NSN 2840-01-394-5230, 2840013945230 Nozzle Turbine Aircraft Gas Turb Parts Sourcing
If you have been looking for United Technologies Corp, Turbine Airfoil Designs Inc, Therm Incorporated parts listed alongside the NSN 2840013945230, ASAP Distribution has you covered with our unmatched inventory of items Nozzle Turbine Aircraft Gas Turb. With over 2 billion parts readily available for purchase on our website, customers can get competitive pricing offers and rapid lead-times on top NSN part numbers such as 804351, 804351CL17. Explore our NSN parts catalog at your leisure, or you may take advantage of our provided search engine to find specific parts in a matter of moments. If you are interested in this particular component or others listed across our website, you may begin the procurement process at any time through the submission of an Instant RFQ form. Using the information that you submit to us, our team of industry experts will quickly craft you a quote that accommodates your individual needs and requirements for NSN 2840013945230.
Alternative NSN: 2840-01-394-5230 | Item Name : Nozzle Turbine Aircraft Gas Turb | FSG : 28 Engines Turbines and Components | Federal Supply Class (FSC) : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components | NIIN: 013945230 | NCB Code: USA (01) |
Part Number's List for NSN 2840-01-394-5230, 2840013945230
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
804351 | United Technologies Corp | nozzle turbine aircraft gas turb | Avl | RFQ |
804351CL17 | Turbine Airfoil Designs Inc | nozzle turbine aircraft gas turb | Avl | RFQ |
804351CL17 | Therm Incorporated | nozzle turbine aircraft gas turb | Avl | RFQ |
804351CL17 | United Technologies Corp | nozzle turbine aircraft gas turb | Avl | RFQ |
Characteristics Data of NSN 2840013945230
MRC | Criteria | Characteristic |
---|---|---|
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
MATT | MATERIAL | COBALT ALLOY OVERALL |
CZCJ | STAGE NUMBER | 1 |
ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC. |
ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
BGLW | BLADE ATTACHMENT METHOD | SLOT |
CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
AGAV | III END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
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