Thank you for your interest in part number 4082943CLR, a component manufactured by United Technologies Corporation that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 2840-01-445-5374 and features the description “Nozzle Turbine Aircraft Gas Turbine Engine.” To request a quote for part number 4082943CLR, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 2840-01-445-5374 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from United Technologies Corporation, which is associated with the CAGECode 77445. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components part number 4082943CLR.
| 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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