804351CL18 by Therm Incorporated with NSN 2840013945231 - Submit a Quote
| Part No. : 804351CL18 | Manufacturer : Therm Incorporated | NSN : 2840-01-394-5231 |
| 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 804351CL18 of NSN 2840013945231 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number 804351CL18 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).
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. 804351CL18 therm incorporated is in stock.
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NSN Information for Part Number 804351CL18 with NSN 2840-01-394-5231, 2840013945231
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5231 Item Description: Nozzle Turbine Aircraft Gas Turb | 2840 | 013945231 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804351cl18 | 5 | 2 | 5 |
Characteristics Data of NSN 2840-01-394-5231, 2840013945231MRC Criteria Characteristic RDAL Reference Data And Literature T.O. 2J-TF33-4 FIG31 IND50 BGLW Blade Attachment Method SLOT CRTL Criticality Code Justification APGF AND CZBJ AND CZCJ AND BGLW AND FEAT APGF Design Type AXIAL COMPRESSOR ABHP Overall Length 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM AGAV End Item Identification TF-33 AIRCRAFT ENGINE MATT Material COBALT ALLOY OVERALL CZBJ Engine Section Location HIGH PRESSURE TURBINE MRC Decoded Requirement Clear Text Reply MDCL Material Document And Classification PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL FEAT Special Features FLOW AREA 1.427-1.436; PITCH 34 DEG. 2 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 ABKW Overall Height 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM CXCY Part Name Assigned By Controlling Agency VANE,HPT,1 STG ABMK Overall Width 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM CZCJ Stage Number 1
| MRC | Criteria | Characteristic |
|---|---|---|
| RDAL | Reference Data And Literature | T.O. 2J-TF33-4 FIG31 IND50 |
| BGLW | Blade Attachment Method | SLOT |
| CRTL | Criticality Code Justification | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| APGF | Design Type | AXIAL COMPRESSOR |
| ABHP | Overall Length | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| AGAV | End Item Identification | TF-33 AIRCRAFT ENGINE |
| MATT | Material | COBALT ALLOY OVERALL |
| CZBJ | Engine Section Location | HIGH PRESSURE TURBINE |
| MRC | Decoded Requirement | Clear Text Reply |
| MDCL | Material Document And Classification | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| FEAT | Special Features | FLOW AREA 1.427-1.436; PITCH 34 DEG. 2 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 |
| ABKW | Overall Height | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| CXCY | Part Name Assigned By Controlling Agency | VANE,HPT,1 STG |
| ABMK | Overall Width | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| CZCJ | Stage Number | 1 |
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