Part No. : 804351CL17 | Manufacturer : Turbine Airfoil Designs Inc | CAGE Code : 96965 |
Item Name : Nozzle Turbine Aircraft Gas Turb | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components | NSN : 2840-01-394-5230 |
You can send a request for quote for p/n 804351CL17 to ASAP Semiconductor using justpartsunlimited.com. This part is manufactured by Turbine Airfoil Designs Inc (CAGE Code 96965). The description of it is Nozzle Turbine Aircraft Gas Turb. The national stock number associated with this part is NSN 2840013945230. This part belongs to FSC Gas Turbines and Jet Engines Aircraft Prime Moving and Components part family. An associate from ASAP Semiconductor will respond within 15 minutes to your query. It is our pleasure to help you with 804351CL17 part requirements.
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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 |
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