FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-01-508-6686, 2840-01-509-0325, 2840-01-509-2010
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
2840-01-508-6686 2840015086686 | 5087T30G01 | Shroud Segment, Turbine, Aircraft | III End Item Identification: J85-GE21 eng Criticality Code Justification: AGAV Engine Section Location: Turbine | General Electric Company (99207) | |
2840-01-508-7006 2840015087006 | 6005T48G12 | Compressor Rotor | III End Item Identification: Item used on turbo prop engines (T64) Criticality Code Justification: AGAV | General Electric Company (99207) | |
2840-01-508-7508 2840015087508 | 5037T01P04 | Shaft, Turbine, Aircraft gas Turbi | General Electric Company (99207) | ||
2840-01-508-8224 2840015088224 | 4322725-01 | Liner Assy F119 | III End Item Identification: F119 engine Criticality Code Justification: AGAV | United Technologies Corporation (77445) | |
2840-01-509-0005 2840015090005 | 501F-CVS | Kit, Vane Compressor | III End Item Identification: Turboprop engine model T56-A-14 Special Features: Kit contains 1EA. 1ST. stage comp vane part no. 23064891, 1 ea. 2ND stage comp vane part no. 23064892, 1 ea. 3RD stage comp vane part no. 23064893, 1EA. 4TH stage comp vane part no. 23064894, 1 ea. 5TH stage comp vane part no. 23064895, 1EA. 6TH stage comp vane 23064896, 1 ea. 7TH stage comp vane part no. 23064897, 1 ea. 8TH stage comp vane part no. 23064898, 1 ea. 9TH stage comp vane part no. 23064899, 1EA. 10TH stage comp vane part no. 23064880, 1 ea. 11TH stage comp vane part no. 23064881, 1 ea. 12TH stage comp vane part no. 23064882, 1 ea. 13TH stage comp vane part no. 23064883 | Rolls-Royce Engine Services-Oakland (58320) | |
2840-01-509-0304 2840015090304 | 6064T07P06 | Plate, Cooling, Turbine Engine | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0307 2840015090307 | 6071T04G29 | Nozzle, Turbine, Aircraft gas Turb | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0308 2840015090308 | 5066T16G25 | Nozzle, Turbine, Aircraft gas Turb | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0315 2840015090315 | 4106T80P01 | Plate, Cooling, Turbine Engine | Special Features: Used on T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0321 2840015090321 | 6058T99G07 | Blade, Turbine Rotor, Aircraft gas | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0325 2840015090325 | 3056T94P02 | Shroud Segment, Turbine, Aircraft | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0326 2840015090326 | 6080T32P21 | Damper, Turbine Blade, Aircraft Tu | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0327 2840015090327 | 6068T35G15 | Support, Turbine Component, Aircra | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0348 2840015090348 | 3056T17P09 | Blade, Turbine Rotor, Aircraft gas | III End Item Identification: T700-GE-701D engine for UH-60 blackhawk and AH-64 apache helicopter | General Electric Company (99207) | |
2840-01-509-0509 2840015090509 | 3281717 | Fan, Aircraft gas Turbine Engine | Special Features: Weight 11.7 lbs; length 22 in; width 22 in; height 3 in | Cummins Inc. (0B8S3, 15434) | |
2840-01-509-0795 2840015090795 | 6078T11P01 | Blade, Turbine Rotor, Aircraft gas | III End Item Identification: TF34-GE-2 jet engines Criticality Code Justification: AGAV | General Electric Company (99207) | |
2840-01-509-1960 2840015091960 | 23031782 | Nozzle Segment, Turbine, Aircraft | Rolls-Royce Corporation (63005) | ||
2840-01-509-1985 2840015091985 | 23031781 | Nozzle Segment, Turbine, Aircraft | Rolls-Royce Corporation (63005) | ||
2840-01-509-1990 2840015091990 | 23031780 | Nozzle Segment, Turbine, Aircraft | Rolls-Royce Corporation (63005) | ||
2840-01-509-2010 2840015092010 | 5087T31G01 | Shroud Segment, Turbine, Aircraft | III End Item Identification: J-85 Criticality Code Justification: AGAV Engine Section Location: Turbine | General Electric Company (99207) |