Whether you are in need of military aviation parts, NSN components, or various forms of aerospace and defense parts, Aerospace Store is a single-sourcing solution with over 2 billion product listings readily available for purchase at any time with competitive pricing. You have reached the Request for Quote (RFQ) page for part number 804351CL17, a Turbine Airfoil Designs Inc component we feature that is listed with the NSN 2840013945230 and item name “Nozle Turbine Aircraft Gas Turb.” For further identification, part number 804351CL17 was also specifically produced under CAGE Code 96965 and belongs to Federal Supply Class (FSC) 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. If you would like to receive specific options for procurement that have been tailored to your unique needs and restrictions alike, we ask that you please fill out and submit the form provided on this page with as much information as you can. Once our team has a chance to receive and review your offered details, a dedicated account manager will be in touch shortly after.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5230 Item Description: 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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM" |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM" |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE" |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR" |
| BGLW | BLADE ATTACHMENT METHOD | SLOT" |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT" |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG" |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE" |
| CZCJ | STAGE NUMBER | 1" |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC." |
| MATT | III MATERIAL | COBALT ALLOY OVERALL" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50" |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM" |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM" |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE" |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR" |
| BGLW | BLADE ATTACHMENT METHOD | SLOT" |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT" |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG" |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE" |
| CZCJ | STAGE NUMBER | 1" |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC." |
| MATT | III MATERIAL | COBALT ALLOY OVERALL" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50" |
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