NSN 2840-01-431-9242 · NIIN 014319242 · FSC 2840
NO DASHES 2840014319242
In Stock
ROTOR,TURBINE,AIRCRAFT GAS TURBI
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F118-GE-100 AIRCRAFT GAS TURBINE ENGINE
Technical characteristics
8 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 | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| FEAT | SPECIAL FEATURES | HPT ROTOR AFT SHAFT DAMPER REDESIGN INCLUDES ECP FH165, HPT AFT SHAFT P/N 1385M24P01; SLEEVE DAMPER P/N 1864M56P01; SUPERSEDES P/N 9545M18G01, G02 AND G03; SUPERSEDED BY 9545M18G14, G15, G16 AND THEN G21 |
| MATT | MATERIAL | OVERALL NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL MFR REF SINGLE MATERIAL RESPONSE INCONEL 718 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F118-4, FIG 1, IND 13, FIG 68 & 69, BREAKOUTS |