You are currently exploring our in-stock options for part number 709451CL13 with the NSN 2840000637367. This product is listed with the description “Nozzle Turbine Aircraft Gas Turb” and is manufactured by United Technologies Corporation. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number 709451CL13 is listed alongside the NSN 2840-00-063-7367 and belongs to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, it is also under the CAGE Code 77445, which is assigned to United Technologies Corporation. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number 709451CL13 seamless.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-063-7367 Item Description: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 000637367 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 709451CL13 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.919 INCHES MINIMUM AND 1.923 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 2.019 INCHES MINIMUM AND 2.099 INCHES MAXIMUM |
| AGAV | III END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | 1.227-1.237 SQ IN. FLOW AREA |
| MATT | III MATERIAL | NICKEL ALLOY VANE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA657 ASSN STD 1ST MATERIAL RESPONSE VANE AND AMS5540 ASSN STD 2ND MATERIAL RESPONSE VANE |
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