Turbo Power & Marine System Inc. NSN Parts: 578296 - 500511
FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
---|---|---|---|---|---|
578296 | 2840-00-988-5007 | Plate, Locking, Compr | 11449 | ||
697089 | 2840-00-469-7107 | Plate, Mounting eng | 11449 | ||
626904 | 2840-00-927-6097 | Plate, Mounting Strap | III End Item Identification: TF-30 aircraft engine | 11449 | |
446110 | 2840-00-823-6611 | Plate, Mounting, Case, Compressor | III End Item Identification: Engine model TF33 General Characteristics Item Description: Steel, AMS6350 or AMS6355, rockwell C32-38 hardness, cadmium plate, ams 2400, 2.757 in. lg, 2.465 in. W, 0.115-0.135 in. thk III Fsc Application Data: Aircraft jet engine | 11449 | |
503218 | 2840-00-690-2097 | Plate, Mounting, Case, Compressor | III End Item Identification: Engine model TF33 General Characteristics Item Description: Steel, AMS6350 or AMS6355, rockwell C32-38 hardness, cadmium-plate, AMS2400, 2.520 in. lg, 1.690 in. W, 0.071-0.085 in. thk III Fsc Application Data: Acft jet engine | 11449 | |
428749 | 2840-00-806-7802 | Plate, Mounting, Case, Diffuser | III End Item Identification: Engine model TF33 General Characteristics Item Description: Cres, AMS5504, rockwell C30-38 hardness, 3.602 in. lg, 1.735 in. W, 0.056-0.062 in. thk III Fsc Application Data: Acft jet engine | 11449 | |
428750 | 2840-00-806-7818 | Plate, Mounting, Case, Diffuser | III End Item Identification: Engine model TF33 General Characteristics Item Description: Cres, AMS5504, rockwell C30-38 hardness, 2.650 in. lg, 1.745 in. W, 0.056-0.062 in. thk III Fsc Application Data: Acft jet engine | 11449 | |
428798 | 2840-00-808-1020 | Plate, Mounting, Case, Diffuser | III End Item Identification: Engine model TF33 General Characteristics Item Description: Cres, AMS5504, rockwell C30-38 hardness, 1.810-1.870IN. lg, 1.510-1.670 in. W, 0.056-0.062 in. thk III Fsc Application Data: Acft jet engine | 11449 | |
503220 | 2840-00-690-2092 | Plate, Mounting, Case, Diffuser | III End Item Identification: Engine model TF33 General Characteristics Item Description: Cres, ams 5504, 1.702 in. O/a lg, 1.675 in. O/a W, 0.071-0.085 in. thk III Fsc Application Data: Aircraft jet engine | 11449 | |
503221 | 2840-00-690-2090 | Plate, Mounting, Case, Diffuser | III End Item Identification: Engine model TF33 General Characteristics Item Description: Cres, ams 5504, rockwell C30-38 hardness, 1.734-1.858 in. lg, 1.638-1.762 in. W, 0.071-0.085 in. W III Fsc Application Data: Aircraft jet engine | 11449 | |
504875 | 2840-00-759-6326 | Plate, Mounting, Case, Turbine | III End Item Identification: Engine model TF33 General Characteristics Item Description: Cres, ams 5504, rockwell C30-38 hardness, 2.624 in. lg, 2.212 in.W, 0.120-0.130 in. thk III Fsc Application Data: Aircraft jet engine | 11449 | |
404998 | 2840-00-806-7748 | Plate, Mounting, Control, Fuel | III End Item Identification: Engine model TF33 General Characteristics Item Description: Steel, AMS6350 or AMS6355, rockwell C32-38 hardness, cadmium plate, AMS2400, 6.509 in. lg, 2.339 in. W, 0.085 in. thk III Fsc Application Data: Acft jet engine | 11449 | |
493623 | 2840-00-755-7521 | Plate, Mounting, Fuel Filter | III End Item Identification: Engine model TF33 General Characteristics Item Description: Cres, ams 5504, 1.847 in. lg, 1.515-1.525 in. W, 0.115-0.125 in.thk, rockwell C30-38 hardness III Fsc Application Data: Aircraft jet engine | 11449 | |
421546 | 2840-00-801-0867 | Plate, Mounting, Gearbox | III End Item Identification: Engine model TF33 General Characteristics Item Description: Steel, AMS6350 or AMS6355, rockwell C32-38 hardness, 3.670 in. lg, 2.212 in. W, 0.044-0.056 in. thk III Fsc Application Data: Acft jet engine | 11449 | |
328235 | 2840-00-166-2360 | Plate, Nozzle Segment, Afterburner | III End Item Identification: Engine model J75 General Characteristics Item Description: Cres, ams 5525, 2.340-2.360 in. lg, 0.056-0.060 in. thk, 0.440-0.450 in. W, straight serration data-teeth 17 per inch, linearpitch 0.0588 in., pressure angle 30 deg, O/a depth 0.035 in., filletradius 0.005 in. max III Fsc Application Data: Aircraft jet engine | 11449 | |
738227 | 2840-00-166-2360 | Plate, Nozzle Segment, Afterburner | III End Item Identification: Engine model J75 General Characteristics Item Description: Cres, ams 5525, 2.340-2.360 in. lg, 0.056-0.060 in. thk, 0.440-0.450 in. W, straight serration data-teeth 17 per inch, linearpitch 0.0588 in., pressure angle 30 deg, O/a depth 0.035 in., filletradius 0.005 in. max III Fsc Application Data: Aircraft jet engine | 11449 | |
4013199 | 2840-01-016-5749 | Plate, Nozzle Stator | III End Item Identification: Engine, acft, turbofan, model no. F100-PW-100 General Characteristics Item Description: Cobalt alloy per pratt and whitney spec no. pwa 1015, 0.690 in. min, 0.710 in. max lg, 0.240 in. min, 0.280 in. max W | 11449 | |
231734 | 2840-00-098-2952 | Plate, Oil Pump | 11449 | ||
239788 | 2840-00-098-2952 | Plate, Oil Pump | 11449 | ||
500511 | 2840-00-015-1661 | Plate, Oil Tank Reta | III End Item Identification: Acft eng TF-33 Criticality Code Justification: Matt and abhp and adav and agav Special Features: Matl ams 5510 | 11449 |