Turbo Power & Marine System Inc. NSN Parts: 578296 - 500511

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FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

MFG SKUNSNItem NameDetailsCAGE CodeRFQ
5782962840-00-988-5007Plate, Locking, Compr11449

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6970892840-00-469-7107Plate, Mounting eng11449

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6269042840-00-927-6097Plate, Mounting StrapIII End Item Identification: TF-30 aircraft engine
11449

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4461102840-00-823-6611Plate, Mounting, Case, CompressorIII 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

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5032182840-00-690-2097Plate, Mounting, Case, CompressorIII 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

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4287492840-00-806-7802Plate, Mounting, Case, DiffuserIII 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

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4287502840-00-806-7818Plate, Mounting, Case, DiffuserIII 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

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4287982840-00-808-1020Plate, Mounting, Case, DiffuserIII 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

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5032202840-00-690-2092Plate, Mounting, Case, DiffuserIII 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

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5032212840-00-690-2090Plate, Mounting, Case, DiffuserIII 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

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5048752840-00-759-6326Plate, Mounting, Case, TurbineIII 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

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4049982840-00-806-7748Plate, Mounting, Control, FuelIII 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

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4936232840-00-755-7521Plate, Mounting, Fuel FilterIII 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

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4215462840-00-801-0867Plate, Mounting, GearboxIII 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

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3282352840-00-166-2360Plate, Nozzle Segment, AfterburnerIII 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

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7382272840-00-166-2360Plate, Nozzle Segment, AfterburnerIII 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

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40131992840-01-016-5749Plate, Nozzle StatorIII 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

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2317342840-00-098-2952Plate, Oil Pump11449

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2397882840-00-098-2952Plate, Oil Pump11449

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5005112840-00-015-1661Plate, Oil Tank RetaIII End Item Identification: Acft eng TF-33
Criticality Code Justification: Matt and abhp and adav and agav
Special Features: Matl ams 5510
11449

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