Defence NSN Source is a one-stop shop for Nozzle Turbine Aircraft Gas Turbine Engine components and other similar products that meet the needs of our customer base. You have taken a specific interest in part number 4082943, a United Technologies Corporation offering we carry that is listed alongside the NSN 2840-01-445-5374 to streamline identification and procurement. If you fill out and submit the Request for Quote (RFQ) form located below, you can secure pricing options for your comparisons. Within 15 minutes of one of our team members receiving and reviewing your submission, you can anticipate a customized response.
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We strive to make the procurement process more straightforward and efficient by offering comprehensive details for listed components whenever possible. For instance, part number 4082943 was manufactured by United Technologies Corporation under the CAGECode 77445. Moreover, by using the first digits of the NSN 2840-01-445-5374, we can see that this product belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Utilizing such information, you can ensure that you are securing precisely what you need to carry out operations or meet your project requirements. Keeping this in mind, obtain a quote on part number 4082943 with our online services.
| 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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