FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-181-0292, 2840-00-184-4984, 2840-00-184-5042
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-181-0292 2840001810292 | 5900T34P05 | Hanger, Afterburner Casing | III End Item Identification: Eng J-85 General Characteristics Item Description: Steel, B50T1181, general electric co, 125 aa microinchsurface finish rating | General Electric Company (99207) | |
| 2840-00-181-0293 2840001810293 | 5900T34P06 5900T34P13 | Hanger, Afterburner Casing | Barnes Group Inc. (75440) General Electric Company (99207) | ||
| 2840-00-181-0296 2840001810296 | 3029T09G01 | Rod, Afterburner Liner | III End Item Identification: Eng J-85 General Characteristics Item Description: Steel, B50TF74, general electric co, 43.660 in. min, 43.760 in.max, lg of rod, 0.156 in. min, 0.160 in. max dia, rod is mtd on bracket, cobalt base alloy, B50TF59, general electric co, 1.320 in. min, 1.360 in.max lg, 0.230 in.min, 0.250 in. max W, 0.100 in. min, 0.130 in. max thk, one hole 0.188 in. dia, 43.780 in. min, 43.880 in. max, O/a lg | General Electric Company (99207) Columbia Manufacturing Inc. (8U485) | |
| 2840-00-181-0297 2840001810297 | 3901T71G01 | Hanger, Afterburner Casing | Criticality Code Justification: TEXT General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125 aa microinchsurface finish rating | General Electric Company (99207) | |
| 2840-00-181-0298 2840001810298 | 3901T72G01 | Hanger, Afterburner Casing | III End Item Identification: Eng J-85 General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125MICROINCH surface finish rating | General Electric Company (99207) | |
| 2840-00-181-0498 2840001810498 | 3901T73G01 | Hanger, Afterburner Casing | III End Item Identification: Eng J-85 General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125 microinchsurface finish rating | General Electric Company (99207) | |
| 2840-00-181-0572 2840001810572 | 5900T37G01 | Hanger, Afterburner Casing | III End Item Identification: Engine, turbojet model J85-21 General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125 microinchfinish O/a | Barnes Group Inc. (75440) General Electric Company (99207) | |
| 2840-00-181-0573 2840001810573 | 5900T37G02 | Hanger, Afterburner Casing | III End Item Identification: Engine, turbojet model J85-21 General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125 microinchfinish O/a | General Electric Company (99207) | |
| 2840-00-181-0574 2840001810574 | 5900T37G03 | Hanger, Afterburner | III End Item Identification: Engine, turbojet model J85-21 General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125 microinchfinish O/a | General Electric Company (99207) | |
| 2840-00-181-0580 2840001810580 | 5900T37G04 | Hanger, Afterburner Casing | III End Item Identification: Engine, turbojet model J85-21 General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125 microinchfinish O/a | General Electric Company (99207) | |
| 2840-00-181-0582 2840001810582 | 5900T37G05 | Hanger, Afterburner Casing | III End Item Identification: Engine, turbojet model J85-21 General Characteristics Item Description: Cobalt base alloy, B50TF59, general electric co, 125 microinch finisho/a | General Electric Company (99207) | |
| 2840-00-184-4980 2840001844980 | 673723 | Plate, Component Mounting, Aircraf | Criticality Code Justification: Czbj and abhp and abmk and agav Engine Section Location: Combustion chamber Material: Nickel alloy overall | United Technologies Corporation (77445) | |
| 2840-00-184-4982 2840001844982 | 694854 | Liner, Combustion Chamber, Aircraf | Criticality Code Justification: AGAV Overall Length: 2.100 inches minimum and 2.200 inches maximum End Item Identification: TF-30 aircraft engine | United Technologies Corporation (77445) | |
| 2840-00-184-4983 2840001844983 | 694855 | Liner, Combustion Chamber, Aircraf | Criticality Code Justification: AGAV Overall Length: 2.100 inches minimum and 2.200 inches maximum End Item Identification: TF-30 aircraft engine | United Technologies Corporation (77445) | |
| 2840-00-184-4984 2840001844984 | 655968 | Scoop, Combustion Chamber | III End Item Identification: TF-30 aircraft engine | United Technologies Corporation (77445) | |
| 2840-00-184-4986 2840001844986 | 694856 | Liner, Combustion Chamber, Aircraf | Criticality Code Justification: AGAV Overall Length: 2.100 inches minimum and 2.200 inches maximum End Item Identification: TF-30 aircraft engine | United Technologies Corporation (77445) | |
| 2840-00-184-4987 2840001844987 | 655969 | Scoop, Combustion Chamber | III End Item Identification: TF-30 aircraft engine | United Technologies Corporation (77445) | |
| 2840-00-184-5017 2840001845017 | 694858 | Chamber, Combustion, Aircraft gas | Criticality Code Justification: AGAV End Item Identification: TF-30 aircraft engine | United Technologies Corporation (77445) | |
| 2840-00-184-5031 2840001845031 | 694859 | Liner, Combustion Chamber, Aircraf | Criticality Code Justification: AGAV Engine Section Location: Combustion chamber Overall Length: 1.480 inches minimum and 1.520 inches maximum | United Technologies Corporation (77445) | |
| 2840-00-184-5042 2840001845042 | 694860 | Liner, Combustion Chamber, Aircraf | Criticality Code Justification: AGAV Overall Length: 1.480 inches minimum and 1.520 inches maximum End Item Identification: TF-30 aircraft engine | United Technologies Corporation (77445) |