NSN 2840-01-467-8591 · NIIN 014678591 · FSC 2840
NO DASHES 2840014678591
In Stock
HUB,COMPRESSOR,AIRCRAFT GAS TURB
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: TF33 AIRCRAFT ENGINE
Technical characteristics
12 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 16.550 AND INCHES MAXIMUM 16.570 |
| ABMZ | DIAMETER | INCHES MINIMUM 18.740 AND INCHES MAXIMUM 18.760 |
| AGAV | END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | HUB-REAR, COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | 16 HOLES EQUALLY SPACED 0127-.132DIA; SPLINE AT END OF SHAFT, NO. OF TEETH 51, DP 10/20, 30 DEG.; SPLINE AT FWD OF SHAFT, NO. OF TEETH 87, DP 16/32, 30 DEG. ANGLE |
| MATT | MATERIAL | HUB NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL ASSN STD SINGLE MATERIAL RESPONSE A-S5660 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG. 19, IND 15 |