FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-084-1369, 2840-00-084-8677, 2840-00-085-8968
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-084-1369 2840000841369 | 7054R43P19 133A1827P1 | Stop, Turbine Shroud | General Electric Co. (24446) General Electric Company (07482) | ||
| 2840-00-084-3107 2840000843107 | 9685M85G96 9084M45G02 9685M85G95 | Rotor, Compressor, Aircraft gas Tu | III End Item Identification: Gas turbine and jet acft engs Criticality Code Justification: AGAV Engine Section Location: Compressor | General Electric Company (07482) | |
| 2840-00-084-6695 2840000846695 | 5007T40P09 | Blade, Compressor, Aircraft gas Tu | III End Item Identification: Engine J-47, J-79, J-58 and T-64 Engine Section Location: Turbine Material: Titanium alloy blade | General Electric Company (99207) | |
| 2840-00-084-6860 2840000846860 | 6860192 | Vane, Outlet Guide | III End Item Identification: Acft eng TF-41 Criticality Code Justification: AGAV | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | |
| 2840-00-084-6867 2840000846867 | 6860194 | Vane, Outlet Guide | III End Item Identification: Acft eng TF-41 Criticality Code Justification: AGAV | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-084-6897 2840000846897 | 6860309 EU80062 | Tube, Transfer, Restr | Rolls-Royce Airlines (K0680) Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | ||
| 2840-00-084-6968 2840000846968 | 6860498 | Sleeve Assy, Air Ble | III End Item Identification: Eng TF-41 | Allison Transmission Inc. (73342) | |
| 2840-00-084-7050 2840000847050 | 6865643 | Blade, Compressor Rotor, Turbine Engine | Allison Transmission Inc. (73342) | ||
| 2840-00-084-7761 2840000847761 | 1-030-141-03 | Retainer, Bolt, sun Gear | III End Item Identification: T-53 series engines General Characteristics Item Description: Steel AMS6382, black oxide finish AMS2485, rockwell C scale 26 min, 28MAX hardness | Honeywell International Inc. (99193) | |
| 2840-00-084-7762 2840000847762 | 1-100-090-06 | Case, Combustion Chamber, Aircraft | III End Item Identification: AH-1, UH-1, OV-1 turbine engine, rotary wing aircraft III Part Name Assigned By Controlling Agency: Housing assembly, impellar | Honeywell International Inc. (99193) | |
| 2840-00-084-7916 2840000847916 | 6878193 | Ring, Adapter, Turbine Engine | III End Item Identification: Acft eng TF41 Criticality Code Justification: Adav and matt Material: Steel corrosion resisting | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-084-8469 2840000848469 | 2-160-730-01 | Clamp, Tube Assembly | III End Item Identification: T55-ENGINE General Characteristics Item Description: Clamp, steel, AMS5042, 75 min, 81.5 max rockwell 15 T scalehardness, two screw holes 0.218 in. dia, 1.000 in. C to C, oneteflon tape W/adhesive, 0.013 in. thk, 0.560 in. W, 1.750 in. lg, two screws per MS35276-263 III Fsc Application Data: Engine, acft, turbine | Honeywell International Inc. (99193) | |
| 2840-00-084-8677 2840000848677 | 6868839 | Plug, Borescope Port, Turbine | General Characteristics Item Description: Cres, ams 5754, 1.660-1.700 in. lg, 0.630-0.650 in. W, TWO0.279-0.288 in. dia holes on 0.5625 in. centerline radius 0.370 in.hole center to outer edge of beveled side III Fsc Application Data: Aircraft jet engine, TF41 | Allison Transmission Inc. (73342) | |
| 2840-00-085-3880 2840000853880 | 1-140-420-04 | Nozzle, Turbine, Aircraft gas Turb | III End Item Identification: T-53 series engines Special Features: 23 vanes, 2.025 in.min, 2.035 in.max O/a lg, 14.700 in.nom od, 2.615 in.min, 2.168 in.max id support, 44 holes 0.220 in.nom dia through nozzle flange equally spaced on 14.250 in.nom bolt circle dia, 12 holes 0.0975 in.min, 0.1025 in.max through support on 3.220 in.bolt circle dia; | Honeywell International Inc. (99193) | |
| 2840-00-085-4569 2840000854569 | 470492 | Shaft, Turbine, Aircraft gas Turbi | United Technologies Corporation (77445) | ||
| 2840-00-085-4573 2840000854573 | 408136 | Seal, Air, Aircraft gas Turbine En | Material: Steel overall Diameter: 1.360 inches nominal Overall Width: 0.0770 inches minimum and 0.0780 inches maximum | United Technologies Corporation (77445, 52661) | |
| 2840-00-085-7719 2840000857719 | 444976 | Seal, Air, Aircraft gas Turbine En | Material: Steel corrosion resisting overall Material Document and Classification: Ams 5643 assn std 1ST material response overall Overall Width: 0.0920 inches minimum and 0.0930 inches maximum | Dover Fluid Management (71687) United Technologies Corporation (77445) | |
| 2840-00-085-7743 2840000857743 | SSCY1526 | Plate, Backup | Stein Seal Company (03673) | ||
| 2840-00-085-7744 2840000857744 | 456083 | Seal, Air, Aircraft gas Turbine En | Kaydon Ring & Seal Inc. (75370) United Technologies Corporation (52661, 77445) | ||
| 2840-00-085-8968 2840000858968 | GB3146 32-53005-1011-2 | Head Assy, Pump | III End Item Identification: Eng J-47, J-79, T-58 and T-64 | Parker-Hannifin Corporation (86329) |