We appreciate your interest in United Technologies Corporation part number 804351CL17, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 804351CL17 is listed with the NSN 2840-01-394-5230 and description “Nozzle Turbine Aircraft Gas Turb.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by United Technologies Corporation under the CAGE Code 77445 or that similarly fall under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 2840-01-394-5230 parts and Nozzle Turbine Aircraft Gas Turb items your operations require, so request a quote today.
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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