NSN 2840-01-450-9428 · NIIN 014509428 · FSC 2840
NO DASHES 2840014509428
In Stock
DISK AND HUB,COMPRESSOR,AIRCRAFT
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: TF33-PW-102/A&B/103 AIRCRAFT GAS TURBINE ENGINES
Technical characteristics
7 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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF33-PW-102/A&B/103 AIRCRAFT GAS TURBINE ENGINES |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR; SUPERSEDES P/N 431001; THE CRITICALITY CODE CHANGE TO F IS ESSENTIAL TO WEAPON SYSTEM PERFORMANCE AND OPERATION. A FAILURE COULD CAUSE CATASTROPHIC FAILURE RESULTING IN THE LOSS OF OR SERIOUS DAMAGE TO THE AIRCRAFT OR WEAPON SYSTEM OR AN UNCOMMANDED ENGINE SHUTDOWN THAT JEPORDIZES SAFETY |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 5, IND 1 |