Mfg Part Number: 804351CL20
NSN : 2840-01-394-5228
NIIN : 013945228
CAGE Code : 96965
Manufacturer: Turbine Airfoil Designs Inc
Item Name : Nozzle Turbine Aircraft Gas Turb
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-394-5228 Item Description: Nozzle Turbine Aircraft Gas Turb | 2840 | 013945228 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
804351cl20 | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CZCJ | STAGE NUMBER | 1 |
MATT | MATERIAL | COBALT ALLOY OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT 1 STG |
CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
FEAT | SPECIAL FEATURES | FLOW AREA 1.446-1.455; PITCH 34 DEG. 20 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 IN. |
BGLW | BLADE ATTACHMENT METHOD | SLOT |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
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