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HomeNSNEngines, Turbines, and ComponentsGas Turbines and Jet Engines, Aircraft, Prime Moving; and Components1559M63G04-118 NSN 2840-01-459-1286 - 7ce75f2b

1559M63G04-118 NSN 2840-01-459-1286 - 7ce75f2b

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NSN 2840-01-459-1286 - (2840014591286) Technical Details :

MRCNameDetails
ABHPOVERALL LENGTH6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM
ABMZDIAMETER17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM
APGFDESIGN TYPEAXIAL COMPRESSOR
CRTLCRITICALITY CODE JUSTIFICATIONABHP AND ABMZ AND FEAT
CXCYPART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME HPC COMPRESSOR SPOOL
CZBJENGINE SECTION LOCATIONCOMPRESSOR
FEATSPECIAL FEATURES"T.O. 2J-F110-4, FIG 67, IND 5; HPCR STG 1-2, SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE; CAN ONLY BE USED ON THE F118-GE-100 AIRCRAFT JET TURBINE ENGINE"
MATTIII MATERIALTITANIUM ALLOY OVERALL
MATTMATERIALTITANIUM ALLOY OVERALL

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