FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-01-038-3207, 2840-01-038-3219, 2840-01-039-0904
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-01-038-3207 2840010383207 | 9113M91P02 | Nozzle Assembly, Discharge | III End Item Identification: Acft engine J79-15/17 Criticality Code Justification: AGAV | General Electric Company (07482) | |
| 2840-01-038-3217 2840010383217 | 767922 | Shroud Segment, Turbine, Aircraft | III End Item Identification: Acft engine TF33-P3/5/9/11A Criticality Code Justification: Czbj and apgf and abhp and abmz Engine Section Location: Turbine | United Technologies Corporation (77445) | |
| 2840-01-038-3219 2840010383219 | 749975 | Strut, Exit fan | III End Item Identification: Acft engine TF30-P100 Criticality Code Justification: Feat and agav Special Features: Matl titanium alloy ams 4926 | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 2840-01-038-3299 2840010383299 | 4059351 | Strap, Bleed Valve | III End Item Identification: Aircraft engine, F100-PW-100 Criticality Code Justification: Abhp and agav Overall Length: 74.218 inches minimum and 74.238 inches maximum | United Technologies Corporation (77445, 52661) | |
| 2840-01-038-3316 2840010383316 | 37E501086P112 | Blade, Turbine Rotor, Aircraft gas | General Electric Company (99207) | ||
| 2840-01-038-3317 2840010383317 | 5007T93P02 | Blade, Compressor, Aircraft gas Tu | III End Item Identification: Aircraft engine, J85-GE-5, -17, -13 Criticality Code Justification: AGAV Engine Section Location: Compressor | General Electric Company (99207) | |
| 2840-01-038-4295 2840010384295 | 3900T20P04 | Pinstrapassy | General Characteristics Item Description: Pin, 0.156 in. dia, first end chamfered 15 deg 0.050 lg, second end pointed 30 deg with 0.02 spherical radius, AMS5796, strap is AMS5536, 0.600 in.lg, 0.028 in. min 0.036 in. max thick, 0.970 in. wd over pin, welded to pin, 0.060 from chamfered end | General Electric Company (99207) | |
| 2840-01-038-5562 2840010385562 | 4050T18G01 | Bracket, Igniter Lead-Rear | III End Item Identification: Aircrft engine J85-GE-21A | General Electric Company (99207) | |
| 2840-01-038-5663 2840010385663 | 304D912P5 | Support, Compressor | General Electric Company (07482) | ||
| 2840-01-038-7094 2840010387094 | 4024264 | Brace, Turbine Exhaust Cone | III End Item Identification: Aircraft engine F100-PW-100 General Characteristics Item Description: Steel, corrosion resistiant, ams 5599, 2.480 in. min. l, 2.560 in. max. l, 0.990 in. min. W, 1.010 in. max. W, O/a dim. 0.160 in. min. H, 0.180 in. max. H | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 2840-01-038-8329 2840010388329 | 7014M80G02 | Bellcrank, Lever Van | General Electric Company (07482) | ||
| 2840-01-038-8939 2840010388939 | 546234 | Brace, Inlet Case | III End Item Identification: Acft engine J-57 Criticality Code Justification: Feat and abmk and abhp and agav Special Features: Matl titanium ams 4901 | United Technologies Corporation (77445) | |
| 2840-01-038-8987 2840010388987 | 4050207 | Support, Turbine Duct | III End Item Identification: Aircraft engine F100-PW-100 Criticality Code Justification: Matt and adav and abhp and agav Special Features: Matl ams 5707 | United Technologies Corporation (77445) | |
| 2840-01-038-8988 2840010388988 | 6738627 6890918 6789386 | Flange, Starter Drive | III End Item Identification: Acft engine T56-A-9B/C | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) General Motors Corp. (24617) | |
| 2840-01-038-9083 2840010389083 | 634E592P11 | Blade, Turbine Rotor, Aircraft gas | General Electric Company (99207) | ||
| 2840-01-038-9104 2840010389104 | 6013T84G06 | Case, Combustion Chamber, Aircraft | General Electric Company (99207) | ||
| 2840-01-038-9105 2840010389105 | 37R601231P118 6013T84G07 37R601112P119 | Case, Combustion Chamber, Aircraft | III End Item Identification: Aircraft engine, J85-GE-21A Criticality Code Justification: AGAV Engine Section Location: Combustion chamber | General Electric Company (99207) | |
| 2840-01-038-9111 2840010389111 | 4050593 4050590 4050591 050591 | Case, Diffuser, Aircraft gas Turbi | United Technologies Corporation (52661, 77445) | ||
| 2840-01-039-0903 2840010390903 | 3026768 | Liner, Combustion Chamber, Turbine | III End Item Identification: Engine model T400 | Pratt and Whitney Canada Inc. (00198) | |
| 2840-01-039-0904 2840010390904 | 3024862CL12-0 | Nozzle Assembly, Turbine, Aircraft | III End Item Identification: Engine model T400 | Pratt and Whitney Canada Inc. (00198) |