NSN 2840-01-455-0363 · NIIN 014550363 · FSC 2840
NO DASHES 2840014550363
In Stock
SEAL,AIR,AIRCRAFT GAS TURBINE EN
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F110-GE-100 AIRCRAFT GAS TURBINE 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 1.880 AND INCHES MAXIMUM 1.908 |
| ABMZ | DIAMETER | INCHES MINIMUM 23.095 AND INCHES MAXIMUM 23.097 |
| AGAV | END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABMZ AND ABHP AND FEAT AND CZBJ |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL,ROTATING,AIR HIGH PRESSURE TURBINE,FRONT |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| FEAT | 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 |
| MATT | MATERIAL | OVERALL NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL MFR REF SINGLE MATERIAL RESPONSE RENE95 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 52, IND 9 |