You are currently exploring our in-stock options for part number 804351CL20 with the NSN 2840013945228. This product is listed with the description “Nozzle Turbine Aircraft Gas Turb” and is manufactured by Therm Incorporated. 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 804351CL20 is listed alongside the NSN 2840-01-394-5228 and belongs to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, it is also under the CAGE Code 99160, which is assigned to Therm Incorporated. 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 804351CL20 seamless.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5228 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013945228 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804351 | 2 | 9 | D |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| CZCJ | STAGE NUMBER | 1 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT 1 STG |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.446-1.455; PITCH 34 DEG. 20 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 IN. |
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