| DESIGN TYPE | AXIAL COMPRESSOR |
| DIAMETER | 23.095 INCHES MINIMUM AND 23.097 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | ABMZ AND ABHP AND FEAT AND CZBJ |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| MATERIAL DOCUMENT AND CLASSIFICATION | RENE95 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| III MATERIAL | NICKEL ALLOY OVERALL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL,ROTATING,AIR HIGH PRESSURE TURBINE,FRONT |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 1.880 INCHES MINIMUM AND 1.908 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 52, IND 9 |
| SPECIAL FEATURES | CID 907068 INTRODUCES A CHANGE IN MATL FOR THE HPT ROTOR OUTER SEAL AND DISK, CHG FROM -140 MESH R95 TO -270 R95; MADE FROM FINER POWDER WHICH INCREASES THE LCF LIFE AND RESIDUAL LIFE; MAINTAINABLILITY SAME |