NSN 2840-01-456-6799 · NIIN 014566799 · FSC 2840
NO DASHES 2840014566799
In Stock
ROTOR,TURBINE,AIRCRAFT GAS TURBI
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F110-GE-100B AIRCRAFT GAS TURBINEENGINE
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 |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES MINIMUM 18.993 AND INCHES MAXIMUM 19.028 |
| AGAV | END ITEM IDENTIFICATION | F110-GE-100B AIRCRAFT GAS TURBINEENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| FEAT | SPECIAL FEATURES | ECP F248; EPD A611D36R0; MODIFICATIONS TO THE F110GE100 UPGRADES TAC ENSIP TO 4000 CYCLES INSPECTION INTERVAL; INCOPORATES SEVERAL DURABILITY AND SAFETY IMPROVEMENTS AND LIFE LIMITED HARWARE REPLENISHMENTS GRP TOGETHER AS 1PACKAGE TO THE CURRENT F110GE100 ENGINE; THE CHG WILL HAVE NO IMPACT TO ENGINE WEIGHT, BALANCE, STABILITY OR MOMENT SINCE THE ONLY CHANGE BEING DONE IS A NAMEPLATE CHG TO IDENTIFY THE COMPLETE ACCUMULATION OF CHANGES TO PROVIDE 4000 TAC ENSIP INSPECTIONS; ROTORS AND CDNS THAT ARE TO INSTALLED WILL BE 4000 TAC INTERVAL CAPABLE & WILL REQUIRE REIDENTIFIED TO THE 9546M PART NUMBERS PER THE TCTO; REPL P/NS 9521M18G30, 9521M18G22, 9521M18G08, 9521M18G06, 9521M18G04, 9521M18G02 AND 9521M18G01 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 1, IND 13 |