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804351CL19 by Therm Incorporated with NSN 2840013945226 - Submit a Quote

Part No. : 804351CL19 Manufacturer : Therm Incorporated NSN : 2840-01-394-5226
Item Name : Nozzle Turbine Aircraft Gas Turb CAGE Code : 99160 FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components

ASAP Aviation Procurement is pleased to announce that part number 804351CL19 of NSN 2840013945226 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number 804351CL19 is a nozzle turbine aircraft gas turb manufactured by therm incorporated under CAGE Code 99160. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote.In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea). 

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804351CL19 Nozzle Turbine Aircraft Gas Turb
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We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA.  804351CL19 therm incorporated is in stock.

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NSN Information for Part Number 804351CL19 with NSN 2840-01-394-5226, 2840013945226

NSNFSCNIINCLSHazmatDEMILCancelled NSN
2840-01-394-5226

Item Description:

Nozzle Turbine Aircraft Gas Turb

28400139452260N
CIICHCCESDPMICCriticalityENAC
U A0
Part NumberISCRNVCRNCCHCCMSDSSADC
804351cl19623

Characteristics Data of NSN 2840-01-394-5226, 2840013945226

MRCCriteriaCharacteristic
ABHPOVERALL LENGTH2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM"
ABKWOVERALL HEIGHT4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM"
ABMKOVERALL WIDTH1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM"
AGAVEND ITEM IDENTIFICATIONTF-33 AIRCRAFT ENGINE"
APGFDESIGN TYPEAXIAL COMPRESSOR"
BGLWBLADE ATTACHMENT METHODSLOT"
CRTLCRITICALITY CODE JUSTIFICATIONAPGF AND CZBJ AND CZCJ AND BGLW AND FEAT"
CXCYPART NAME ASSIGNED BY CONTROLLING AGENCYVANE-TURB STTR, 1 STG"
CZBJENGINE SECTION LOCATIONHIGH PRESSURE TURBINE"
CZCJSTAGE NUMBER1"
FEATSPECIAL FEATURESFLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780"
MATTIII MATERIALCOBALT ALLOY OVERALL"
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONPWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL"
RDALREFERENCE DATA AND LITERATURET.O. 2J-TF33-4 FIG31 IND50"
ABHPOVERALL LENGTH2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM"
ABKWOVERALL HEIGHT4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM"
ABMKOVERALL WIDTH1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM"
AGAVEND ITEM IDENTIFICATIONTF-33 AIRCRAFT ENGINE"
APGFDESIGN TYPEAXIAL COMPRESSOR"
BGLWBLADE ATTACHMENT METHODSLOT"
CRTLCRITICALITY CODE JUSTIFICATIONAPGF AND CZBJ AND CZCJ AND BGLW AND FEAT"
CXCYPART NAME ASSIGNED BY CONTROLLING AGENCYVANE-TURB STTR, 1 STG"
CZBJENGINE SECTION LOCATIONHIGH PRESSURE TURBINE"
CZCJSTAGE NUMBER1"
FEATSPECIAL FEATURESFLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780"
MATTIII MATERIALCOBALT ALLOY OVERALL"
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONPWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL"
RDALREFERENCE DATA AND LITERATURET.O. 2J-TF33-4 FIG31 IND50"

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