Turbo Power & Marine System Inc. NSN Parts: 321514 - 211147
FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 321514 | 2840-00-566-1826 | Spacer, Turbine Fron | 11449 | ||
| 194472 | 2840-00-396-4740 | Spacer, Turbine Nozzle | III End Item Identification: J-57 aircraft engine | 11449 | |
| 253538 | 2840-00-509-6058 | Spacer, Turbine Oute | 11449 | ||
| 348734 | 2840-00-475-0438 | Spacer, Turbine Outer | III End Item Identification: J-57 aircraft engine Criticality Code Justification: AGAV | 11449 | |
| 502364 | 2840-00-915-9631 | Spacerxgearbox Bear | 11449 | ||
| 275232 | 2840-00-523-3307 | Spring, E, Haust Nozz | 11449 | ||
| 4004058 | 2840-00-367-8391 | Spring, Finger Valve | General Characteristics Item Description: Nickel alloy, AMS5544, 2.150 in. min, 2.160 in. max, od, 0.004 in. min, 0.006 in. max thk | 11449 | |
| 4037401 | 2840-00-348-6204 | Stiffener, Augmentor Combustion C | III End Item Identification: Engine, acft, turbofan, model F100PW100 Criticality Code Justification: AGAV | 11449 | |
| 4050562-04 405056204 | 2840-01-084-6138 | Stiffener, Augmentor, Nozzle | III End Item Identification: Acft eng F100 General Characteristics Item Description: Titaninum alloy, ams 4911:ON a 77 deg. angle, 0.750 in. high, 0.677 in. lg, 0.020 min 0.028 max in. thk | 11449 | |
| 4037185 | 2840-00-348-6191 | Stiffener, Heatshield, Aircraft Ga | Engine Section Location: Turbine Material: Steel comp 321 shield End Item Identification: F100-PW-100/-200 aircraft engines | 11449 | |
| 4046904 | 2840-01-068-3901 | Stiffener, Manifold, Engine | III End Item Identification: Acft eng F16 General Characteristics Item Description: Stainless steel, ams 5643;ROCKWELL hardness C31-39, 3.815 in. min 3.835 in. max lg, 0.240 in. min 0.260 in. max THK;0.276 in. min 0.286 in. max dia of 2 holes | 11449 | |
| 4053560 | 2840-01-098-9505 | Stiffener, Nozzle Support | III End Item Identification: Acft eng F100 General Characteristics Item Description: Titanium alloy ams 4911, 6.470 in. lg, 0.018 min 0.023 max in. thk | 11449 | |
| 4053561 | 2840-01-098-9504 | Stiffener, Nozzle Support | III End Item Identification: Acft eng F100 General Characteristics Item Description: Titanium alloy ams 4911, 4.850 in. lg, 0.250 min 0.280 max in. dia of 2 holes | 11449 | |
| 4055310 | 2840-01-098-9498 | Stiffener, Nozzle Support | III End Item Identification: Acft eng F100 General Characteristics Item Description: Titainum alloy ams 4911, 13.260 min 13.300 max in. lg, irregularly shaped, 0.038 min 0.043 max in. thk | 11449 | |
| 4027176 | 2840-01-070-7272 | Stiffener, Turbine Exhaust Case | III End Item Identification: Acft eng F100 General Characteristics Item Description: Nickel alloy, spec pwa 1060;15.767 in. min 15.787 in. max dia, 0.183 in. min 0.191 in. max thk | 11449 | |
| 562927 | 2840-00-928-0817 | Stop, Bearing Tube | III End Item Identification: TF-30 aircraft engine | 11449 | |
| 589638 | 2840-00-819-7302 | Stop, Combustion Cha | 11449 | ||
| 634693 | 2840-01-087-7129 | Stop, Combustion Chamber Duct | III End Item Identification: Acft eng TF33 Criticality Code Justification: Matt and abhp and abmk and agav Special Features: Matl ams 5536 | 11449 | |
| 205359 | 2840-00-477-4213 | Stop, Compressor Bleed Valve Scre | General Characteristics Item Description: Steel, AMS5510, 0.420 in. H, 0.250 in. W III Fsc Application Data: Jet engine, J57 | 11449 | |
| 211147 | 2840-00-395-5663 | Stop, Compressor Stator | III End Item Identification: J-57 aircraft engine Criticality Code Justification: AGAV | 11449 |
