FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-01-161-9820, 2840-01-162-2957, 2840-01-162-9518
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-01-161-9820 2840011619820 | 541957 | Vane, Compressor, Aircraft gas Tur | United Technologies Corporation (77445) | ||
| 2840-01-161-9821 2840011619821 | 4060866 | Duct, Exhaust, Aircraft gas Turbin | Criticality Code Justification: AGAV Engine Section Location: Exhaust Material: Titanium alloy overall | Unison Engine Components-Manchester (1J4P3) United Technologies Corporation (77445, 52661) | |
| 2840-01-162-0862 2840011620862 | 762859 | Plate, Diffuser Case | III End Item Identification: Acft eng TF33 General Characteristics Item Description: Steel ams 5504, rockwell C25-33 hardness, 0.071 min 0.085 max in. thk, 1.250 min 1.270 max in. dia 1 hole, 1.640 min 1.660 max in. dia 1 hole, 0.110 min 0.140 max in. dia | United Technologies Corporation (77445) | |
| 2840-01-162-1048 2840011621048 | 777875 576837 627424 627422 650792 | Housing, Gearbox, Turbine Engine | Engine Section Location: Accessory gearbox Material: Steel overall Overall Length: 7.114 inches nominal | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445, 52661) | |
| 2840-01-162-1049 2840011621049 | 704793 | Nozzle, Lubricating, Aircraft gas | Criticality Code Justification: Matt and abhp and agav Material: Steel overall Overall Length: 0.773 inches minimum and 0.777 inches maximum | United Technologies Corporation (77445) | |
| 2840-01-162-1050 2840011621050 | 761880 | Nozzle, Turbine, Aircraft gas Turb | III End Item Identification: Acft eng TF33 Special Features: Steel ams 5355, NO.2 bearing seal, 0.155 min in. 0.157 max IN.1 dia to 0.095 in.depth, 0.136 min IN.0.146 max IN.1 dia to 0.370 in.depth, 0.136 min IN.0.146 max IN.1 dia to 0.295 in.depth, 0.216 in.dia 28 UNJF-3B thd; | United Technologies Corporation (77445) | |
| 2840-01-162-2954 2840011622954 | B935253 B935255 | Vane, Turbine | III End Item Identification: Aircraft engine model F402RR406 | Rolls - Royce PLC (K0378) | |
| 2840-01-162-2955 2840011622955 | B936831 | Casing, Combustion | III End Item Identification: Aircraft engine model F402RR406 | Rolls - Royce PLC (K0378) | |
| 2840-01-162-2956 2840011622956 | B937342 B937956 | Blade, Turbine | III End Item Identification: Engine model F402 | Rolls - Royce PLC (K0378) | |
| 2840-01-162-2957 2840011622957 | B505030 | Rotor, Turbine, Aircraft gas Turbi | III End Item Identification: Engine model F402 Special Features: Cognizant service:navy | Rolls - Royce PLC (K0378) | |
| 2840-01-162-2958 2840011622958 | B937003 | Disk, Turbine, Turbine Engine | Rolls - Royce PLC (K0378) | ||
| 2840-01-162-3195 2840011623195 | 2-121-102-01 | Baffle, Turbine Nozzle | General Characteristics Item Description: Cres, ams 5536, rockwell 1ST scale 82 min 93 max hardness, lg 2.000 in. nom, 15.965 in. nom od, 15.280 in. nom id, 0.016 in. min 0.022 in. max thk material | Honeywell International Inc. (99193) | |
| 2840-01-162-3196 2840011623196 | 2-121-047-05 | Curl, Turbine Nozzle | General Characteristics Item Description: Cres fscm 91547 M3614, hardness rockwell 15-T82-92, irregular circular shape, curl od 17.980 in. nom, thk 0.030 in. min 0.038 in. max III Functional Description: Used on first turbine nozzle | Honeywell International Inc. (99193) | |
| 2840-01-162-4871 2840011624871 | 4044217-709 | Rotor and Stator as | United Technologies Corporation (77445) | ||
| 2840-01-162-5001 2840011625001 | B936967 | Disk, Turbine Rotor | Rolls - Royce PLC (K0378) | ||
| 2840-01-162-6087 2840011626087 | B505031 | Turbine, High Pressure | III End Item Identification: Engine model F402 | Rolls - Royce PLC (K0378) | |
| 2840-01-162-6962 2840011626962 | 2-141-460-06 | Vane Assembly, Exit | III End Item Identification: CH-47 turbine engine, rotary wing aircraft | Honeywell International Inc. (99193) | |
| 2840-01-162-7402 2840011627402 | 9940M34P03 | Seal, Metallic, Aircraft gas Turbi | III End Item Identification: Acft eng F101 Criticality Code Justification: AGAV Engine Section Location: Turbine | General Electric Company (07482) Unison Engine Components Inc. (16190) Electro-Methods Inc. (33617) | |
| 2840-01-162-9485 2840011629485 | 758029-1 | Lever, Idler | III End Item Identification: CH-47 turbine engine, rotary wing aircraft | Hamilton Sundstrand Corporation (73030) | |
| 2840-01-162-9518 2840011629518 | 2-300-831-02 442938-04 | Harness Assembly, Th | Honeywell International Inc. (99193) Ametek Inc. (97424) |