technologies Corporation under the CAGE Code 77445. Additionally, by using the initial digits of the NSN 2840-00-927-2618, you can discover that this component is associated with the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. If you have any specific questions about our database, you may always give us a call or email, as we would be delighted to assist you however we can. Otherwise, we encourage you to secure a quote for part number 576712 at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-927-2618 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 009272618 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
576712 | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 1.944 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 0.834 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.415 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | TF30 AIRCRAFT 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 | NICKEL ALLOY BLADE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1003 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
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