FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-01-378-6267, 2840-01-379-4636, 2840-01-379-4980
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-01-378-6267 2840013786267 | 6042T63P07 | Shaft, Turbine, Aircraft gas Turbi | General Electric Company (99207) | ||
| 2840-01-378-8414 2840013788414 | 200692-1 | Seal, Metallic, Aircraft gas Turbi | Kaydon Ring & Seal Inc. (75370) | ||
| 2840-01-378-9286 2840013789286 | 3001158-1 | Seal, Air, Aircraft gas Turbine En | Honeywell International Inc. (99193) | ||
| 2840-01-378-9975 2840013789975 | 3075370-2 | Engine, Aircraft, Turbo-Prop | Honeywell International Inc. (99193) | ||
| 2840-01-379-0135 2840013790135 | 5060T23P04 5060T23P05 42H30249 | Insulator Metal, Power Turbine | General Characteristics Item Description: Insulation is fabricated from nickel alloy, AMS5540, 0.001 inch minimum to 0.005 inch maximum thick. insulation is 0.750 inch minimum to 0.810 inch maximum width and 0.120 inch minimum to 0.200 inch maximum height. the insulation has 0.020 inch minimum to 0.100 inch maximum radius in six places and one 0.050 inch minimum to 0.090 inch maximum radius. maximum operating temperature is 2000 degrees fahrenheit. maximum density of the insulation must be 14 lbs/cu ft. | A G C Incorporated (98500) General Electric Company (99207) Tighitco Inc. (22013) | |
| 2840-01-379-0746 2840013790746 | 201311-03 | Seal Ring, Labyrinth, Aircraft gas | Kaydon Ring & Seal Inc. (75370) | ||
| 2840-01-379-0760 2840013790760 | 2194434 | Shaft, Turbine, Aircraft gas Turbi | United Technologies Corporation (77445, 52661) | ||
| 2840-01-379-3493 2840013793493 | 740852CL7 | Vane, Compressor, Aircraft gas Tur | United Technologies Corporation (77445) | ||
| 2840-01-379-3651 2840013793651 | 3092485-2 | Stiffener, Divergent Nozzle, Aircr | III End Item Identification: Pacer dawn Special Features: Matl waspaloy, ams 5544; length 3.970-4.030; height 1.070-1.130; 1ST end width (top) 0.130-0.190; 2ND end width (bottom) 0.290-0.350; stock thickness 0.040; goes on the variable nozzle divergent seal assembly; T.O. 2J-F10424 | Honeywell International Inc. (99193) | |
| 2840-01-379-4418 2840013794418 | 6027T12G21 | Case and Vane Assembly, fan, Aircr | General Electric Company (99207) | ||
| 2840-01-379-4421 2840013794421 | 6026T30G05 | Disk, gas Turbine Engine | General Electric Company (99207) | ||
| 2840-01-379-4429 2840013794429 | 6084T11P01 | Blade, Turbine Rotor, Aircraft gas | General Electric Company (99207) | ||
| 2840-01-379-4635 2840013794635 | 6072T70G07 | Rotor, Compressor, Aircraft gas Tu | General Electric Company (99207) | ||
| 2840-01-379-4636 2840013794636 | 6084T13G03 | Case and Vane Assembly, fan, Aircr | General Electric Company (99207) | ||
| 2840-01-379-4637 2840013794637 | 6049T51G13 | Case, Turbine, Aircraft gas Turbin | General Electric Company (99207) | ||
| 2840-01-379-4638 2840013794638 | 6072T93P02 | Disk, Turbine, Aircraft gas Turbin | III End Item Identification: Engine model F404 Engine Section Location: High pressure turbine | General Electric Company (99207, 03350) | |
| 2840-01-379-4641 2840013794641 | 6084T19G01 | Rotor, Turbine, Aircraft gas Turbi | General Electric Company (99207) | ||
| 2840-01-379-4836 2840013794836 | 9697M22P02 | Shroud, Turbine | General Electric Company (07482) | ||
| 2840-01-379-4838 2840013794838 | 9697M22P07 | Shroud, Turbine | General Electric Company (07482) | ||
| 2840-01-379-4980 2840013794980 | 6072T51P02 | Disk, Turbine, Aircraft gas Turbin | General Electric Company (03350, 99207) |