FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-831-8037, 2840-00-832-3303, 2840-00-832-3310
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-831-8037 2840008318037 | EU13005 6864586 | Grommet, Retaining | Rolls-Royce Airlines (K0680) Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | ||
| 2840-00-831-8038 2840008318038 | 6864588 EU13008 | Window, Level, Tank | Rolls-Royce Corporation (63005) Rolls-Royce Airlines (K0680) Allison Transmission Inc. (73342) | ||
| 2840-00-831-8047 2840008318047 | EU56593A 6863848 | Shield, Heat, Aircraft gas Turbine | Engine Section Location: Turbine End Item Identification: TF-41 aircraft engine | Allison Transmission Inc. (73342) Rolls-Royce Airlines (K0680) Rolls-Royce Corporation (63005) | |
| 2840-00-831-8052 2840008318052 | 6863895 EU57728 | Plate, Retaining | Rolls-Royce Airlines (K0680) Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | ||
| 2840-00-831-8082 2840008318082 | 6865616 EU80892 | Blade, Turbine Rotor, Aircraft gas | III End Item Identification: TF-41 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Turbine | Rolls-Royce Airlines (K0680) Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | |
| 2840-00-831-8086 2840008318086 | 6860007 | Nozzle Assembly, Turbine, Aircraft | III End Item Identification: TF-41 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Turbine | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | |
| 2840-00-831-8087 2840008318087 | 6860920 | Washer, cup | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | ||
| 2840-00-831-8088 2840008318088 | EU24718 6863374 | Segment, Locating | Rolls-Royce Airlines (K0680) Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | ||
| 2840-00-831-8090 2840008318090 | 6860015 | Blade, Compressor, Aircraft gas Tu | III End Item Identification: TF-41 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Low pressure compressor | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-831-8104 2840008318104 | 5019M62P01 | Bracket, Angle, Engine | III End Item Identification: Acft eng Criticality Code Justification: Matt and abmk and abhp and agav Special Features: Matl ams 5510 | General Electric Company (07482) | |
| 2840-00-831-8113 2840008318113 | 6860027 | Disk and hub, Turbine, Turbine eng | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | ||
| 2840-00-831-8118 2840008318118 | 6860031 | Shaft, Turbine, Aircraft gas Turbi | III End Item Identification: TF-41 aircraft engine Criticality Code Justification: AGAV | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-831-8121 2840008318121 | 6860032 | Shaft, Turbine, Aircraft gas Turbi | III End Item Identification: TF-41 aircraft engine Criticality Code Justification: AGAV | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | |
| 2840-00-832-3082 2840008323082 | 37D400189G002 | Turbine Rotor, Turbine Engine | General Electric Company (99207) General Electric Co. (24446) | ||
| 2840-00-832-3300 2840008323300 | 3005T29P02 | Housing, Antifriction Bearing, Air | Criticality Code Justification: AGAV Engine Section Location: Accessory gearbox Material: Steel housing | General Electric Company (99207) | |
| 2840-00-832-3301 2840008323301 | 37E501296P112 | Case, Turbine, Aircraft gas Turbin | General Electric Company (99207) | ||
| 2840-00-832-3302 2840008323302 | 4005T91P01 | Seal, Metallic, Aircraft gas Turbi | III End Item Identification: J-85 aircraft engine Criticality Code Justification: Matt and abmk and agav Special Features: Matl ams 6322/5323 | General Electric Company (99207) | |
| 2840-00-832-3303 2840008323303 | SSCY2723 4006T75P02 | Seal, Rubbing | General Characteristics Item Description: Steel ams 5610 and carbon rings ls graphite co compound 67, irregular cross-sectional shape, 1.530 in. O/a lg cross-section, 0.936 in. thk cross-section, 2.667 in. id, 4.540 in. od, six 0.224IN. dia mtg holes equally spaced on 4.100 in. dia, mtg holes positionedin relation to one 0.125 in. dia thru hole in body | General Electric Company (99207) Stein Seal Company (03673) | |
| 2840-00-832-3305 2840008323305 | 4007T13P05 | Seal Segment, Turbine | III End Item Identification: J-85 aircraft engine General Characteristics Item Description: Steel AMS5759 material of body, steel ams 5536 material ofhoneycomb, 64 deg 18 min segment, 4.114 in. inside radius, 4.164 in.outside radius of flange, 0.355 in. max H O/a, three 0.1665 in.dia holes spaced 20 deg C to C on 4.355 in. radius | Union Machine Company of Lynn Inc. (51992) Ferrotherm Corporation (01993) Metro Machine Works Inc. (50554) | |
| 2840-00-832-3310 2840008323310 | 5011T76P01 | Disk, Turbine, Turbine Engine | General Electric Company (99207) |