Part Number : 804351CL19 | NSN : 2840-01-394-52262840013945226 |
Item Name : Nozzle Turbine Airc | Manufacturer : Turbine Airfoil Designs Inc |
CAGE Code : 96965 | FSC : FSC2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
NIIN : 013945226 |
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-394-5226 Item Description: Nozzle Turbine Airc | 2840 | 013945226 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
804351cl19 | 6 | 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-TURB STTR, 1 STG |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
CZCJ | STAGE NUMBER | 1 |
FEAT | SPECIAL FEATURES | FLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 |
MATT | III MATERIAL | COBALT ALLOY OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
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