Aircraft and Missile Prime Movers Engine Fuel System Components: 575843, 576449, 576761

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
575843 2915-00-062-9706Sleeve, Piston GuideIII End Item Identification: 29151391823
Hamilton Sundstrand Corporation (73030)

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575969 2915-00-962-9060Bell Crank, AdjustinExperimental Tool Corp. (18751)
Hamilton Sundstrand Corporation (73030)
The Durol Company (7D869)

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575970 2915-01-509-1148Lever, Adjustment Speed setIII End Item Identification: TF33PW102 aircraft engine
Hamilton Sundstrand Corporation (73030)

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575C263P2 2915-00-611-7387Valve Assembly, RestGeneral Electric Co. (24446)
General Electric Company (07482)

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575C315P2 2915-00-632-0605Attenuator Assy, fueGeneral Electric Co. (24446)
General Electric Company (07482)

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576049 2915-00-963-1512Retainer, CylinderHamilton Sundstrand Corporation (73030)

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576050 2915-00-754-6160Bushing, Spherical, Fuel ControlIII End Item Identification: 29159549585
General Characteristics Item Description: Plastic, hamilton standard, spec no. HS1401, grade a, 0.622 in. spherical body dia, 0.375 in. min, 0.376 in. max body id, 0.350 in. body lg
Hamilton Sundstrand Corporation (73030)

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5763164-101
5763164101
2915-01-207-8728Diaphragm Assembly, SecondaryParker-Hannifin Corporation (59211)

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576320 2915-00-074-2273Lock, FeedbackIII End Item Identification: Engine model T58-GE-8B
Hamilton Sundstrand Corporation (73030)

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576354 2915-00-981-1754Plate, FlapperHamilton Sundstrand Corporation (73030)

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576360 2915-00-981-1758Plate, FlapperHamilton Sundstrand Corporation (73030)

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576362 2915-00-353-8074Diaphragm and StopGeneral Characteristics Item Description: Steel and fabric coated with rubber, 6 mtg holes 0.164 in. dia, 0.307 in. O/a W
A G C Incorporated (98500)
Hamilton Sundstrand Corporation (73030)
Ontic Engineering & Manufacturing (45934)

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576384 2915-00-074-2274Cap, EndIII End Item Identification: Engine model T58-GE-8B
Hamilton Sundstrand Corporation (73030)

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576388 2915-00-761-9844Plate, LockingIII End Item Identification: 29159539325
General Characteristics Item Description: Cres, AMS5513, AMS5515, AMS5516 or MIL-S-5059, comp 302, rockwell superficial hardness, 75.5 R15N, irregular shape, 0.042 in. O/a thk
Hamilton Sundstrand Corporation (73030)

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576391 2915-00-761-9845Sleeve, FittingIII End Item Identification: Engine model T58
Hamilton Sundstrand Corporation (73030)

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576449 2915-00-757-9160Retainer, Spring, Fuel ControlIII End Item Identification: 29150508338
General Characteristics Item Description: Cres, 0.535 in. O/a lg
Hamilton Sundstrand Corporation (73030)

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576588 2915-01-190-9221Tube Assembly, Aircraft EngineIII End Item Identification: Acft eng TF33
Criticality Code Justification: AGAV
United Technologies Corporation (77445)

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576703 2915-00-074-3398Housing and InsertsIII End Item Identification: Fuel control model no. JFC26
Hamilton Sundstrand Corporation (73030)

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576710 2915-00-962-9066Restrictor and ScreHamilton Sundstrand Corporation (73030)

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576761 2915-00-931-5742Manifold Assembly, Afterburner SpGeneral Characteristics Item Description: Nickel alloy, ams 5586 tube material, 0.042-0.056 in. tube thk, 0.309-0.315 in. tube od, rockwell C34 min hardness
III Fsc Application Data: Aircraft jet engine, TF30
United Technologies Corporation (52661,77445)
Woodward FST Inc. (65065)

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