FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-008-6440, 2840-00-009-6059, 2840-00-009-7603
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-008-6440 2840000086440 | 576897 | Brace, Compressor Stator | General Characteristics Item Description: Corrosion resisting steel, ams 5504, 3.710 in. lg, 0.038-0.043 in. thkexcept at bends, 0.034-0.043 in. thk at bends III Fsc Application Data: Aircraft jet engine, J57 | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 2840-00-008-6441 2840000086441 | 576904 | Brace, Compressor Stator | General Characteristics Item Description: Corrosion resisting steel, ams 5504, 3.085 in. lg, 0.038-0.043 in. thkexcept at bends, 0.034-0.043 in. thk at bends III Fsc Application Data: Aircraft jet engine, J57 | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 2840-00-008-6442 2840000086442 | 576905 | Brace, Compressor Stator | General Characteristics Item Description: Corrosion resisting steel, AMS5504, 3.085 in. lg, 0.038-0.043 in. thkexcept at bends, 0.034-0.043 in. thk at bends III Fsc Application Data: Aircraft jet engine, J57 | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 2840-00-008-6444 2840000086444 | 576908 | Brace, Compressor Stator | General Characteristics Item Description: Corrosion resisting steel, ams 5504, 2.830 in. lg, 0.038-0.043 in. thkexcept at bends, 0.034-0.043 in. thk at bends III Fsc Application Data: Aircraft jet engine, J57 | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 2840-00-008-6445 2840000086445 | 576903 | Brace, Compressor Stator | III End Item Identification: Acft eng J57 Criticality Code Justification: ABHP Material: Steel corrosion resisting | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 2840-00-008-6447 2840000086447 | 709495 | Liner, Combustion Chamber, Aircraf | Criticality Code Justification: AGAV Engine Section Location: Combustion chamber Overall Length: 1.200 inches minimum and 1.210 inches maximum | United Technologies Corporation (77445) | |
| 2840-00-008-6448 2840000086448 | 709496 | Patch, Chamber, Combustion | III End Item Identification: Acft eng TF30 Criticality Code Justification: Abhp and abmk Material: Nickel alloy | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 2840-00-008-6449 2840000086449 | 709497 | Patch, Chamber, Combustion | III End Item Identification: Acft eng TF30 Criticality Code Justification: Abhp and abmk Material: Nickel alloy | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 2840-00-008-6452 2840000086452 | 6005T23G08 | Case, Axial Compressor, Turbine En | General Electric Company (99207) | ||
| 2840-00-008-9392 2840000089392 | 6012T94G02 | Case, Diffuser, Aircraft gas Turbi | III End Item Identification: J-85 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Compressor | General Electric Company (99207) | |
| 2840-00-008-9557 2840000089557 | 6867996 | Bracket Assembly, Fuel Tube | General Characteristics Item Description: Steel, ams 5512, consisting of one 6867996 bracket, one NUTPLATE6865392-4 or 6865394-4 or 6865395-4 III Fsc Application Data: Aircraft jet engine, TF41 | Allison Transmission Inc. (73342) | |
| 2840-00-009-3489 2840000093489 | 1-120-039-14 | Vane, fan, Aircraft gas Turbine En | III End Item Identification: T-63 series engines Special Features: Nickle alloy, M3602 fscm 91547, rockwell C scale 35 min, 40 maxhardness | Chromalloy Castings Tampa (52011) Honeywell International Inc. (99193) Howmet Corporation (3V257) | |
| 2840-00-009-4083 2840000094083 | 3038M78P02 3038M78P01 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: Acft eng. TF-39 Criticality Code Justification: AGAV Engine Section Location: Turbine | General Electric Company (07482) | |
| 2840-00-009-4084 2840000094084 | 3038M79P02 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: Acft eng. TF-39 Engine Section Location: Turbine Special Features: T.O. 2J-TF39-4;HONEYCOMBED | General Electric Company (07482) Kentucky Metals Inc. (8M212) | |
| 2840-00-009-4085 2840000094085 | 3038M80P02 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: Acft eng. TF-39 Engine Section Location: Turbine Special Features: T.O. 2J-TF39-4 | General Electric Company (07482) | |
| 2840-00-009-4285 2840000094285 | 576898 | Brace, Compressor Stator | III End Item Identification: Acft eng. J-57 Criticality Code Justification: Abhp and matt Material: Steel corrosion resisting | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 2840-00-009-6058 2840000096058 | 6866777 | Case, Combustion Chamber, Aircraft | III End Item Identification: TF41 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Compressor | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-009-6059 2840000096059 | 6866778-3 | Plate, Vane Retaining | III End Item Identification: Acft eng TF41 Criticality Code Justification: ABHP Material: Steel corrosion resisting | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-009-6060 2840000096060 | 6868739 | Housing, Antifriction Bearing, Air | Criticality Code Justification: AGAV Engine Section Location: Turbine Material: Steel housing | Allison Transmission Inc. (73342) Rolls-Royce Airlines (K0680) Rolls-Royce Corporation (63005) | |
| 2840-00-009-7603 2840000097603 | 6873603 | Housing, Antifriction Bearing, Air | Criticality Code Justification: AGAV Engine Section Location: Turbine Material: Steel comp 420 housing | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) |