If your operations demand part number 804351CL22, an item produced by Turbine Airfoil Designs Inc and listed with the description “Nozzle Turbine Aircraft Gas Turb,” look no further than this page. At your convenience, you can complete the Request for Quote (RFQ) form below with details like your budget, desired quantity, and anticipated fulfillment timeline to receive customized procurement options on part number 804351CL22. Our representatives will happily treat you to competitive pricing and swift lead times upon their receipt and review of a completed form, regularly responding in 15 minutes or less.
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If you are interested, be sure to explore our website further for related CAGE Code 96965 items or other various products manufactured by Turbine Airfoil Designs Inc. We also present a catalog of all related FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components parts that we currently carry for your perusal. Regardless of what you decide to purchase from us, we will work closely with you to provide dependable, authentic products while ensuring that we address every requirement possible. This being said, get started on requesting quotes for part number 804351CL22 and any other NSN parts you need on Sky Forge Components to experience our unrivaled fulfillment services.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-394-7115 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013947115 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
804351 | 2 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 4.153 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | TF-33 |
CZCJ | STAGE NUMBER | 1 |
MATT | MATERIAL | COBALT ALLOY VANE |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
ABHP | OVERALL LENGTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
BGLW | BLADE ATTACHMENT METHOD | SLOT |
CRTL | CRITICALITY CODE JUSTIFICATION | ABMK |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31,IND 50 |
ABMK | OVERALL WIDTH | 2.045 INCHES NOMINAL |
FEAT | SPECIAL FEATURES | FLOW AREA 1.464-1.489.PITCH IS 34DEG 38MIN 28SEC |
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