FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-01-223-1197, 2840-01-223-5155, 2840-01-224-0986
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-01-223-1197 2840012231197 | 9125M13G30 | Support, Accessory, Aircraft gas T | III End Item Identification: Acft eng. F108 Criticality Code Justification: AGAV | General Electric Company (07482) CFM International Inc. (58828) | |
| 2840-01-223-1199 2840012231199 | SSCY7073-1 | Ring, Matched, Seal | III End Item Identification: Acft ENG.F110 Criticality Code Justification: AGAV | Stein Seal Company (03673) | |
| 2840-01-223-1259 2840012231259 | 4025642 | Flameholder, Afterburner, Turbine | Criticality Code Justification: AGAV Engine Section Location: Afterburner Material: Steel overall | United Technologies Corporation (52661, 77445) | |
| 2840-01-223-1260 2840012231260 | 4025644 | Flameholder, Afterburner, Turbine | Criticality Code Justification: AGAV Engine Section Location: Afterburner Material: Steel overall | United Technologies Corporation (77445, 52661) | |
| 2840-01-223-1261 2840012231261 | 4042582 | Flameholder, Afterburner, Turbine | Criticality Code Justification: AGAV Engine Section Location: Afterburner Material: Steel overall | United Technologies Corporation (52661, 77445) | |
| 2840-01-223-1262 2840012231262 | 4042574 | Flameholder, Afterburner, Turbine | Criticality Code Justification: AGAV Engine Section Location: Afterburner Material: Steel overall | United Technologies Corporation (77445) | |
| 2840-01-223-1263 2840012231263 | 4025645 | Flameholder, Afterburner, Turbine | Engine Section Location: Afterburner Material: Steel overall Overall Length: 1.000 inches nominal | United Technologies Corporation (52661, 77445) | |
| 2840-01-223-5107 2840012235107 | 6049T90G03 | Rotor, Turbine, Aircraft gas Turbi | General Electric Company (99207) | ||
| 2840-01-223-5108 2840012235108 | 6049T69P02 | Disk, Turbine, Aircraft gas Turbin | General Electric Company (99207, 03350) | ||
| 2840-01-223-5155 2840012235155 | 4067034 | Bell Crank | III End Item Identification: Acft eng F100-PW-100/200B Criticality Code Justification: AGAV | United Technologies Corporation (77445) | |
| 2840-01-223-5821 2840012235821 | 4074T00P02 9153 | Seal, Metallic, Aircraft gas Turbi | III End Item Identification: Acft eng TF34 Criticality Code Justification: AGAV Material: Steel overall | General Electric Company (99207) Eaton Corporation (15284) | |
| 2840-01-223-5867 2840012235867 | 4067481 | Rotor, Compressor, Aircraft gas Tu | III End Item Identification: Acft ENG100PW100/200 Engine Section Location: Compressor Special Features: Was compressor rotor, axial, turbine engine | United Technologies Corporation (77445) | |
| 2840-01-223-6516 2840012236516 | 125D200AA-22 | Nozzle, Turbine | General Electric Co. (03502) | ||
| 2840-01-223-7663 2840012237663 | 2181891 | Rotor, Compressor, Aircraft gas Turbine Engine | United Technologies Corporation (77445) | ||
| 2840-01-223-8384 2840012238384 | 2188012 2185612 | Disk, Compressor | United Technologies Corporation (77445, 52661) | ||
| 2840-01-224-0972 2840012240972 | 9550M14 9550M14G02 | Rotor, Compressor, Aircraft gas Tu | III End Item Identification: Acft.eng. F101 Engine Section Location: Compressor Special Features: Includes stages 1-9; was compressor rotor, axial, turbine engine | General Electric Company (07482) | |
| 2840-01-224-0973 2840012240973 | 9550M19G03 | Rotor, Turbine, Aircraft gas Turbi | III End Item Identification: F101 aircraft engine Engine Section Location: Low pressure turbine Special Features: T.O. 2J-F101-4, fig 1, ind 19; includes 1ST and 2ND stage disks | General Electric Company (07482) | |
| 2840-01-224-0974 2840012240974 | 9550M28G26 9550M28G11 9550M28G12 9550M28G18 9550M28G05 | Rotor, Compressor, Aircraft gas Tu | III End Item Identification: Acft.eng. F101 Engine Section Location: Compressor Special Features: Was compressor rotor, axial, turbine engine | General Electric Company (07482) | |
| 2840-01-224-0985 2840012240985 | 9507M60G14 9507M60G16 9507M60 | Chamber, Combustion, Aircraft gas | Engine Section Location: Combustion chamber Overall Length: 7.487 inches nominal End Item Identification: Acft.eng. F101 | General Electric Company (07482) | |
| 2840-01-224-0986 2840012240986 | 1359M25P01 | Disk, Compressor, Aircraft gas Tur | III End Item Identification: Acft.eng. F101 Engine Section Location: Compressor Special Features: Original name disk, axial compressor, turbine engine | General Electric Company (07482) |