| Alternative NSN: 2840-01-394-5230 |
| Item Name: Nozzle Turbine Airc |
| CAGE Code : 99160 , 96965 , 77445 |
| NIIN: 013945230 |
| FSC Name: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NCB Code: USA (01) |
| Manufacturers: therm incorporated , turbine airfoil designs inc , united technologies corporation |
|
Part No Part No
|
Manufacturer |
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
|---|---|---|---|---|
| 804351CL17 | therm incorporated | nozzle turbine airc | Avl | |
| 804351CL17 | turbine airfoil designs inc | nozzle turbine airc | Avl | |
| 804351 | united technologies corporation | nozzle turbine airc | Avl | |
| 804351CL17 | united technologies corporation | nozzle turbine airc | Avl |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| 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 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
| CZCJ | STAGE NUMBER | 1 |
| 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 |
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