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ENGINES BRACKETS FLANGES SUPPORTS Parts 2840-01-315-1685 through 2840-01-323-5982
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We solve sourcing challenges for parts like 2840-01-315-1685, 2840-01-316-7807, 2840-01-316-8848, 2840-01-317-1624, 2840-01-317-2005, 2840-01-317-7859, 2840-01-317-7878, 2840-01-317-8321, 2840-01-318-1317, 2840-01-318-1319 -- hard to find, long lead time, and obsolete part requirements.
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Part numberDescriptionCategoryDetails
2840-01-315-1685RFQ plus Technical Data for 2840-01-315-1685SUPPORT, LINER, EXHAUSTGENERAL CHARACTERISTICS ITEM DESCRIPTION1.46 IN. LG
2840-01-316-7807RFQ plus Technical Data for 2840-01-316-7807SUPPORT, CHAMBER DUCT, COMBUSTION, OUTER REARIII END ITEM IDENTIFICATIONAIRCRAFT MODEL A-4; A-6
2840-01-316-8848RFQ for 2840-01-316-8848BRACKET ASSEMBLY
2840-01-317-1624RFQ plus Technical Data for 2840-01-317-1624FRAME ASSEMBLY, EXHAUSTIII END ITEM IDENTIFICATIONENGINE MODEL F-404-GE-400
2840-01-317-2005RFQ for 2840-01-317-2005SUPPORT, TURBINE ASSEMBLY, TURBINE ENGINE
2840-01-317-7859RFQ plus Technical Data for 2840-01-317-7859SUPPORT, CHAMBER DUCT, COMBUSTIONIII END ITEM IDENTIFICATIONAIRCRAFT MODEL A-4; A-6
2840-01-317-7878RFQ plus Technical Data for 2840-01-317-7878FRONT FRAMEIII END ITEM IDENTIFICATIONF110-GE-400 ENGINE
2840-01-317-8321RFQ plus Technical Data for 2840-01-317-8321SUPPORT, FAN COMPONENT, AIRCRAFT GAS TURBINE ENGINEMATERIALTITANIUM ALLOY
2840-01-318-1317RFQ plus Technical Data for 2840-01-318-1317SUPPORT, BLEED CONTROLIII END ITEM IDENTIFICATIONENGINE MODEL J-52
2840-01-318-1319RFQ plus Technical Data for 2840-01-318-1319SUPPORT, COMBUSTION CHAMBERIII END ITEM IDENTIFICATIONJ52 ENGINE
2840-01-318-5586RFQ plus Technical Data for 2840-01-318-5586SUPPORT, BEARING, AIRCRAFT GAS TURBINE ENGINECRITICALITY CODE JUSTIFICATIONAGAV
2840-01-319-1536RFQ plus Technical Data for 2840-01-319-1536SUPPORT, SEAL, AIRCRAFT GAS TURBINE ENGINECRITICALITY CODE JUSTIFICATIONAGAV
2840-01-320-0741RFQ plus Technical Data for 2840-01-320-0741FRAME, FAN, AIRCRAFT GAS TURBINE ENGINEMATERIALSTEEL
2840-01-320-0785RFQ for 2840-01-320-0785FRAME, FAN, AIRCRAFT GAS TURBINE ENGINE
2840-01-322-6120RFQ plus Technical Data for 2840-01-322-6120SUPPORT, AUGMENTOR COMPONENT, AIRCRAFT GAS TURBINE EMATERIALTITANIUM ALLOY
2840-01-322-6123RFQ plus Technical Data for 2840-01-322-6123HANGER SUPPORT, EXHAUST LINER, TURBINE ENGINESPECIAL FEATURESO/A LENGTH 1.893-1.923; O/A HEIGHT 0.755-0.775; O/A WIDTH 1.250-1.290; GOES ON THE EXHAUST DUCT
2840-01-322-6197RFQ plus Technical Data for 2840-01-322-6197SUPPORT, TURBINE COMPONENT, AIRCRAFT GAS TURBINE ENGMATERIALSTEEL
2840-01-322-6204RFQ plus Technical Data for 2840-01-322-6204SUPPORT, AUGMENTOR EXHAUST, TURBINEENGINECRITICALITY CODE JUSTIFICATIONAGAV
2840-01-323-0131RFQ plus Technical Data for 2840-01-323-0131RING, ACTUATION, FRONT FRAMESPECIAL FEATURES2J-F118-4
2840-01-323-0150RFQ plus Technical Data for 2840-01-323-0150FRAME, TURBINE, AIRCRAFT GAS TURBINE ENGINEMATERIALSTEEL
2840-01-323-0152RFQ plus Technical Data for 2840-01-323-0152BRACKET, ENGINE SUPPORT, TURBINE ENGINECRITICALITY CODE JUSTIFICATIONAGAV
2840-01-323-0153RFQ plus Technical Data for 2840-01-323-0153FRAME, TURBINE, AIRCRAFT GAS TURBINE ENGINECRITICALITY CODE JUSTIFICATIONAGAV
2840-01-323-0755RFQ plus Technical Data for 2840-01-323-0755SUPPORT, ACCESSORY, AIRCRAFT GAS TURBINE ENGINEMATERIALSTEEL CORROSION RESISTING
2840-01-323-5981RFQ plus Technical Data for 2840-01-323-5981SUPPORT, TURBINE COMPONENT, AIRCRAFT GAS TURBINE ENGOVERALL LENGTH20.500 INCHES MINIMUM AND 20.520 INCHES MAXIMUM
2840-01-323-5982RFQ plus Technical Data for 2840-01-323-5982SUPPORT, TURBINE COMPONENT, AIRCRAFT GAS TURBINE ENGMATERIALNICKEL ALLOY
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