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Part Number 804351CL18 described as Nozzle Turbine Aircraft Gas Turb with NSN 2840-01-394-5231 with FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components by Manufacture Turbine Airfoil Designs Inc is available in stock. We provide comprehensive database of aerospace and aviation components, sub-assemblies, and completed assemblies allows us to respond to your RFQ within 15 minutes.
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| 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 |
| 804351 | 5 | 9 | D |
| 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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