When you require Nozzle Turbine Aircraft Gas Turb components such as part number 804351CL17 with the NSN 2840013945230 for your operations, Broadline NSN is your best bet. Whether you are searching for parts from manufacturers like United Technologies Corporation or something else, our team is dedicated to helping you acquire what you need with competitive rates and rapid lead times for your benefit. As such, when you have discovered items of interest, we encourage you to take advantage of our rapid RFQ service by filling out and submitting the form featured throughout our website. On this form, be sure to include relevant details such as your desired part quantity and budget parameters so that our dedicated team members can craft a customized solution that suits your particular operational needs.
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At Broadline NSN, we are dedicated to distributing reliable products such as those with the NSN 2840-01-394-5230 or CAGE code 77445. As an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited parts distributor, you can rely on the caliber of our offerings which feature more than 2 billion new, used, obsolete, and hard-to-find components that are readily available for your purchase at any time. Countless products are subject to rigorous quality control measures to guarantee their fit, form, and function prior to your purchase for your benefit, and all come from leading manufactures like United Technologies Corporation. Those looking for high-quality parts like listings belonging to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components can count on our team to get them what they need in rapid time. Call or email us with any questions and we will be more than happy to assist you through any stage of the procurement process.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5230 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013945230 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804351CL17 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC. |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
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