Turbo Power & Marine System Inc. NSN Parts: 752308 - 432580

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FSC 2995 Miscellaneous Engine Accessories, Aircraft

MFG SKUNSNItem NameDetailsCAGE CodeRFQ
7523082995-01-011-3774Detector, Metallic ParticleSpecial Features: APPLICATION-TF33 engine oil system;steel body, 1.055 in. lg, 3A thd class, 3/4 in. hex head, lead not included
Thread Quantity per inch: 20
Nominal Thread Size: 0.500 inches
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7523072995-01-012-0873Holder, Metal Chip DetectorGeneral Characteristics Item Description: Consists of aluminum body, aluminum piston and steel spring, lg 1.205 in. min 1.295 in. max, body od 0.655 in. min 0.665 in. max, hex head 0.928 in. min 0.940 in. max across flats, external thd 0.750-16 UNF-3A, internal thd 0.500-20 UNF-3B
III Fsc Application Data: Oil sump, TF33 turbine engine
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4710502995-01-161-7441Housing Assembly, BlIII End Item Identification: U/O TF33-PW-102 eng, E/I KC135 acft
General Characteristics Item Description: C/O 2 pins pn 268830 nsn 5315008055848, 6 studs pn 463067 ea 2.260 in. lg, housing pn 565387, 2 pn AN152626
III Fsc Application Data: Miscellaneous engine accessories, aircraft
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5192582995-00-941-7447Housing Assy, Contro11449

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4917422995-00-919-6246Housing, Control PistonIII End Item Identification: 2995001398687 743548 control assy, pressure ratio bleed, acft engine
General Characteristics Item Description: Steel, chrome plated
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2361182995-00-611-3615Housing, Oil Pump Assembly, EngineFsc Application Data: Gas turbines and jet engines, aircraft; and components
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4968392995-00-794-8577Housing, RegulatorIII End Item Identification: 2995007418399 425809 regulator
General Characteristics Item Description: Cres cylindrical housing and rectangular support
III Fsc Application Data: Regulator assy, anti and icing air, acft engine
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3939092995-00-771-3199Lever, Pressure Rati11449

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4674392995-00-979-7947Manifold, Air, Diffus11449

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3150622995-00-567-6647Manifold, Fluid, AircraftConnection Quantity: 3
Metering Valves: Not provided
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3283152995-00-614-5378Manifold, Fluid, AircraftIII End Item Identification: Acft eng J57
Criticality Code Justification: AGAV
III Reference Data and Literature: T.O. 2J-57-24
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3755562995-00-777-0347Manifold, Fluid, AircraftIII End Item Identification: Acft eng J75
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40336732995-00-345-4025Manifold, Fluid, AircraftIII Part Name Assigned By Controlling Agency: Manifold-fuel supply, left, assembly of
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40336742995-00-345-4029Manifold, Fluid, AircraftIII Part Name Assigned By Controlling Agency: Manifold-fuel supply, right, assembly of
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4293122995-00-808-1019Manifold, Fluid, AircraftIII End Item Identification: Acft eng TF33
Criticality Code Justification: AGAV
III Reference Data and Literature: T.O.2J-TF33-4
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4889592995-00-966-2985Manifold, Fluid, AircraftIII End Item Identification: Acft eng TF33
Criticality Code Justification: AGAV
III Reference Data and Literature: T.O. 2J-TF33-4
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5055692995-00-761-8023Manifold, Fluid, AircraftIII End Item Identification: Acft eng TF33
Criticality Code Justification: AGAV
III Reference Data and Literature: T.O. 2J-TF33-14
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5129952995-00-941-3655Manifold, Pressure s11449

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6115762995-00-406-2818Manifold-Supply, AircraftIII End Item Identification: TF-30 aircraft engine
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4325802995-00-854-5986Nut, Anti-Icing AirIII End Item Identification: 2995007948577 496839 regulator
General Characteristics Item Description: Matl ams 5735 sst;o/a lg 0.490 to 0.510 in.;o/a W 0.365 to 0.385 in.;hole dia 0.190 in., thd 0.190-32 unjf, thd class 3B;SILVER plate, ams 2411, 0.0003 to 0.0006 in.
III Fsc Application Data: Anti and icing air, acft engine
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