578041 NSN 2840-01-458-3129 - 394639df


1 U

NSN 2840-01-458-3129 - (2840014583129) Technical Details :

MRCNameDetails
AGAVEND ITEM IDENTIFICATIONTF33-PW-102C AIRCRAFT GAS TURBINE ENGINE
AGUCUNIT PACKAGE QUANTITY2
AJJWCOMPONENT QUANTITY16
CRTLCRITICALITY CODE JUSTIFICATIONFEAT
FEATSPECIAL FEATURES"MATL TITANIUM ALLOY, AMS 4928; DESIGN TYPE, AXIAL COMPRESSOR; ENGINE LOCATION, COMPRESSOR; STAGE 1; BLADE ATTACHMENT, DOVETAIL; WIDTH 0.839; HEIGHT 3.870-8.880; THIS ITEM COMES OFF A JT3D-7 COMMERICAL ENGINE; THE ORIGINAL P/N 572901 REPLC P/N 430401; IT TAKES 2 OF P/N 572901 TO MAKE SET; THE FORM, FIT, FUNCTION IS EXACTLY THE SAME, THE ANGLE OF THE BLADE IS DIFFERENT; BLADE WILL PROVIDE 1200 LBS MORE THRUST WHEN IN USE; ONCE REPLD WILL MODIFY THE TF33-PW-102B TO THE 102C; JOINT STAR AIRCRAFT PROJECT"
RDALREFERENCE DATA AND LITERATURE"T.O. 2J-TF33-34, FIG 3, IND 3"
RDALIII REFERENCE DATA AND LITERATURE"T.O. 2J-TF33-34, FIG 3, IND 3"
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