Thank you for taking an interest in our selection of 2840-01-458-3129 parts here on Boost AOG. You are currently on the RFQ form for part number 578041, a United Technologies Corporation product listed with the Blade Set Compressor Aircraft Ga If part number 578041 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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To ensure the quality of our NSN components, we adhere to a strict NO CHINA SOURCING pledge, meaning every purchased item will be delivered alongside any pertinent qualifying certifications or manufacturing trace documentation for your benefit. Paired with numerous other commitments, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. If you happen to be facing a time constraint and require NSN parts quickly, contact us at your earliest convenience, and we will discuss the expedited shipping options we have available for domestic and international customers alike. With our various dedications in mind, kick off procurement for United Technologies Corporation part number 578041 and other Blade Set Compressor Aircraft Ga products today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-458-3129 Item PartTypeName: BLADE SET,COMPRESSOR,AIRCRAFT GA | 2840 | 014583129 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
578041 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | TF33-PW-102C AIRCRAFT GAS TURBINE ENGINE |
AGUC | UNIT PACKAGE QUANTITY | 2 |
AJJW | COMPONENT QUANTITY | 16 |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
FEAT | SPECIAL FEATURES | 8MATL 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 |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 3, IND 3 |
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