Aerospace Engineering Solutions is proud to offer immediate purchasing options on United Technologies Corporation part number 4082943CLR, a Nozzle Turbine Aircraft Gas Turbine Engine product we carry that is listed with the NSN 2840-01-445-5374 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to United Technologies Corporation through the CAGE Code 77445, as well as categorized under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components based on the first four digits of the NSN 2840-01-445-5374. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 4082943CLR and other NSN items of need.
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM" |
| ABKW | OVERALL HEIGHT | 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM" |
| ABMK | OVERALL WIDTH | 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE" |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR" |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABMK AND ABHP AND ABKW AND FEAT AND CZCJ" |
| CZBJ | ENGINE SECTION LOCATION | TURBINE" |
| CZCJ | STAGE NUMBER | 3" |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-14, FIG 132; FLOW AREA 4.689-4.714" |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL" |
| ABHP | OVERALL LENGTH | 2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM" |
| ABKW | OVERALL HEIGHT | 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM" |
| ABMK | OVERALL WIDTH | 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE" |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR" |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABMK AND ABHP AND ABKW AND FEAT AND CZCJ" |
| CZBJ | ENGINE SECTION LOCATION | TURBINE" |
| CZCJ | STAGE NUMBER | 3" |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-14, FIG 132; FLOW AREA 4.689-4.714" |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL" |
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