NSN 2840-01-394-5230 · NIIN 013945230 · FSC 2840
NO DASHES 2840013945230
In Stock
NOZZLE,TURBINE,AIRCRAFT GAS TURB
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: TF-33 AIRCRAFT ENGINE
Technical characteristics
14 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES MINIMUM 2.035 AND INCHES MAXIMUM 2.045 |
| ABKW | OVERALL HEIGHT | INCHES MINIMUM 4.270 AND INCHES MAXIMUM 4.300 |
| ABMK | OVERALL WIDTH | INCHES MINIMUM 1.110 AND INCHES MAXIMUM 1.130 |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC. |
| MATT | MATERIAL | OVERALL COBALT ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL ASSN STD SINGLE MATERIAL RESPONSE AWA647 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |