ROTOR,TURBINE,AIRCRAFT GAS TURBI

Name: ROTOR,TURBINE,AIRCRAFT GAS TURBI
Brand: Atlas Air Supply
SKU: 2840014566799
Availability: LimitedAvailability

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.

Technical characteristics from the federal item record
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

8 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.